| ALSTOM TECHNOLOGY LTD Patent applications |
| Patent application number | Title | Published |
|---|
| 20120129113 | SYSTEM AND METHOD OF MANAGING ENERGY UTILIZED IN A FLUE GAS PROCESSING SYSTEM - A method for managing an amount of energy utilized by a carbon dioxide capture system that includes providing a fuel and a feed stream including oxygen to a combustion system. The feed stream includes a portion of a flue gas stream generated upon combustion of the fuel in the combustion system. The flue gas stream is subjected to a carbon dioxide capture system to remove carbon dioxide therefrom and an amount of at least one of an oxygen stream or the portion of the flue gas stream introduced to the feed stream is adjusted such that the feed stream maintains an oxygen concentration in a range of between 10% to 90% by volume and the carbon dioxide capture system operates at an energy load between about 1.4 GJ/ton of carbon dioxide and about 3.0 GJ/ton of carbon dioxide. | 05-24-2012 |
| 20120128473 | ROTATING MACHINE - A rotating machine cooled by a cooling medium directed through the rotating machine in a main flow and a secondary flow includes a rotor. A stator includes a swirl passage configured to guide the secondary flow so as to be discharged from a pre-swirl nozzle. At least one control device includes a shape-memory alloy disposed in an area of the pre-swirl nozzle and is configured to control the secondary flow based on a temperature in an automated manner. | 05-24-2012 |
| 20120127766 | CONFIGURABLE HYBRID CONVERTER CIRCUIT - A circuit for a hybrid voltage source converter suitable for high voltage DC power transmission and reactive power compensation. The circuit comprises an assembly of electrically interconnected elements (Elements | 05-24-2012 |
| 20120126044 | OSCILLATION MONITOR FOR PULVERIZER JOURNAL ASSEMBLY - A pulverizer | 05-24-2012 |
| 20120125240 | SYSTEM AND METHOD OF MANAGING ENERGY UTILIZED IN A FLUE GAS PROCESSING SYSTEM - A method is provided for managing an amount of energy utilized by a carbon dioxide capture system. The method includes providing a fuel and a feed stream to a combustion system. The feed stream includes oxygen and a portion of a flue gas stream generated upon combustion of the fuel. The method also includes subjecting the flue gas stream to a carbon dioxide capture system to remove carbon dioxide therefrom, measuring a concentration of oxygen present in the feed stream, and selectively adjusting an amount of the flue gas stream included in the feed stream based on the measured concentration of oxygen in the feed stream. The selective adjustment is performed such that the feed stream maintains an oxygen concentration in a range of between about 10% to 90% by volume and the carbon dioxide capture system operates at an energy load between 1.4 GJ/ton of carbon dioxide and 3.0 GJ/ton of carbon dioxide. | 05-24-2012 |
| 20120122045 | SEAL ARRANGEMENT - A seal arrangement for a silo combustor includes a first casing and a second casing each forming a passageway for a gas, an end portion of the first casing being disposed radially inside an end portion of the second casing such that the first and the second casing form an overlapping region having a radial gap. A segmented seal has at least two adjacent segments disposed in the overlapping region so as to seal the radial gap, wherein the first casing includes at least one opening disposed in a region between the at least two adjacent segments. | 05-17-2012 |
| 20120122043 | COMBUSTION CHAMBER AND METHOD FOR DAMPING PULSATIONS - A combustion chamber is provided and includes a combustion device and a supply circuit arranged to feed fuel at a plurality of locations of the combustion device. The supply circuit includes manifolds collecting fuel to be distributed among at least some of the locations, ducts extending from the manifolds and feeding the locations. Some of the ducts carry valves having a plurality of predetermined working positions, each working position corresponding to a different fuel flow through the valve. | 05-17-2012 |
| 20120121377 | GAS TURBINE ARRANGEMENT AND METHOD FOR OPERATING A GAS TURBINE ARRANGEMENT - A gas turbine arrangement and a method of operating are provided. The turbine includes an annulus, axially delimited between a rotor unit, and at least one stationary component. Cooling medium outlet openings, lead into the annulus, from the stationary component. The cooling medium flows into cooling medium inlet openings, in the rotor unit in a flow direction, which propagates through the annulus. At least one inner cavity, radially to the annulus, is delimited by the rotor unit and by the stationary component. The inner cavity is pressurized with a purging gas, and is fluidically connected to the annulus. The stationary component and the rotor unit include a constriction by which the inner cavity is separated from the radially outer annulus and via which the inner cavity is fluidically connected to the radially outer annulus. Flow guides, fastened on the stationary component on one side, project into the constriction. | 05-17-2012 |
| 20120114492 | METHOD OF MODIFYING A STEAM TURBINE - A method of modifying a steam turbine to change from a first maximum thermal power of the steam generator to a second maximum thermal power of the steam generator. The method can include replacing, in the high-pressure module, at least one set of fixed blades sized for the first maximum thermal power by at least one set of fixed blades sized for the second maximum thermal power. The at least one set of moving blades are sized to operate at the first and second maximum thermal powers. The rotor and the at least one set of moving blades of the high-pressure module remain unchanged on changing from the first maximum thermal power to the second maximum thermal power. | 05-10-2012 |
| 20120113699 | Converter - A voltage source converter for use in high voltage DC power transmission and reactive power compensation. The voltage source converter comprises at least one converter limb including first and second DC terminals for connection in use to a DC network and an AC terminal for connection in use to an AC network. | 05-10-2012 |
| 20120112583 | ELECTRIC MACHINE, INSULATING CAP AND METHOD FOR FORMING AN INSULATING CAP - The electric machine has a stator with windings connected to phase connections. An insulating cap protects the reciprocally connected portions of the phase connections and windings. The insulating cap has a box-shaped body with an opening for the introduction of a winding within it. The body defines a seat housing the phase connection. The seat is formed in one piece with the body. | 05-10-2012 |
| 20120111978 | SYSTEM AND METHOD FOR MONITORING OPERATIONAL CHARACTERISTICS OF PULVERIZERS - In a system for monitoring the operating condition of a pulverizer, a sensor interface module positioned on or proximal to the pulverizer. The sensor interface module is operable to receive information generated by one or more sensors mounted on the pulverizer. An operator control station is in communication with the sensor interface module and is operable to receive data from the sensor interface module relevant to the signals received from the sensors. The operator control station is also operable to generate operational information indicative of a functional characteristic of the pulverizer and to track the operational information to determine whether degradation of the functional characteristic is occurring. | 05-10-2012 |
| 20120111535 | ORIFICE PLATE FOR CONTROLLING SOLIDS FLOW, METHODS OF USE THEREOF AND ARTICLES COMPRISING THE SAME - Disclosed herein is an orifice plate comprising one or more plates having orifices disposed therein; the orifices being operative to permit the flow of solids from a moving bed heat exchanger to a solids flow control system; where the orifice plate is downstream of a tube bundle of the moving bed heat exchanger and upstream of the solids flow control system and wherein the orifice plate is operative to evenly distribute the flow of solids in the solids flow control system. | 05-10-2012 |
| 20120111243 | CONTROL VALVE AND CONTROL VALVE SYSTEM FOR CONTROLLING SOLIDS FLOW, METHODS OF MANUFACTURE THEREOF AND ARTICLES COMPRISING THE SAME - Disclosed herein is a solids flow control valve comprising a standpipe; a shoe; and a transport pipe; wherein the standpipe is in operative communication with the shoe and lies upstream of the shoe; the standpipe comprising a first end and a second end, where the first end is in contact with a source that contains disposable solids and the second end is in fluid contact with the shoe; the shoe being operative to restrict the flow of the disposable solids; the transport pipe being disposed downstream of the shoe to receive and transport the solids from the shoe. | 05-10-2012 |
| 20120109341 | METHOD FOR ASCERTAINING PROCESS VALUES FOR A PROCESS CONTROL - A method for ascertaining process values for a process control is provided. The method includes detecting a measured value, providing a model that simulates the process, and, on the basis of the model, calculating a calculated real value and a calculated measured value. The method also includes comparing the calculated real value with the calculated measured value to obtain a delay compensation value, and adding the delay compensation value to the measured value to obtain an accelerated value indicative of the process value to be ascertained. | 05-03-2012 |
| 20120107111 | BLADE ARRANGEMENT, ESPECIALLY STATOR BLADE ARRANGEMENT - A blade arrangement on a wall of a fluid flow path of a turbomachine includes a locating channel disposed in the wall and having undercut flanks. A plurality of glades each having a blade-side root section corresponding to the undercut flanks a plurality of intermediate filling pieces correspond to the undercut flanks and separate each of the blade-side root sections. The plurality of blade-side root sections and intermediate filling pieces are seated in a form-fitting manner and fixed in a force-locking manner in the locating channel. The plurality of intermediate filling pieces fill out the locating channel so as to form a gas flow-side surface essentially free of a disturbing contour between the blade-side root sections. Each of the plurality of intermediate filling pieces includes a threaded hole disposed essentially perpendicular to a base of the channel. A screw is disposed in the threaded hole. | 05-03-2012 |
| 20120104055 | FLOW DEFLECTORS FOR FUEL NOZZLES - A fuel nozzle assembly including a conduit defining a fuel inlet and a fuel outlet and being operable to convey a fuel stream comprising a solid particulate fuel entrained in a fluid. The conduit has a flow area defined by an interior surface of the conduit. A first flow deflector and a second flow deflector extend inwardly from the interior surface. The first flow deflector and the second flow deflector are positioned to disrupt a velocity profile of the flow stream established upstream of the conduit. | 05-03-2012 |
| 20120103236 | REDUCED WEAR AND SELF CLEANING STOKER SEAL - A sealing apparatus ( | 05-03-2012 |
| 20120102968 | METHOD FOR CONTROLLING A GAS TURBINE AND GAS TURBINE FOR IMPLEMENTING THE METHOD - A method for controlling a gas turbine, including during transient operating states, and such a gas turbine are provided. The gas turbine includes a compressor for compressing inducted combustion air, a combustion chamber for generating hot gas by combusting a fuel with the aid of the compressed combustion air, and a multistage turbine for expanding the generated hot gas and performing work. The controlling of the gais turbine is carried out in accordance with the hot gas temperature which is derived from a plurality of other measured operating variables of the gas turbine. A reliable controlling of the gas turbine is achieved, even during rapid changes, by pressure measurements being gathered exclusively at different points of the gas turbine for derivation of the hot gas temperature. | 05-03-2012 |
| 20120090328 | POWER PLANT - A power plant includes a gas turbine unit adapted to feed whose flue gases into a boiler of a steam turbine unit, to be then diverted into a recirculated flow and discharged flow. The recirculated flow is mixed with fresh air forming a mixture that is fed into a gas turbine unit compressor. The discharged flow is fed into a CO | 04-19-2012 |
| 20120090327 | POWER PLANT AND METHOD FOR ITS OPERATION - The power plant includes a gas turbine unit adapted to feed flue gases into a diverter where they are divided into a recirculated flow and a discharged flow. The recirculated flow is fed into a mixer together with fresh air to form a mixture that is fed to the gas turbine unit. The gas turbine unit includes a combustion chamber where a fuel is burnt together with the mixture. A control unit is provided, that is supplied with information regarding the fuel C2+ and/or H | 04-19-2012 |
| 20120090326 | POWER PLANT - A power plant includes a gas turbine unit adapted to feed flue gases into a diverter where they are divided into a recirculated flow that is fed into a mixer together with fresh air to form a mixture that is fed to a gas turbine unit compressor inlet, and a discharged flow, that is fed into a CO | 04-19-2012 |
| 20120087852 | METHOD AND SYSTEM FOR REDUCING LIME CONSUMPTION IN DRY FLUE GAS DESULFURIZATION SYSTEMS - In a method for reducing lime consumption in DFGD systems, a slaker is provided wherein lime and water is introduced to produce a slaked lime slurry. The slurry is introduced into a spray dryer wherein the slurry is atomized. A flue gas stream is also introduced into the spray dryer and reacts with the atomized slurry, causing calcium sulfate and sulfite, as well as unreacted lime particulate to form. A portion of the particulate is filtered and sent back in a substantially dry form to the slaker to form part of the slurry. | 04-12-2012 |
| 20120087782 | GAS TURBINE - A gas turbine includes a rotor having a rotor groove and a rotor bore extending through the rotor, the rotor bore having a diffuser-shaped rotor bore exit. A blade is attached to the rotor and includes a blade tip having at least one dust hole. An airfoil has a leading edge and a trailing edge extending along a longitudinal axis of the blade between a lower end of the airfoil and the blade tip. A blade root is disposed at the lower end of the airfoil and is configured to be removably disposed in the rotor groove. The blade root includes a blade inlet having a cross sectional area that exceeds a cross sectional area of the rotor bore in at least one direction. A hollow blade core is disposed in the airfoil and extends along the longitudinal axis of the blade between the blade root and the blade tip. | 04-12-2012 |
| 20120085849 | BOWL MILL DEFLECTOR - A deflector ( | 04-12-2012 |
| 20120085099 | TUNABLE SEAL IN A GAS TURBINE ENGINE - A system and method for tuning a gas turbine combustion system having a plurality of seals positioned between the combustion system and the turbine inlet is disclosed. The system and method provide ways of permitting a predetermined amount of compressed air to bypass the combustion system and enter the turbine so as to control emissions and dynamics of the combustion system. The seals contain a plurality of holes to meter airflow passing therethrough and are positioned such that they can be removed from the engine and modified to increase or decrease the amount of air passing therethrough. | 04-12-2012 |
| 20120084980 | Extending Useful Life of a Cobalt-Based Gas Turbine Component - A method of extending the useable life of a gas turbine component fabricated from a cobalt-based alloy is disclosed. The method includes applying a rejuvenation process to the alloy where the alloy is placed in a protected atmosphere and heated to three different elevated temperatures and held at the elevated temperatures for approximately four hours each. Application of the rejuvenation process allows gas turbine components to be returned to service for at least one more service interval of approximately 24,000 operating hours. | 04-12-2012 |
| 20120073666 | GAS FLOW CONTROL ARRANGEMENT - A gas flow control arrangement for use in an exhaust gas cleaning system, comprising a duct ( | 03-29-2012 |
| 20120073375 | METHOD FOR CHECKING THE MECHANICAL INTEGRITY OF STABILIZING ELEMENTS ON THE ROTOR BLADES OF A TURBINE AND SCANNING DEVICE FOR IMPLEMENTING THE METHOD - A method for checking a mechanical integrity of at least two stabilizing elements includes providing the at least two stabilizing elements that mechanically interconnect blade airfoils of rotor blades of a turbine in a circumferential direction of the turbine in an installed state of the turbine. The at least two stabilizing elements are adjacent to one another and inter-engage to form an engagement section having a material volume of the at least two stabilizing elements in the engagement section. The material volume of the at least two stabilizing elements is scanned, in an automated manner using ultrasound, so as to determine whether cracks are present. The scanning is performed from an outside of the at least two stabilizing elements. | 03-29-2012 |
| 20120073305 | COMBUSTION CHAMBER AND METHOD FOR OPERATING A COMBUSTION CHAMBER - A combustion chamber of a gas turbine including first and second premixed fuel supply devices connected to a combustion device having first zones connected to the first premixed fuel supply devices and second zones connected to the second premixed fuel supply devices. The second fuel supply devices are shifted along a combustion device longitudinal axis with respect to the first fuel supply devices. The first zones are axially upstream of the second premixed fuel supply devices. | 03-29-2012 |
| 20120072053 | ROBOT PLATFORM FOR REMOTELY CONTROLLED AND/OR AUTONOMOUS INSPECTION OF TECHNICAL FACILITIES - A robot platform is provided, which is intended in particular for remotely controlled and/or autonomous inspection of technical facilities, in particular in power stations, and comprises at least a drive mechanism configured to move the robot platform, an inspection device configured to inspect the technical facility and a communication device for exchanging measurement and/or control data. Particular flexibility in use and extended areas of use are achieved in that the robot platform is modular and the communication device operates in accordance with a uniform standard. | 03-22-2012 |
| 20120070309 | BLADE FOR A GAS TURBINE - A blade, for a gas turbine, includes a blade airfoil, having a shroud segment arranged on its upper end. The shroud segment together with shroud segments of other blades of a blade row forming an annular shroud which delimits hot gas passage of the gas turbine, and said shroud segment, on sides on which it adjoins adjacent shroud segments of the annular shroud, is provided with upwardly projecting side rails which extend along a side edge, to improve sealing to the hot gas passage. The side rails include rail-parallel or essentially rail-parallel, upwardly open slots through which cooling air, which is introduced via the shroud segment from an interior of the blade airfoil, discharges into the space above the shroud segment. | 03-22-2012 |
| 20120070308 | COOLED BLADE FOR A GAS TURBINE - A cooled blade for a gas turbine includes an airfoil section which extends in the radial direction of the turbine or in the longitudinal direction of the blade between a platform and a blade tip which is provided with a cap. The airfoil section is bounded transversely with respect to the longitudinal direction by a leading edge and a trailing edge and has a pressure face and a suction face. Cooling channels extend in a radial direction between the platform and the blade tip in an interior of the airfoil section. The cooling channels can be acted upon by a cooling air flow from the platform. The blade tip is cooled by first cooling holes for convection cooling provided on the pressure face of the blade, and second cooling holes for film cooling provided on the suction side of the blade, through the cap of the blade, in the blade tip from the cooling channels, and distributed over the blade width. | 03-22-2012 |
| 20120068560 | ARRANGEMENT OF CONDUCTING BAR ENDS - An arrangement includes conducting bar ends connected together and a cap) covering them filled with a putty. The cap is made of a resin containing a high thermal conductivity filler. The putty is a silicone elastomer containing a high thermal conductivity filler. | 03-22-2012 |
| 20120067046 | POWER PLANT WITH CO2 CAPTURE AND WATER TREATMENT PLANT - A power plant for the generation of electrical energy comprises steam and/or gas turbines ( | 03-22-2012 |
| 20120064610 | SOLVENT AND METHOD FOR CO2 CAPTURE FROM FLUE GAS - The present disclosure describes the efficient use of a catalyst, an enzyme for example, to provide suitable real cyclic capacity to a solvent otherwise limited by its ability to absorb and maintain a high concentration of CO | 03-15-2012 |
| 20120063911 | DUAL BRAZING ALLOY ELEMENT, PROCESS FOR PRODUCING IT AND USES THEREOF - A dual brazing alloy element for a materially integral connection of a ceramic surface to a metallic surface includes a first layer having a Ni-based brazing alloy with a Ni content of at least 50% by weight and having at least one component configured to lower a melting point of the Ni-based brazing alloy selected from the group consisting of Si, B, Mn, Sn and Ge. A second layer includes an active brazing alloy material having a total content of 1-15% by weight of at least one active element selected from the group consisting of Ti, Hf, Zr and V. | 03-15-2012 |
| 20120063891 | COOLED COMPONENT FOR A GAS TURBINE - A cooled component for a gas turbine is disclosed, which by an outer side of a wall delimits hot gas passage of the gas turbine and on an inner side has a device for impingement cooling. The impingement cooling device can include a multiplicity of impingement cooling chambers which are arranged next to each other, operate in parallel, are covered by impingement cooling plates which are equipped with impingement cooling holes, and are impinged upon by cooling air during operation. | 03-15-2012 |
| 20120060689 | METHOD AND SYSTEM FOR REDUCING ENERGY REQUIREMENTS OF A CO2 CAPTURE SYSTEM - A method for reducing energy requirements of a CO | 03-15-2012 |
| 20120060611 | INSPECTION VEHICLE FOR THE INSPECTION OF SUBSTANTIALLY CYLINDRICAL OBJECTS - An inspection vehicle for inspecting a substantially cylindrical object composed of a magnetizable material includes a chassis. A plurality of wheels is disposed on the chassis so as to be rotatable and is configured to move the chassis in a circumferential direction along an external surface of the cylindrical object, at least some of the plurality of wheels being motor-drivable. The plurality of wheels is disposed so as to provide a chassis clearance allowing a movement of the chassis over an obstruction on the external surface of the cylindrical object. A magnetic device is disposed on the chassis and is configured to hold the vehicle on the external surface of the cylindrical object. | 03-15-2012 |
| 20120060503 | TRANSITIONAL REGION FOR A COMBUSTION CHAMBER OF A GAS TURBINE - A gas turbine including a combustion chamber and a first row of guide vanes, arranged essentially directly downstream thereof, of a turbine. The outer and/or inner limitation of the combustion chamber defined by at least one outer and/or inner heat shield, mounted on at least one combustion chamber structure arranged radially outside and/or inside. The hot gases flow path in the region of the guide vane row being restricted radially on the outside and/or inside by an outer and/or inner vane platform, mounted at least indirectly on at least one turbine carrier. A minimal gap size directly upstream of the first row of guide vanes is achieved by mounting at least indirectly on the turbine carrier at least one mini heat shield, arranged upstream of the first row of guide vanes and essentially adjacent the vane platform and in the flow direction between the heat shield and the vane platform. | 03-15-2012 |
| 20120056496 | METHOD FOR CONNECTING AN INDUCTIVE LOAD AND CONNECTING CIRCUIT FOR CARRYING OUT THE METHOD - A method is provided for connecting an inductive load, especially a winding of a generator, for testing purposes to a predetermined alternating medium voltage, whereby the inductive load is connected to the medium voltage by means of a breaker. To reduce the inrush current, the connection is timed to come into effect when the medium voltage has a predetermined phase. | 03-08-2012 |
| 20120055162 | LANCE OF A BURNER - The lance of a burner includes a body that defines a first duct with first nozzles for injecting a liquid fuel and a second duct with second nozzles for injecting a gaseous fuel. Outlets of the first nozzles are spaced apart from outlets of the second nozzles. The body includes a third duct with third and fourth nozzles for injecting air. The third nozzles surround an axis of the first nozzles and the fourth nozzles surround an axis of the second nozzles. | 03-08-2012 |
| 20120039709 | METHOD AND DEVICE FOR ADJUSTING THE ROTOR POSITION IN A GAS TURBINE OR STEAM TURBINE - A method is provided for adjusting the position of a rotor of a turbine. The turbine includes a first casing and a second casing. The second casing, in a bearing region of the rotor, has a fixed relative position, with regard to a rotor end, and is screwed to the first casing via a threaded connection. The method includes releasing the threaded connection; adjusting the relative position of the rotor to the first casing, which encloses the rotor in the flow region, by the relative position of the second casing to the first casing being adjusted; and refastening the threaded connection. Furthermore, a gas turbine or a steam turbine with such a device for adjusting the relative position of rotor and casing is also described. | 02-16-2012 |
| 20120038308 | ROTATING TRANSFORMER FOR SUPPLYING THE FIELD WINDING IN A DYNAMOELECTRIC MACHINE - An apparatus for transmission of electrical power includes an AC voltage source configured to produce AC voltage. A stator includes a primary winding arrangement electrically fed from the AC voltage source, the primary winding arrangement having at least two primary windings. A rotor includes a secondary winding arrangement inductively coupled to the primary winding arrangement of the stator, the rotor being rotatable in a rotation direction about a rotation axis. The rotation axis does not pass through the at least two primary windings, and the at least two primary windings each extend over a predetermined sector with respect to the rotation direction and are disposed offset with respect to one another with in the rotation direction. | 02-16-2012 |
| 20120038241 | DEVICE FOR AXIAL TENSIONING OF A STATOR COIL OF AN ELECTRICAL MACHINE - An apparatus axial stresses a stator winding of an electrical machine, the winding including a plurality of winding bars, the ends of the winding bars passing axially out of a core of a stator and forming a widened end winding at least one axial end face of the core. A plurality of winding supports is distributed circumferentially and substantially at a right angle with respect to the end winding on the at least one axial end face of the core. At least one axially acting compression spring device is configured to support the plurality of winding supports on the at least one axial end face of the core and to axially stress the plurality of winding supports. A readjusting device communicates with at least one of the plurality of winding supports and has an axially adjustable contact surface, the at least one axially acting compression spring device being axially supported on the core and on the axially adjustable contact surface of the readjusting device. | 02-16-2012 |
| 20120036864 | GAS TURBINE ENGINE AND METHOD FOR COOLING THE COMPRESSOR OF A GAS TURBINE ENGINE - A gas turbine engine includes a compressor with rotor blades having roots connected into seats of a compressor drum. The rotor blade roots and/or the compressor drum have longitudinal passages for a cooling fluid, connecting higher pressure areas to lower pressure areas of the gas turbine engine. | 02-16-2012 |
| 20120036860 | GAS TURBINE PLANT WITH EXHAUST GAS RECIRCULATION AND ALSO METHOD FOR OPERATING SUCH A PLANT - A gas turbine plant is provided with exhaust gas recirculation and includes a main gas turbine having a main compressor and main turbine driving a main generator, and a combustion chamber, with an outlet connected to the inlet of the main gas turbine, has a fuel feed, and via the recuperator's high-pressure side obtains combustion air from the main gas turbine's compressor outlet. The outlet of the main turbine and the inlet of the main compressor are connected via the recuperator's low-pressure side and a cooler for exhaust gas recirculation. On the recuperator's low-pressure side, a charging unit, with a compressor and a turbine is arranged, and draws in air via an air intake and by the outlet of its compressor is connected to the recuperator's low-pressure side outlet and by the inlet of its turbine is connected to a surplus-gas extraction line on the recuperator's low-pressure side. | 02-16-2012 |
| 20120031101 | GAS TURBINE WITH FLOW SEPARATION AND RECIRCULATION - A method is provided for CO | 02-09-2012 |
| 20120030936 | METHOD FOR PRODUCTION OF A CONDUCTOR BAR FOR THE STATOR OF AN ELECTRICAL MACHINE, IN PARTICULAR OF A GENERATOR, AND AN APPARATUS FOR PRODUCTION OF A CONDUCTOR BAR - A method is disclosed for production of a conductor bar for the stator of a generator, which conductor bar has a plurality of internal partial conductors which are surrounded externally by insulation which includes an insulating ribbon which is wound around the partial conductors, with the insulating ribbon which is wound around the partial conductors being impregnated with an impregnation fluid. The conductor bar is compressed after the impregnation of the insulating ribbon and at least at times during a curing phase. An apparatus is likewise provided, and can be designed to compress at least an axial section of the conductor bar at least at times during a curing phase of the impregnated insulating ribbon. | 02-09-2012 |
| 20120028199 | IGNITOR SPARK STATUS INDICATOR - An ignitor spark indicator | 02-02-2012 |
| 20120027568 | LOW-PRESSURE STEAM TURBINE AND METHOD FOR OPERATING THEREOF - The disclosure relates to a multi-stage low-pressure steam turbine and a method for operating thereof. The steam turbine includes a last stage in which the leading edge of each vane of the last stage is skewed so as to form a W shaped K-distribution across the span of the vanes. This shape allows for efficient last stage operation at low last stage exit velocities. The disclosure includes a method for operating such a steam turbine at a last stage exit velocity between 125 m/s and 150 m/s. | 02-02-2012 |
| 20120020787 | COOLED BLADE FOR A GAS TURBINE - A cooled blade for a gas turbine includes a blade airfoil extending between leading and trailing edges in a flow direction and on suction and pressure sides is delimited by a wall, which include an interior space in which cooling air flows towards the trailing edge in the flow direction and discharges to the outside in the region of the trailing edge. The pressure-side wall terminates at a distance in front of the trailing edge in the flow direction, forming a pressure-side lip, such that the cooling air discharges from the interior space on the pressure side. Multiple ribs subdivides the interior space, parallel to the flow direction, into a plurality of parallel cooling passages which create a high pressure drop and in which turbulators are arranged for increasing cooling. Before the outlet, multiple flow barriers are provided in the cooling air flow path, distributed transversely to the flow direction. | 01-26-2012 |
| 20120020768 | COOLED CONSTRUCTIONAL ELEMENT FOR A GAS TURBINE - A cooled constructional element for a gas turbine includes a wall having a front and a rear side. The front side is configured to be thermally loaded during operation of the turbine, and the rear side has a plurality of pins projecting therefrom in a two-dimensional distribution, the two-dimensional distribution including a higher density distribution of pins in a critical zone of the cooled constructional element than in the remaining regions of the cooled constructional element. A device is configured to create jets of a cooling medium that are directed onto the rear side of the wall in a region of the plurality of pins so as to cool the rear side of the wall by impingement. | 01-26-2012 |
| 20120017604 | GAS TURBINE ARRANGEMENT AND METHOD FOR RETROFITTING SAME - A gas turbine arrangement includes a compressor, a combustion chamber and a turbine connected to one another. A casing housing the compressor has flanges connectable to pipes providing secondary air to at least one of the combustion chamber and the turbine. The flanges define passages having an asymmetric cross section. A method for retrofitting a gas turbine arrangement is also provided. | 01-26-2012 |
| 20120001514 | STATOR BAR - A high voltage stator bar includes a substantially quadrangular conductive element made of a plurality of interwoven strands, and an electric insulation applied around the conductive element. The permittivity at the corners of the electric insulation decreases by less than 60% from an inner insulation zone facing the conductive element towards an outer insulation zone. | 01-05-2012 |
| 20110318191 | THERMALLY LOADED, COOLED COMPONENT - A thermally loaded, cooled component thermally coupled to a cooling system configured to receive a gaseous cooling introduced in a forced manner from outside that flows through the cooling system so as to absorb and transport heat away from the component as a result of thermal contact with the component. The component includes at least one Helmholtz resonator configured to improve thermal contact between the cooling medium and the component. | 12-29-2011 |
| 20110314815 | POWER PLANT WITH CO2 CAPTURE - A method is provided for operating a combined cycle power plant having at least one gas turbine, a heat recovery steam generator (HSRG), a steam turbine and a CO2 capture system. The method includes recirculating a first partial flow of flue gases from the HRSG. The method also includes capturing CO2 from a second partial flow of flue gases from the HRSG; and operating a supplementary firing to increase the net power output of the plant and to at least partly compensate the power consumption of the CO2 capture system. A combined cycle power plant is also provided. The plant includes at least one gas turbine, at least one heat recovery steam generator, at least one steam turbine at least one CO2 capture system, and flue gas recirculation. The plant also includes a low excess air supplementary firing. | 12-29-2011 |
| 20110311352 | METHOD FOR CHECKING THE BEARING ALIGNMENT IN A GAS TURBINE - The disclosure refers to a method and apparatus for checking the bearing alignment of a rotor of a gas turbine or steam turbine having a rotor with a radial offset and a radial offset surface and in a bearing shell, which supports the rotor, with a radial, at least in sections, end surface, wherein the radial offset surface and the radial end surface face the free end of the rotor. The radial offset is arranged in the bearing shell and offset towards the free end of the rotor. The degree of offset in the axial direction with regard to the rotor is measured at least two different circumferential positions around the rotor periphery in order to determine the alignment of the rotor. Differences in the degree of offset at different circumferential positions are used as measurement for the bearing alignment. | 12-22-2011 |
| 20110308630 | HELMHOLTZ DAMPER AND METHOD FOR REGULATING THE RESONANCE FREQUENCY OF A HELMHOLTZ DAMPER - A Helmholtz damper, including an enclosure, a neck extending from the enclosure, and a pipe for inserting into the neck. The portions of the pipe inserted into the neck is adjusted to regulate a resonance frequency of the Helmholtz damper. | 12-22-2011 |
| 20110304155 | POWER PLANT WITH CO2 CAPTURE AND COMPRESSION | 12-15-2011 |
| 20110303135 | REGENERATIVE AIR PREHEATER DESIGN TO REDUCE COLD END FOULING - An air preheater | 12-15-2011 |
| 20110302929 | EXHAUST GAS HOUSING FOR A GAS TURBINE AND METHOD FOR PRODUCING SAME - An exhaust gas housing for a gas turbine is provided and includes a support structure, which, arranged concentrically, includes an outer ring and an inner ring which are interconnected by radially arranged struts, and a flow liner, which is attached inside the support structure and, arranged concentrically, includes an outer liner and an inner liner which are interconnected by radially arranged liner ribs. The liner ribs each encompass the struts of the support structure, and the outer and inner liners inside the support structure form an annular passage for the turbine's hot exhaust gases. The liner ribs are welded together from front and rear parts in the flow direction, forming welded seams which extend axially in the outer liner and in the inner liner up to the liner edge. End rings, which cover the welded seams at the liner edge, are welded on the liner's rear edges for reinforcement. | 12-15-2011 |
| 20110302922 | POWER PLANT WITH CO2 CAPTURE - A method is provided for operating a combined cycle power plant including a CO | 12-15-2011 |
| 20110300357 | THERMAL BARRIER COATING SYSTEM, COMPONENTS COATED THEREWITH AND METHOD FOR APPLYING A THERMAL BARRIER COATING SYSTEM TO COMPONENTS - A thermal barrier coating system on a base material includes a bond coat layer with a lower face in direct contact with the base material and an upper face, a first ceramic layer in direct contact with the upper face of the bond coating layer and a second ceramic layer disposed on an outermost surface of the coating system and configured to be exposed to hot gas. The first ceramic layer includes a layer, combination, mixture, alloy, blend or multilayer structure of at least one of yttria-stabilized zirconia with a yttria content in a range of 6-8 wt-%, YTaO4 doped zirconia, and titania doped zirconia. The second ceramic layer includes a layer, combination, mixture, alloy, blend or multilayer structure of at least one of YTaO4 doped zirconia, titania doped zirconia, scandia stabilized zirconia, ceria containing perovskite material, yttrium aluminium garnet material, Monazite material, and spinel material. A material of the second ceramic layer is different from a material of the first ceramic layer. | 12-08-2011 |
| 20110297270 | TECHNIQUE FOR APPLYING PROTECTIVE COVERING TO PIPES AND TUBES - The manufacture of clad tubes ( | 12-08-2011 |
| 20110293428 | METHOD FOR OPTIMIZING THE CONTACT SURFACES OF SHROUD SEGMENTS, WHICH ABUT AGAINST ONE ANOTHER, OF ADJACENT BLADES OF A GAS TURBINE - A method for optimizing the contact surfaces of abutting shroud segments of adjacent blades of a rotor blade row of a gas turbine includes providing a 3-D model of an individual blade. A geometry of the individual blade is calculated using the 3-D model while considering centrifugal forces, temperature stresses and pressure loads experienced in a loaded state of the blade during operation. The contact surfaces of the abutting shroud segments of adjacent blades are optimized in the loaded state of the blade. The optimization includes the surfaces of functionally serving interlocking surfaces and functionally serving wedge surfaces disposed on each side of the interlocking surfaces. A geometry of the interlocking surfaces and of the wedge surfaces in an unloaded state corresponding to the optimized contact surfaces in the loaded state of the blade is calculated. | 12-01-2011 |
| 20110293402 | GAS TURBINE - A gas turbine including an inner casing and a rotor having rotatable blades with a shroud and a fin, and a cooling arrangement arranged in a cavity in the casing and about the rotatable blade. The blade shroud includes a protrusion extending away from the blade leading edge into the cavity and openings in the cavity wall for a cooling fluid. The protrusion is defined by angles in relation to the flow channel wall. The protrusion affects a vortex flow of cooling fluid entering through the openings and a vortex flow of hot gas entering from the flow channel into the cavity. The double-vortex formation reduces a mixing of the cooling flow with the hot gas flow and increases the efficiency of the cooling arrangement of the blade shroud and cavity walls. | 12-01-2011 |
| 20110291311 | PROCESS FOR EXTENDING THE CYCLIC SERVICE LIFE OF THERMAL BARRIER COATINGS, IN PARTICULAR ON GAS TURBINE COMPONENTS - A process for extending the cyclic service life of thermal barrier coatings made of yttrium-stabilized zirconium oxide (YSZ) or the like which have been applied to a substrate with an oxidizing bond coat in between includes increasing or long-term stabilizing the strain tolerance of the thermal barrier coating. | 12-01-2011 |
| 20110289899 | COMBINED CYCLE POWER PLANT WITH FLUE GAS RECIRCULATION - An exemplary method for the operation of a CCPP with flue gas recirculation to reduce NOx emissions and/or to increase the CO2 concentration in the flue gases to facilitate CO2 capture from the flue gases as well as a plant designed to operate is disclosed. To allow a high flue gas recirculation ration (rFRG) an imposed combustion inhomogeneity ratio (ri) is used for flame stabilization. The imposed combustion inhomogeneity ratio (ri) is controlled as function of the flue gas recirculation rate (rFRG) and/or combustion pressure. Oxygen or oxygen enriched air to the gas turbine inlet gases or to the combustor is admixed to enhance operatability. | 12-01-2011 |
| 20110289898 | COMBINED CYCLE POWER PLANT WITH FLUE GAS RECIRCULATION - An exemplary system method for the operation of a CCP P with flue gas recirculation to reduce NOx emissions and/or to increase the CO2 concentration in the flue gases to facilitate CO2 capture from the flue gases is disclosed. The flue gas recirculation rate (rFRG) is controlled as function of the combustion pressure and/or the hot gas temperature. Operability is enhanced by admixing of oxygen or oxygen enriched air to the gas turbine inlet gases or to the combustion. | 12-01-2011 |
| 20110286856 | AIRFOIL FOR A COMPRESSOR BLADE - The present disclosure provides an improved second stage airfoil for a compressor blade having a unique chord length (CD) stagger angle (γ) and camber angle (Δβ). The stagger angle (γ) and camber angle (Δβ) provide improved aerodynamics while the chord length (CD) provides for reduced airfoil weight. | 11-24-2011 |
| 20110286850 | AIRFOIL FOR A COMPRESSOR BLADE - The present disclosure provides an improved first stage airfoil for a compressor blade having a unique chord length (CD) stagger angle (γ) and camber angle (Δβ). The stagger angle (γ) and camber angle (Δβ) provide improved aerodynamics while the chord length (CD) provides for reduced airfoil weight. | 11-24-2011 |
| 20110286849 | BLADE FOR A GAS TURBINE - A blade is disclosed for a gas turbine including an airfoil, which extends along a longitudinal axis from a blade root to a blade tip, and has a shroud segment at the blade tip. The shroud segment abuts with first and second edges against shroud segments of adjacent blades to form a ring-like shroud. The first and second edges are each provided with a respective side rail on the upper side of the shroud segment. Each of the side rails is subdivided into sections of different height and/or width. | 11-24-2011 |
| 20110286834 | GUIDE VANE FOR A GAS TURBINE - A guide vane is provided for a gas turbine and has an airfoil extending in the radial direction between an inner platform and an outer platform. The airfoil extends transversely to the direction of the hot gas flow between a leading edge and a trailing edge and has a pressure side and a suction side. A cooling slot running parallel to the trailing edge is provided on the pressure side in front of the trailing edge, a cooling medium can exit through the cooling slot from the guide vane over the entire length of the guide vane and can cool the trailing edge of the guide vane. In such a guide vane, the service life is extended by a thermal stress reducing element provided on the inner platform below the trailing edge and the cooling slot. | 11-24-2011 |
| 20110284669 | LANCE OF A GAS TURBINE BURNER - A lance of a gas turbine burner includes an inner duct having inner nozzles; an annular outer duct encircling the inner duct and having outer nozzles; and a spacer disposed between a terminal portion of the inner duct and a terminal portion of the outer duct, the spacer being fixed to both the inner duct and the outer duct. | 11-24-2011 |
| 20110270503 | SELECTING AND APPLYING TO FUEL-FLOW SPLITS BIAS VALUES TO CORRECT FOR ELEVATED INLET AIR HUMIDITY - Methods for controlling a gas turbine engine are provided, where a compressor inlet temperature, ambient temperature, and relative humidity are measured. Utilizing these measurements, it is first determined whether an evaporation cooler is actively importing water content into inlet air entering the compressor. This determination is based on whether the inlet air is substantially cooler than the ambient temperature. If so, an EC correction factor is added to an inlet air temperature value (CTIM) and set as an air temperature parameter (INLETIM). Second, it is determined whether the relative humidity is greater than a predefined threshold. If so, a relative humidity (RH) correction factor is added to CTIM and set as the INLETIM. Next, the INLETIM and TTRF are located in a look-up table, and a bias value corresponding to these inputs is identified. The fuel-flow for a fuel circuit is adjusted according to the identified bias value. | 11-03-2011 |
| 20110270502 | EMPLOYING FUEL PROPERTIES TO AUTO-TUNE A GAS TURBINE ENGINE - A tuning process is provided for monitoring fuel properties of a fuel being consumed by a gas turbine (GT) engine, and for dynamically tuning the GT engine as a function of changes to the monitored fuel properties. Initially, readings are taken from the GT engine during a reference calibration, or commissioning, and utilized to calculate an initial-pressure-drop reference value. The tuning process during commercial operation takes post-calibration readings from the GT engine to calculate a fuel property parameter, which represents a heating value of the fuel. Specifically, the fuel property parameter is calculated by deriving a corrected-pressure-drop dynamic value as a function of pressure and temperature readings of the fuel at a point upstream of a combustor and pressure drops across fuel nozzles that introduce the fuel into the combustor, and solving a ratio of the dynamic value and the reference value. | 11-03-2011 |
| 20110268582 | COOLED BLADE FOR A GAS TURBINE - A blade for a gas turbine, is provided and includes a blade airfoil which extends in a blade longitudinal direction and at the lower end merges into a shank which terminates in a blade root for fastening the blade on a blade carrier, particularly on a rotor disk. Devices for cooling the blade, which are supplied with a cooling medium, especially cooling air, via a feed hole arranged on the shank at the side, are arranged inside the blade airfoil. In the region of the feed hole provision is made for a planar stiffening element which reaches beyond the immediate region of the feed hole for reducing peaks of mechanical stress. | 11-03-2011 |
| 20110268574 | BLADE ROW FOR THE FINAL STAGE OF A STEAM TURBINE - A rotating blade row is provided for the final stage of a steam turbine has blades with an integrated shroud. The shroud of each blade has a projection in the axial direction, in each case on its pressure side, which prevents droplets in the working fluid of the steam turbine from reaching the shroud fillet of the respective subsequent blade in the flow direction. The shroud fillet is therefore protected against erosion damage caused by droplets impact erosion. The projection is positioned and of such a size that mass equilibrium is ensured between the suction side and the pressure side of the shroud, and stress equilibrium is ensured between the projection on the pressure side and the suction-side shroud. The projection furthermore has a recess between its greatest axial extent and the leading edge. | 11-03-2011 |
| 20110265487 | Dynamically Auto-Tuning a Gas Turbine Engine - Tuning processes implemented by an auto-tune controller are provided for measuring and adjusting the combustion dynamics and the emission composition of a gas turbine (GT) engine via a tuning process. Initially, the tuning process includes monitoring parameters, such as combustion dynamics and emission composition. Upon determining that one or more of the monitored parameters exceed a critical value, these “out-of-tune” parameters are compared to a scanning order table. Upon comparison, the first out-of-tune parameter that is matched within the scanning order table is addressed. The first out-of-tune parameter is then plotted as overlaid slopes on respective graphs, where the graph represents a fuel-flow split. Typically, the slopes are plotted as a particular out-of-tune parameter against a particular fuel-flow split. The slopes for each graph are considered together by taking into account the combined impact on each out-of-tune parameter when a fuel-flow split is selected for adjustment. | 11-03-2011 |
| 20110265475 | METHOD AND APPARATUS FOR COLD STARTING A STEAM TURBINE - The disclosure relates to a method and apparatus for cold starting a steam turbine by preheating a steam turbine component using eddy currents. The process includes providing an electrically conducting steam turbine component, an electro-magnetic coil, and a supply of AC to the coil. The coil is located relative to the component so that the coil is capable of forming eddy currents in the component. In this location, an AC current is passed through the coil thus heating the component. | 11-03-2011 |
| 20110259574 | ADJUSTABLE HEAT EXCHANGER - Disclosed herein is a novel, adjustable heat exchanger | 10-27-2011 |
| 20110254562 | METHOD AND DEVICE FOR DETECTING SHORT-CIRCUITS IN THE STATOR CORE OF ELECTRIC MACHINES - A method for detecting turn-to turn faults in a laminate stack of a stator of an electrical machine or a generator includes magnetizing the stator using an auxiliary coil and an auxiliary current so as to form a magnetic field. The magnetic field is measured using a pickup device including at least two detectors disposed in at least two respective different radial positions with respect to a rotor axis so as to provide at least two signals corresponding to the magnetic field at the respective radial positions. The method includes evaluating and comparing a magnitude and/or a phase angle of the signals so as to determine a relative magnitude and/or relative phase angle by subtraction in order to detect turn-to-turn faults. Relative differences in the at least two signals are recorded. Also a device for performing the method. | 10-20-2011 |
| 20110253470 | DRIVE UNIT FOR A VEHICLE FOR USE AS A ROBOT IN PIPE SYSTEMS, CAVITIES OR THE LIKE AND A VEHICLE HAVING SAME - A drive unit for a vehicle is provided for use as a robot in pipe systems, cavities or the like. The drive unit includes at least one ring-like outer wheel and at least one driven magnetic wheel. The outer and the magnetic wheels have axes parallel to each other and are arranged eccentrically to one another, and engage one another such that when rotating relative to the outer wheel, the magnetic wheel delineates with its wheel axis a concentric circle lying within the outer wheel. In such a drive unit, stronger magnetic adhesion is enabled by the outer and magnetic wheels being arranged one behind the other in an axial direction. The engagement between the outer and magnetic wheels is effected by a circular, concentric disk connected securely against rotation to the magnetic wheel and rolls with its outer peripheral surface on the inner peripheral surface of the outer wheel. | 10-20-2011 |
| 20110243803 | HOT SOLIDS GASIFIER WITH CO2 REMOVAL AND HYDROGEN PRODUCTION - A gasifier | 10-06-2011 |
| 20110243756 | METHOD FOR PRODUCING A BLADE BY CASTING AND BLADE FOR A GAS TURBINE - A method is provided for producing a blade, by casting, for a gas turbine. The blade includes an elongate airfoil which extends in a blade longitudinal direction, merges into a blade root at the lower end, has a shroud segment at the blade tip and is pervaded by a single cooling air channel running in the blade longitudinal direction from the blade root to the blade tip. The method includes, during the casting of the blade, the blade material being fed exclusively from the blade root into the mold provided therefor, and the cooling air channel is formed during the casting of the blade by using a single core body, which is provided, at the blade tip, with a local casting cross section increasing element. | 10-06-2011 |
| 20110243755 | COOLED BLADE FOR A GAS TURBINE, METHOD FOR PRODUCING SUCH A BLADE, AND GAS TURBINE HAVING SUCH A BLADE - A blade for a gas turbine includes an airfoil extending in radial direction of the turbine or longitudinal direction of the blade, respectively, between a platform and a blade tip. The airfoil is bordered across the airfoil by a leading edge and a trailing edge and has a suction side and a pressure side. At the trailing edge a first cooling passage runs parallel to the trailing edge from the platform to the blade tip in the interior of the airfoil. The cooling passage is supplied with a cooling air flow from the platform side, and from which cooling air is discharged through a plurality of cooling holes arranged all over the blade. For such a blade the cooling is optimized by providing a first cooling passage, the passage area of which is tapered in radial direction by between 35% and 59%. | 10-06-2011 |
| 20110239961 | ONCE-THROUGH VERTICAL EVAPORATORS FOR WIDE RANGE OF OPERATING TEMPERATURES - An evaporator for steam generation is presented. The evaporator includes a plurality of primary evaporator stages and a secondary evaporator stage. Each primary stage includes one or more primary arrays of heat transfer tubes, an outlet manifold coupled to the arrays, and a downcomer coupled to the manifold. Each of the primary arrays has an inlet for receiving a fluid and is arranged transverse to a flow of gas through the evaporator. The gas heats the fluid flowing through the arrays to form a two phase flow. The outlet manifold receives the two phase flow from the arrays and the downcomer distributes the flow as a component of a primary stage flow. One or more of the plurality of primary evaporator stages selectively form the primary stage flow from respective components of the two phase flow, and provide the primary stage flow to inlets of the secondary evaporator stage. | 10-06-2011 |
| 20110239782 | METHOD AND SYSTEM FOR MEASUREMENT OF A FLOW RATE OF A FLUID - A system for measuring a flow rate of a fluid through a plurality of tubes sharing a common flow orifice, the system includes an ultrasonic transducer having a plurality of sensors in communication with a plurality of tubes sharing a common flow orifice. The system includes an electronic module coupled to the ultrasonic transducer, the electronic module connecting selected sensors to a flow rate analyzer for determining a flow rate of fluid through the plurality of tubes on which the sensors are in communication with. | 10-06-2011 |
| 20110236223 | BLADE FOR A GAS TURBINE - A blade for a gas turbine includes an airfoil extending in a longitudinal direction and extending transversely to the longitudinal direction between a leading edge and a trailing edge. The airfoil has a pressure side, a suction side, and a slot-like cooling medium outlet extending along the trailing edge. The cooling medium outlet is configured to discharge cooling medium supplied from an inner space of the blade. A platform extends transversely to the longitudinal direction. An end of the airfoil merges into an underside of the platform and has a transition from the airfoil to the platform at the trailing edge of the airfoil that increases in thickness in a direction toward the underside of the platform. The cooling medium outlet extends into the platform so as to reduce an operating temperature in a region of the transition from the blade airfoil to the platform. | 09-29-2011 |
| 20110236222 | BLADE FOR A GAS TURBINE AND CASTING TECHNIQUE METHOD FOR PRODUCING SAME - A blade for a gas turbine has a leading edge and a trailing edge, and an interior cavity, which is delimited by internal surfaces, for guiding cooling air therethrough. A multiplicity of turbulators or pins, which are formed on the wall, are arranged in a distributed manner in the region of the trailing edge and project from the internal surfaces into the cavity, to improve the transfer of heat between the wall of the blade and the cooling air. An improvement of the internal cooling is achieved by the turbulators or pins extending into the cavity in a direction which can be freely selected within an angular range. | 09-29-2011 |
| 20110234181 | DEVICE AND METHOD FOR MONITORING AND/OR ANALYZING ROTORS OF ELECTRIC MACHINES IN OPERATION - A method is provided for monitoring and/or analysis of electrical machines during operation. An electrical machine has at least one generator with a shaft, an exciter system and drive device that drives the shaft. In this case, a first signal, which describes a voltage across a rotor winding, and a second signal, which describes a current flowing through the rotor winding, are measured simultaneously. The two signals are supplied to an analysis unit. The signals are split into individual frequency components in the analysis unit. The impedance of the rotor winding is then determined in order to identify fault states in the electrical machine. | 09-29-2011 |
| 20110232295 | METHOD FOR OPERATION OF AN INTEGRATED SOLAR COMBINED-CYCLE POWER STATION, AND A SOLAR COMBINED-CYCLE POWER STATION FOR CARRYING OUT THIS METHOD - A method is provided for operation of an integrated solar combined-cycle power station. The power station includes a water/steam circuit having a steam turbine and a heat recovery steam generator through which hot exhaust gases from a gas turbine flow. The water/steam circuit is additionally supplied with heat from a solar array. In such a method, an optimum cost-benefit relationship is achieved in that the water/steam circuit is designed only for the full load on the gas turbine, and in that, when feeding additional power from the solar array into the water/steam circuit, the load on the gas turbine is reduced, on the basis of the power additionally fed in from the solar array, to such an extent that the total output power of the integrated solar combined-cycle power station remains substantially constant. | 09-29-2011 |
| 20110223083 | SYSTEM AND METHOD FOR GENERATING A CARBON DIOXIDE STREAM - A flue gas stream processing system includes a fuel reactor for combusting a fuel to generate a flue gas stream including water vapor, carbon monoxide and carbon dioxide. The system includes an oxidation catalyst downstream of the fuel reactor, the oxidation catalyst configured to receive the flue gas stream and oxidize the carbon monoxide to form a carbon dioxide rich flue gas stream, and a processing unit to liquefy carbon dioxide in the carbon dioxide rich flue gas stream and generate an exhaust gas. | 09-15-2011 |
| 20110223036 | BLADE FOR A GAS TURBINE - The blade for a gas turbine includes a blade airfoil having a leading edge and a trailing edge and extending in the blade longitudinal direction up to a blade tip, and at the blade tip the blade airfoil merges into a shroud segment, wherein on the shroud segment a first rib, projecting upwards, is arranged in the flow direction, extending transversely to the flow direction, and upstream of the first rib, in the region of the leading edge of the blade airfoil, a winglet is formed on the shroud segment for guiding of the hot gas flow in this region. With such a blade, a longer service life is achieved by provision being made for direct cooling of the winglet. | 09-15-2011 |
| 20110220614 | PORTABLE EDM SYSTEM FOR MAKING CALIBRATION STANDARDS - A portable EDM device and system thereof for producing calibration reflectors on a pipe includes a base mountable on the pipe, a motor mounted on the base, a cutting tool operably connected to the motor, an electrode operably connected to the cutting tool, a power source mounted on the base and operably connected to the electrode and operably connectable to the pipe, and a source of dielectric fluid mounted on the base. The power source is configured to electrically discharge a voltage from the electrode to the pipe to remove material from the pipe. The source of dielectric fluid is in fluid communication with the pipe to remove the material removed from the pipe. | 09-15-2011 |
| 20110210705 | METHOD FOR REGULATING THE REACTIVE POWER GENERATED OR ABSORBED BY A SYNCHRONOUS ELECTRIC GENERATOR AND SYNCHRONOUS ELECTRIC GENERATOR - A method for regulating the reactive power generated or absorbed by a synchronous electric generator includes regulating a quantity of coils disposed in line with a stator winding. Additionally, a generator operating point of the generator is regulated. | 09-01-2011 |
| 20110203456 | WET SCRUBBER AND A METHOD OF CLEANING A PROCESS GAS - A wet scrubber ( | 08-25-2011 |
| 20110203280 | METHOD FOR OPERATING A POWER PLANT AND POWER PLANT - A method for operating a power plant is disclosed. The power plant includes a power machine and a flue gas flow path following downstream of the power machine. A flue gas flow path is scavenged with fresh air before the flue gas flow path is acted upon with flue gas. To carry out the scavenging operation, air is extracted from a pressure accumulator and the air is introduced into the flue gas flow path downstream of the power machine. The power machine can be an exhaust gas heat exchanger. | 08-25-2011 |
| 20110203274 | STEAM TURBINE PLANT - An exemplary steam plant having a steam circuit which includes a superheater defining a boundary between a superheated steam region and an unsuperheated steam region. The steam circuit includes a branch, from a superheated steam region of the steam circuit, with a branch valve and a steam desuperheater upstream of the branch valve. The desuperheater provides cooling to the branch during flow mode operation of the branch. During a no flow mode, a first preheat line and a second preheat line provide the cooling by supplying unsuperheated steam to the branch and directing this flow through to a lower pressure region of the steam circuit. | 08-25-2011 |
| 20110203250 | COMBUSTION DEVICE FOR A GAS TURBINE - A combustion device for a gas turbine includes an interior portion, an inner wall having a plurality of first passages and an outer wall having a plurality of second passages configured to cool the inner wall, each of the plurality of second passages having an outlet opening into a third passage. An intermediate layer is disposed between the inner wall and the outer wall and defines a plurality of chambers, each chamber forming a Helmholtz damper and being connected to the interior portion by at least one of the plurality of first passages and being connected to at least one of the plurality of second passages by at least one of the plurality of third passages | 08-25-2011 |
| 20110197593 | GAS TURBINE AND METHOD FOR ITS OPERATION - A gas turbine and method are disclosed by which the gas turbine can be safely operated at nominal speed with reduced margin to a surge limit of a compressor. The gas turbine, via a directly driven generator which generates alternating current with an operating frequency and which is connected in a frequency-coupled manner to an electricity grid, can deliver electric power to this grid. In the case of an underfrequency event the compressor of the gas turbine is unloaded by controlled, fast closing of the variable compressor guide vanes (VGV) and as a result maintains a sufficient margin to the surge limit of the compressor. | 08-18-2011 |
| 20110194972 | NICKEL-BASE SUPERALLOY WITH IMPROVED DEGRADATION BEHAVIOR - A nickel-base superalloy with improved degradation behavior consists essentially of the following chemical composition (details in % by weight): 7.7-8.3 Cr, 5.0-5.25 Co, 2.0-2.1 Mo, 7.8-8.3 W, 5.8-6.1 Ta, 4.9-5.1 Al, 1.3-1.4 Ti, 0.1-0.6 Pt, 0.1-0.5 Nb, 0.11-0.15 Si, 0.11-0.15 Hf, 200-750 ppm C, 50-400 ppm B, and the remainder Ni and production-related impurities. | 08-11-2011 |
| 20110193018 | ROTARY BOTTOM ASH REGENERATION SYSTEM - A rotary bottom ash regenerating (RBAR) system [ | 08-11-2011 |
| 20110190939 | CONTROL AND OPTIMIZATION SYSTEM AND METHOD FOR CHEMICAL LOOPING PROCESSES - A control system for optimizing a chemical loop system includes one or more sensors for measuring one or more parameters in a chemical loop. The sensors are disposed on or in a conduit positioned in the chemical loop. The sensors generate one or more data signals representative of an amount of solids in the conduit. The control system includes a data acquisition system in communication with the sensors and a controller in communication with the data acquisition system. The data acquisition system receives the data signals and the controller generates the control signals. The controller is in communication with one or more valves positioned in the chemical loop. The valves are configured to regulate a flow of the solids through the chemical loop. | 08-04-2011 |
| 20110187545 | METHOD AND SYSTEM OF MONITORING MASS IN A PULVERIZED COAL FIRED FURNACE | 08-04-2011 |
| 20110179796 | HELMHOLTZ DAMPER FOR A COMBUSTOR OF A GAS TURBINE AND A METHOD FOR INSTALLING THE HELMHOLTZ DAMPER - A Helmholtz damper for a combustor of a gas turbine includes first and second damping volumes. The combustor has a combustion chamber disposed in a housing and closed off by a front plate at which a plurality of burners are exchangeably fastened. The burners are supplied with fuel via fuel lances which extend from outside the housing through a bushing of the housing to the associated burner. The first damping volume has a first end and a second end, the first end of the first damping volume being configured to attach a connecting passage extending to a front panel such that the Helmholtz damper is connectable with the front plate of the combustion chamber in place of one of the burners. The second damping volume has a first end and a second end and is arranged in series with the first damping volume along an axis of the Helmholtz damper with the first end of the second damping volume being detachably connected to the second end of the first damping volume so as to form a combined larger damping volume. The second end of the second damping volume is configured to attach a connecting tube extending from the second damping volume and through the bushing in place of a respective one of the fuel lances. | 07-28-2011 |
| 20110174565 | VEHICLE AND METHOD FOR THE INDEPENDENT INSPECTION OF HARD-TO-REACH INNER SPACES - A vehicle is provided for the independent inspection of hard-to-reach inner spaces which are bounded by ferromagnetic inner walls, especially in large cast parts, such as steam chests of a steam turbine. The vehicle includes at least two wheels which are rotatable around a common axis, are at a distance from each other in the axial direction, and can be driven independently of each other. With such a vehicle, the entire inner space can be inspected if the vehicle has adherence elements which hold the vehicle against the gravity force with the wheels on the respective inner wall. | 07-21-2011 |
| 20110173981 | UTILIZATION OF LOW GRADE HEAT IN A REFRIGERATION CYCLE - A system for reducing the power required to cool a combustion gas for cleaning and a method for performing the same are disclosed. The system includes an expander for producing power. Energy in the form of heat is transferred from the combustion gas to a working fluid. The working fluid drives the expander to generate at least a portion of the power required for performing to drive a compressor in a refrigeration system. After the combustion gas transfers energy the combustion gas is cooled with the refrigeration system. In some embodiments the expander and the compressor are arranged along a common shaft. | 07-21-2011 |
| 20110171039 | BLADE ARRANGEMENT OF A GAS TURBINE - A blade arrangement of a gas turbine, with at least one blade which in the radial direction projects into a hot gas passage arranged concentrically to an axis, and terminates in a blade tip which with a clearance lies opposite a heat shield which delimits the hot gas passage. The blade and the heat shield are movable in relation to each other in the circumferential direction, and the blade tip and the heat shield are covered with coatings, which enable a directed cutting of the blade tip into the heat shield. By such a blade arrangement, a reduction of the clearance as a result of cutting in is simply achieved by the heat shield having a porous thermal barrier coating as an outer, abradable coating, and by the blade tip being provided with a homogenous, metallic cover coating. | 07-14-2011 |
| 20110171013 | SHROUD SEAL SEGMENTS ARRANGEMENT IN A GAS TURBINE - A gas turbine is provided that includes a rotor which is rotatable around an axis and equipped with rotor blades, and which is concentrically enclosed at a distance by a casing, which is equipped with stator blades, forming an annular hot gas passage. Rings with stator blades and rotor blades are arranged in a manner alternating in the axial direction. Between adjacent stator blades, heat shield segments are arranged, which delimit the hot gas passage on the outside in a region of the rotor blades and are cooled by impingement cooling where a cooling medium from an outer annular cavity flows into the heat shield segment. | 07-14-2011 |
| 20110168020 | WASH WATER METHOD AND SYSTEM FOR A CARBON DIOXIDE CAPTURE PROCESS - A system and method for recovering a solvent from a decarbonated flue gas in an absorption column, the decarbonated flue gas having had carbon dioxide absorbed and removed by vapor-liquid contact with a carbon dioxide absorbing solution containing the solvent. The system includes an emission control section configured to bring a water stream substantially free of the solvent into contact with the decarbonated flue gas to recover the solvent from the decarbonated flue gas and to form a solvent containing wash water and a reduced solvent containing flue gas and a flue gas cooling section configured to bring cooled wash water into contact with the reduced solvent containing flue gas to cool the reduced solvent containing flue gas and condense water from the decarbonated flue gas thereby forming a cooled flue gas and used wash water. | 07-14-2011 |
| 20110164970 | Stator blade for a turbomachine, especially a stream turbine - The invention relates to a stator blade ( | 07-07-2011 |
| 20110163607 | METHOD FOR SYNCHRONIZING AN ELECTRIC MACHINE WITH AN ELECTRIC GRID AND ARRANGEMENT OF AN ELECTRIC MACHINE AND AN ELECTRIC GRID - A method is provided for synchronizing an electric machine with an electric grid. The method includes synchronizing the frequency of a generator with a frequency of the grid, and regulating the voltage of the generator towards the voltage of the grid, by connecting the generator to the grid when the voltage of the generator reaches a first voltage value lower than the grid voltage. The present disclosure also provides arrangements of an electric generator and an electric grid. | 07-07-2011 |
| 20110160979 | METHOD OF ESTIMATING THE MAXIMUM POWER GENERATION CAPACITY AND FOR CONTROLLING A SPECIFIED POWER RESERVE OF A SINGLE CYCLE OR COMBINED CYCLE GAS TURBINE POWER PLANT, AND A POWER GENERATING SYSTEM FOR USE WITH SAID METHOD - An estimation unit can estimate, on a real-time basis, a maximum power generation capacity of a single cycle or combined cycle gas turbine power plant. For example, the actual power output and the maximum power generation capacity can be calculated relying on a mathematical process model. Subsequently, the calculated actual power output can be compared with the measured power output yielding a model-estimation error. Based on the model-estimation error, a correction signal can be deduced, to correct the calculated maximum power generation capacity. A controller can maintain a specified power reserve. The controller can use an estimate of the maximum power generation capacity as a reference, subtract a load offset, and apply the resulting signal as upper limit of the load set-point. | 06-30-2011 |
| 20110155347 | ECONOMIZER WATER RECIRCULATION SYSTEM FOR BOILER EXIT GAS TEMPERATURE CONTROL IN SUPERCRITICAL PRESSURE BOILERS - A fluid recirculation system includes an arrangement of a flow control valve located to receive a flow of fluid from an inlet. The system further comprises an economizer inlet mixing device located to receive the flow of hotter fluid from the arrangement of the flow control valve and from a cooler feedwater stream. An economizer inlet mixing device located upstream of an economizer in a supercritical pressure boiler includes a sparger assembly through which a flow of fluid from the waterwall outlet is received, an inlet through which a flow of fluid from a feed stream is received, and a wave breaker assembly through which an outlet stream from the economizer inlet mixing device is directed. A method of increasing and controlling the temperature of a flue gas exiting an economizer in a supercritical pressure boiler includes receiving at least a flow of fluid from a fluid stream from a furnace waterwall outlet, combining at least a portion of the received flow of fluid with a feedwater stream, and directing the combined received flow of fluid and feedwater stream to an economizer inlet to decrease the economizer heat absorption. | 06-30-2011 |
| 20110150733 | DESULFURIZATION OF, AND REMOVAL OF CARBON DIOXIDE FROM, GAS MIXTURES - A method of heating a used absorption liquid resulting from a carbon dioxide absorption stage in which a CO | 06-23-2011 |
| 20110150660 | AIRFOIL FOR A COMPRESSOR BLADE - The present disclosure provides an improved first stage airfoil for a compressor blade having a unique chord length (CD), stagger angle (γ) and camber angle (Δβ). The stagger angle (γ) and camber angle (Δβ) provide improved aerodynamics while the chord length (CD) provides for reduced airfoil weight. | 06-23-2011 |
| 20110150659 | AIRFOIL FOR A COMPRESSOR BLADE - The present disclosure provides an improved second stage airfoil for a compressor blade having a unique chord length (CD), a stagger angle (γ), and camber angle (Δβ). The stagger angle (γ) and camber angle (Δβ) provide improved aerodynamics while the chord length (CD) provides for reduced airfoil weight. | 06-23-2011 |
| 20110146598 | CUFF FOR BOILER TUBE ASSEMBLY AND METHOD OF MANUFACTURE - A system for retaining boiler tubes in an array includes a bracket having a contoured surface defining at least one channel, the channel being semi-cylindrical and defined by an elongated cross section having a rounded portion and two elongated legs extending therefrom to define a substantially U-shaped cross section, and a planar section located at a terminus of each leg. The system also comprises a plate connectable to at least one planar section of the bracket. A method of manufacturing a cuff for a boiler tube assembly includes bending a bracket having at least one channel therein, the channel being configured to receive a boiler tube of the boiler tube assembly; and machining a plate, the plate being configured and sized to be positioned over the channel. | 06-23-2011 |
| 20110146546 | METHOD FOR BURNING REFINING RESIDUES - The method of the invention for combustion of residues from refining petroleum in a boiler comprising a hearth and injectors is characterized in that cooled gas containing oxygen is injected into the hearth in the hottest region of said hearth. Injection into the very hot region of the hearth cracks tar or aromatic polycyclic hydrocarbons and converts them into basic compounds that are easily combustible and therefore less pollutant. | 06-23-2011 |
| 20110146489 | AMMONIA REMOVAL, FOLLOWING REMOVAL OF CO2, FROM A GAS STREAM - A process for removal of CO | 06-23-2011 |
| 20110135497 | TURBINE BLADE - A blade is provided and includes a platform and a root configured to be connected to a blade carrier. Airfoil portions extend from opposite sides of the platform. Each airfoil portion defines an operating surface being the surface facing the other airfoil portion. An operating surface of one of the airfoil portions defines a suction side and the other operating surface of the other airfoil portion defines a pressure side. | 06-09-2011 |
| 20110135480 | STEAM TURBINE ROTOR - A joined rotor that includes a primary join and a locking device and a method for joining thereof is disclosed. The primary join includes a threaded boss that is inserted in a tapped cavity formed in an adjacent rotor section. The primary join is locked, so as to prevent unscrewing, by at least one locking member that is located partially in both first and second rotor sections. This arrangement enables the join to be locked at a desired torque point. | 06-09-2011 |
| 20110135451 | GAS TURBINE - A gas turbine includes a turbine section; an annular combustor disposed upstream of the turbine section and configured to discharge a hot gas flow on an outlet side to the turbine section; an outer shell delimiting the combustor and splittable at a parting plane; a plenum enclosing the outer shell; a rotor; a turbine vane carrier encompassing the rotor; a plurality of stator vanes disposed on the vane carrier, and at least two sealing segments forming a ring, each of the at least two sealing segments having an inner edge and a head and a foot section and being movably mounted on the inner edge by the foot section to the outer shell and by the head section to the turbine vane carrier so as to mechanically connect the combustor to the turbine vane carrier. | 06-09-2011 |
| 20110131993 | STEAM POWER PLANT WITH HEAT RESERVOIR AND METHOD FOR OPERATING A STEAM POWER PLANT - A steam power plant is suggested having, parallel to the preheater passage (VW | 06-09-2011 |
| 20110131796 | GENERATOR WITH HIGH PHASE ORDER - A method for re-powering a star-connected stator having a plurality of parallel stator slots, wherein a plurality of stator winding bars having external winding connections are disposed in stator slots includes bridging the external winding connections so as to connect the stator winding bars in series and to form a polygonal stator capable of producing a polyphase alternating current. | 06-09-2011 |
| 20110123313 | AXIAL FLOW STEAM TURBINE - An exemplary axial flow steam turbine is disclosed which includes a motor, a turbine casing and at least first and second turbine stages, with the second turbine stage being located adjacent to and downstream from the first turbine stage. A radially outer static diaphragm ring of the second turbine stage includes an annular axial extension extending in an upstream axial direction and carrying a circumferential tip sealing device which cooperates with shrouds of a circumferential row of moving blades of the first turbine stage. An upstream end of the annular axial extension is axially spaced from a radially outer static diaphragm ring of the first turbine stage such that a circumferential passage is defined between the upstream end of the annular axial extension and the radially outer static diaphragm ring of the first turbine stage. Solid particles are diverted from steam flow by a circumferential passage during operation. | 05-26-2011 |
| 20110120309 | ADVANCED INTERCOOLING AND RECYCLING IN CO2 ABSORPTION - The present invention relates processes of removal of acidic gases from a gas stream, comprising the steps of
| 05-26-2011 |
| 20110120308 | SINGLE ABSORBER VESSEL TO CAPTURE CO2 - A system for removing carbon dioxide from a flue gas stream is provided, the system comprising an absorber vessel configured to receive a flue gas stream, the absorber vessel comprising a first absorption stage configured to receive the flue gas stream and contact it with a first ionic solution, a second absorption stage configured to receive flue gas which has passed the first absorption stage and contact it with a second ionic solution, a first sump vessel, and a second sump vessel. Furthermore, a method for removing CO | 05-26-2011 |
| 20110120128 | METHOD OF CONTROLLING A POWER PLANT - The present invention relates to a method of controlling a power plant, which power plant comprises: a boiler being adapted for combusting an organic fuel and for generating steam and a process gas comprising carbon dioxide; a steam system being; and a carbon dioxide capture system being adapted to remove at least a portion of the carbon dioxide from the process gas by contacting a carbon dioxide absorbent solution with the process gas, the method comprising: forwarding a portion of the steam produced by the power plant boiler to a regenerator of the carbon dioxide capture system; regenerating the absorbent solution in said regenerator through heating of said carbon dioxide absorbent solution by means of the forwarded steam; and automatically controlling the operation of the carbon capture system by means of at least one automatic controller. The invention also relates to a power plant including a carbon dioxide capture system. | 05-26-2011 |
| 20110117507 | PIVOT PIN FOR FURNACE SIDE REMOVAL - Disclosed herein is a novel nozzle tip assembly | 05-19-2011 |
| 20110117458 | FUEL CELL SYSTEM AND OPERATING METHOD - A fuel cell system comprises a fuel cell main body containing a fuel cell having an anode side at which fuel is reacted, exhaust products arising at the anode side of the fuel cell as a result of the reaction at the anode side. A recirculation passage is located inside the fuel cell main body and recirculates a proportion of the exhaust products directly to the anode side of the fuel cell for reaction at the anode side. The recirculation passage may include an ejector arrangement for mixing fresh fuel with the recirculated exhaust products and may also include a reforming catalyst for partially reforming the mixture in the recirculation passage. | 05-19-2011 |
| 20110113790 | THERMAL MACHINE - A thermal machine including a wall defining a hot gas duct for transferring a hot gas stream and a cooling jacket disposed at a distance from the wall on an outside of the hot gas duct so as to define a cooling duct with an inlet and an outlet. The cooling duct is configured to conduct a cooling medium along an external face of the wall from the inlet to an outlet in a direction counter to a flow of hot gas in the hot gas duct. An impingement cooling plate is disposed at the inlet of the cooling duct and includes cooling baffle holes configured such that cooling medium entering the cooling duct through the cooling baffle holes flows in a direction perpendicular to the wall. The impingement cooling plate is positioned such that an inflow-side edge sealingly abuts the wall of the hot gas duct so as to reduce a transverse flow of the cooling medium through the cooling duct. | 05-19-2011 |
| 20110113785 | THERMAL MACHINE - A thermal machine is provided, in particular a gas turbine, which includes an annular combustion chamber which is bounded on the outside by an outer shell and an inner shell. The outer shell and the inner shell are each split on a separating plane into an upper half and a lower half, which are mechanically interlocked by welding one to the other on the separating plane. Increased mechanical robustness and a longer life of the combustion chamber are achieved in that an additional mechanical interlock is provided on the separating planes in order to absorb tensile and shear forces acting on the separating planes. | 05-19-2011 |
| 20110110785 | ROTOR FOR AN AXIAL-THROUGHFLOW TURBOMACHINE AND MOVING BLADE FOR SUCH A ROTOR - A rotor is provided for an axial-throughflow turbo machine, which carries a plurality of moving blades which are each pushed with a blade root into a rotor groove extending about the axis and are held. The blade root includes a hammer root with a hammerhead and is supported on radial stop faces of the rotor groove which lie further outward in the radial direction, against centrifugal forces acting on the moving blades, and are supported on axial stop faces lying further inward in the radial direction, against axial forces which act on the moving blade. The rotor groove has at its bottom, to reduce thermal stresses, an axially and radially widened bottom region with a continuously curved cross-sectional contour. In such a rotor, an advantageous adaptation of the blading is achieved by the blade root of the moving blades being adapted to the widened bottom region in the radial direction. | 05-12-2011 |
| 20110110761 | GAS TURBINE HAVING AN IMPROVED COOLING ARCHITECTURE - A thermal machine includes a hot gas channel; a shell bounding the hot gas channel; a cooling shirt surrounding the shell; and a cooling channel disposed between the shell and the cooling shirt and configured to convection cool the hot gas channel with a cooling medium, wherein the cooling shirt includes at least one local divergence in the guidance of the cooling medium so as to compensate for non-uniformities in at least one of a thermal load on the shell and a flow of the cooling medium in the cooling channel. | 05-12-2011 |
| 20110109186 | CONDUCTOR BAR FOR THE STATOR OF A GENERATOR AND METHOD FOR ITS PRODUCTION - A conductor bar for a stator of a generator includes a plurality of internal conductor elements; an insulation wound around the plurality of internal conductor elements so as to externally enclose the plurality of internal conductor elements, the insulation including impregnated glass/mica bands; and at least one interlayer disposed between the insulation and the plurality of internal conductor elements so as to improve a mechanical connection between the plurality of internal conductor elements and the insulation. | 05-12-2011 |
| 20110106717 | QUALITY CONTROL RECORD AND DATA PROCESSING SYSTEM FOR CREATING AND MAINTAINING SAME - A system and method are presented for creating and maintaining quality control records. The system includes a plurality of client devices. Each client device captures information, data and decisions associated with raw material, components and assemblies of components. The information, data and decisions document operations and operating conditions at a plurality of stages in a life cycle of the raw materials, components and assemblies. The system includes a communication network and one or more servers operatively coupled to the client devices over the network. The servers create quality control records including the information, data and decisions for the materials, components and assemblies. The system includes one or more data stores that store the quality control records. The information, data and decisions includes measurements and readings taken by the input-output devices and decisions made at the stages and that document properties of the raw materials, components and assemblies. | 05-05-2011 |
| 20110106460 | AUTOMATED COMPONENT VERIFICATION SYSTEM - A system and method are presented for qualifying a component. The system includes a receiving station, a control section, a plurality of test/inspection stations, a data storage section and a marking station. The receiving station receives a component. The control section includes a processor. The plurality of test/inspection stations each include equipment to measure one or more of physical, compositional and resistance properties of the component. The processor and the equipment cooperate to compare the measured properties to predefined properties for acceptance of the component, and to determine conformance between the measured properties and the predefined properties to qualify the component for use. The data storage section includes data store that receives and stores the predefined properties, the unique identifier, and the measured properties of the component. The marking station includes marking equipment to mark the component with the unique identifier. | 05-05-2011 |
| 20110104015 | APC PROCESS PARAMETER ESTIMATION - A virtual analyzer is provided to estimate either an attribute of a reactant applied during performance of, or an amount of a reactant exhausted by, a process having multiple process parameters (MPPs) that is performed to control an amount of a pollutant emitted into the air. The virtual analyzer includes an interface which receives signals corresponding to attributes of the MPPs. If the process is a wet flue gas desulfurization (WFGD) process, the signals include a signal corresponding to a measured pH level of the applied reactant. If the process is a selective catalytic reduction (SCR) process, the signals include a signal corresponding to a measured amount of the reactant exhausted by the process. | 05-05-2011 |
| 20110103970 | STEAM TURBINE WITH RELIEF GROOVE ON THE ROTOR - A steam turbine is provided having a relief groove which is arranged in the region of the equalizing piston and extends in the circumferential direction of the rotor. The relief groove, with regard to an inlet passage, is arranged in the axial upstream direction so that it is arranged on the rotor outside a region in which the steam flow enters the bladed flow path via the inlet passage. The relief groove, with regard to the first blade row, is arranged in a region in which the greatest thermal stresses can arise in the rotor. As an option, the relief groove has a cover for reducing vortex flows, and also devices for reducing heating of the groove or devices for active cooling. The steam turbine allows an increased number of risk-free running up and running down operations of the steam turbine with minimum detriment to the turbine performance. | 05-05-2011 |
| 20110103968 | WEAR-RESISTANT AND OXIDATION-RESISTANT TURBINE BLADE - A wear- and oxidation-resistant turbine blade and a method for producing the blade are provided. At least portions of the surface of the main blade section are provided with at least one first protective coating comprised of oxidation-resistant material, the first, oxidation-resistant coating is a metallic coating, which is optionally covered by a ceramic thermal barrier coating. The metallic first protective coating is arranged at least at the inner and outer crown edge of the blade tip, but not at the radially outer blade tip. The radially outer blade tip of the turbine blade is comprised of a second, single- or multi-layer wear- and oxidation-resistant protective coating, which is built up by laser metal forming and is comprised of abrasive and binder materials. The second protective coating on the blade tip overlaps along the outer and/or inner crown edge at least partially with the first, metallic protective coating arranged there. | 05-05-2011 |
| 20110103967 | ABRASIVE SINGLE-CRYSTAL TURBINE BLADE - A turbine blade for a turbine rotor, is provided having a single-crystal basic body which has a blade tip and extends in the radial direction. The turbine blade includes at least one oxidation-resistant intermediate coating, which is applied by laser metal forming and is epitaxially bonded to the basic body, is arranged on the radially outer blade tip, and in that an at least single-layer, wear-resistant and oxidation-resistant coating, which is applied by laser metal forming and consists of oxidation-resistant binder material and abrasive particles embedded therein, is arranged on at least certain regions of said epitaxial intermediate coating. | 05-05-2011 |
| 20110103947 | GAS TURBINE EXHAUST STRUT REFURBISHMENT - A gas turbine exhaust strut installed in an exhaust case of a gas turbine is disclosed which includes a trailing portion configured with an inner surface for mounting to an inner annular member of the exhaust case and an outer surface for mounting to an outer annular member of the exhaust case, a block attached to the trailing portion, an angled piece attached to the block and configured with a surface on a pressure side of the strut angled with respect to a surface of the trailing portion on the pressure side of the strut, and a transition piece attached to the block and configured with a surface on the pressure side of the strut for smoothing the transition between the height of the block on the pressure side of the strut and the height of the trailing portion on the pressure side of the strut. A method of refurbishing an exhaust strut installed in an exhaust case of gas turbine while retaining at least a portion of the strut in the exhaust case is also disclosed. An exemplary method includes removing a leading edge portion from a trailing portion of the strut, and attaching a replacement leading edge portion to the trailing portion of the strut. | 05-05-2011 |
| 20110103932 | STATOR BLADE FOR A GAS TURBINE AND GAS TURBINE HAVING SAME - A stator blade for a gas turbine with sequential combustion, has a blade airfoil which extends in the radial direction between a blade tip and a shroud, with cooling passages extending inside the blade airfoil, through which a cooling medium can flow for cooling the blade and can then discharge from the stator blade into the hot gas flow flowing through the turbine. The blade airfoil has a sharply curved shape in space in the radial direction, and three cooling passages, which extend in the radial direction, arranged inside the blade airfoil in series in the hot gas flow direction and are interconnected by deflection regions, which are arranged at ends of the blade airfoil, so that the cooling medium flows through the cooling passages one after the other, with change of direction. The cooling passages follow the curvature of the blade airfoil in space in the radial direction. | 05-05-2011 |
| 20110100961 | WELDING PROCESS FOR PRODUCING ROTATING TURBOMACHINERY - A method for welding dissimilar metals involved selecting a steel having approximately 1-3 weight % chromium (Cr) content and a first coefficient of thermal expansion at a predetermined first temperature for a first part [ | 05-05-2011 |
| 20110100216 | GAS STREAM PROCESSING - A power generation plant ( | 05-05-2011 |
| 20110097201 | STEAM TURBINE CASING SYSTEM - The disclosure relates to a steam turbine outer casing that can be at least partially cast out of a first material and has a plurality of support regions adapted to support an inner casing. The outer casing can be at least one support region that has a metal insert, made of a second material, with a flaring portion for retaining the metal insert in the casting of the outer casing. The second material has a greater hot strength than the first material. The support region can include a guide for limiting the movement of the inner casing in the outer casing. | 04-28-2011 |
| 20110085955 | SYSTEM AND METHOD FOR REDUCING NO2 POISONING | 04-14-2011 |
| 20110085915 | BLADE FOR A GAS TURBINE - A blade for a gas turbine includes a leading edge running in a longitudinal direction substantially radially to an axis of the turbine; a trailing edge running in the longitudinal direction; a blade body disposed between the leading edge and the trailing edge so as to define a pressure side and a suction side; an exit slot disposed in the blade body in an area of the trailing edge and running in the longitudinal direction and configured to discharge a cooling medium from an interior of the blade body; and a row of first and second control elements disposed in the exit slot in a distributed manner in the longitudinal direction and configured to control a mass flow of the cooling medium exiting through the exit slot, the first control elements having a first configuration and the second control elements having a second configuration different from the first configuration. | 04-14-2011 |
| 20110085894 | GAS TURBINE WITH A STATOR BLADE - A gas turbine with a stator blade is disclosed. The stator blade is fastened on a blade carrier and includes a blade airfoil which extends inwards in the radial direction from an outer platform into a hot gas passage. A cooling medium can flow through an interior of the blade airfoil, such as cooling air, which flows through an access in the blade carrier into a first plenum which is arranged above the outer platform, and from there, via an inlet which is provided in the outer platform, flows into the interior of the blade airfoil. | 04-14-2011 |
| 20110085887 | HIGH TEMPERATURE RADIALLY FED AXIAL STEAM TURBINE - The disclosure relates to a radially fed axial steam turbine with a cold inlet duct, axially displaced from a hot inlet duct such that is it further away from a first blade row than the hot inlet duct. The cold inlet duct receives a cold steam from a cold inlet spiral and directs it into the hot inlet duct in such a way that a boundary layer of cold steam is formed over the rotor circumferential surface between the outlet end of the cold inlet duct and the blade and vane rows. The rotor circumferential surface is also adapted to promote and maintain the boundary layer. In this way, a maximum temperature to which the rotor is exposed can be reduced. | 04-14-2011 |
| 20110084671 | METHOD FOR MONITORING AN ELECTRODYNAMIC MACHINE - A method for monitoring an electrodynamic machine a stator and a rotor arrangement mounted along a rotatable shaft. The rotor arrangement is disposed within the stator and forms an air gap between the rotor arrangement and the stator. At least one sensor is disposed in the air gap and/or within the stator. Measurement signals are detected that are dependent on a magnetic field produced by the electrodynamic machine. The measurement signals are used as a basis for detecting oscillations of the shaft. | 04-14-2011 |
| 20110079014 | BURNER ARRANGEMENT, AND USE OF SUCH A BURNER ARRANGEMENT - A burner arrangement includes a tubular mixing tube extending along an axis and configured to mix fuel and air, the mixing tube opening into a combustion chamber in a direction of flow; and a film air ring disposed in the mixing tube and arranged concentrically to the axis, the film air ring configured to prevent a backfiring of the fuel disposed in the mixing tube and to generate or reinforce an air film near the wall, wherein the film air ring has at least one annular gap concentric to the axis and configured to inject air. | 04-07-2011 |
| 20110076155 | GUIDE BLADE FOR A GAS TURBINE - A guide blade for a gas turbine includes an inner and an outer platform, an airfoil extending in a radial direction between the inner and the outer platforms and having a height in the radial direction, and at least one cooling channel disposed in an interior of the airfoil and configured to receive a cooling medium flowing through the at least one cooling channel configured to cool the guide blade, wherein a cross-sectional area of a blade material of the airfoil varies over the height. | 03-31-2011 |
| 20110070136 | PROMOTER ENHANCED CHILLED AMMONIA BASED SYSTEM AND METHOD FOR REMOVAL OF CO2 FROM FLUE GAS STREAM - A method and system for CO | 03-24-2011 |
| 20110070089 | GUIDE VANE FOR A GAS TURBINE - A stator blade for a gas turbine includes a blade airfoil extending in a longitudinal direction of the blade and is delimited by leading and trailing edges. The stator blade includes a shroud, whose inner side is exposed to hot gas which flows through the gas turbine. A hook-like fastening element for fastening the stator blade on a casing of the gas turbine projects outwards in the region of the trailing edge. The fastening element has a locating slot above the trailing edge for fixing a heat shield, which is connected to the shroud in the flow direction of the hot gas. A cavity is provided on the shroud between the locating slot for the heat shield and the trailing edge of the blade airfoil for reducing the thermal and mechanical stresses in the region of transition between the trailing edge and shroud, thereby extending the service life of the stator blade. | 03-24-2011 |
| 20110068585 | METHOD AND SYSTEM FOR CAPTURING AND UTILIZING ENERGY GENERATED IN A FLUE GAS STREAM PROCESSING SYSTEM - A system and process for utilizing energy generated within a flue gas processing system ( | 03-24-2011 |
| 20110068576 | METHOD FOR EARLY DETECTION AND ANTICIPATORY CONTROL OF CONSUMER-END LOAD SHEDDING IN AN ELECTRICAL GRID, AND APPARTUS FOR CARRYING OUT THE METHOD - A method for early detection and anticipatory control of consumer-end load shedding in a single-phase or polyphase electrical grid supplied with single phase or polyphase by at least one generator driven by at least one rotating machine includes measuring a current and a voltage between the at least one generator and the electrical grid and/or a current and a voltage in the electrical grid, deriving at least one signal from the measured current and voltage and using the at least one derived signal to act on the at least one rotating machine. | 03-24-2011 |
| 20110067570 | SQUARE FILTER BAG AND CAGE DESIGN - A fabric filter bag ( | 03-24-2011 |
| 20110067567 | METHOD AND SYSTEM FOR REGENERATING A SOLUTION USED IN A WASH VESSEL - A process and system ( | 03-24-2011 |
| 20110064636 | METHOD FOR REMOVAL OF CARBON DIOXIDE FROM A PROCESS GAS - The invention relates to a method of removing carbon dioxide from a process gas, the method comprising: a) allowing an ammoniated solution to enter an absorption arrangement, said absorption arrangement comprising at least a first absorber; b) contacting the ammoniated solution with the process gas in said first absorber, the ammoniated solution capturing at least a part of the carbon dioxide of the process gas; c) allowing the ammoniated solution to exit the absorption arrangement; d) cooling the ammoniated solution, wherein at least a part of the captured carbon dioxide is precipitated as solid salt; e) allowing the cooled ammoniated solution to enter a separator, in which separator at least a part of the precipitated solids are removed from the ammoniated solution, after which the ammoniated solution is allowed to exit the separator; f) heating the ammoniated solution; and g) allowing the heated ammoniated solution to re-enter the absorption arrangement. The invention also relates to a carbon dioxide removal system. | 03-17-2011 |
| 20110064585 | COOLING DUCT ARRANGEMENT WITHIN A HOLLOW-CAST CASTING - Described is a cooling passage arrangement inside a hollow-cast cast part, with a flow region, delimited by at least two spaced apart cast-part walls, for a cooling medium (K), which flow region is divided in the flow direction into two cooling passages ( | 03-17-2011 |
| 20110061831 | SYSTEM AND METHOD FOR NON-CONTACT SENSING TO MINIMIZE LEAKAGE BETWEEN PROCESS STREAMS IN AN AIR PREHEATER - A rotary air preheater | 03-17-2011 |
| 20110059408 | METHOD AND BURNER ARRANGEMENT FOR THE PRODUCTION OF HOT GAS, AND USE OF SAID METHOD - A method for producing hot gas for operating a turbomachine fired with at least one combustion chamber includes premixing a fuel with a plurality of operating gases by introducing fuel into the plurality of operating gases in a mixing chamber disposed upstream of the combustion chamber using a burner arrangement, wherein the fuel includes at least one of a combustible gas and a H | 03-10-2011 |
| 20110058957 | BLADE FOR A GAS TURBINE - A blade is provided for a gas turbine, especially for the low-pressure turbine of a gas turbine with sequential combustion, and is produced in accordance with a casting process and has a blade airfoil which extends in the radial direction between an inner platform and an outer platform, and in the interior of which extends a cooling passage, bypassing the platforms, and through which flows a cooling medium, especially cooling air, for cooling the blade. In the outer and/or inner platform there are core outlet openings which arise from the use of a casting core and which connect the cooling passage to the outside space and are sealed off by means of a sealing element. Optimum cooling is ensured by the sealing elements being formed and inserted into the core outlet openings so that they align with the wall surface of the cooling passage in a flush manner. | 03-10-2011 |
| 20110058953 | TURBINE BLADE - A turbine blade is provided having an airfoil and a platform manufactured in two separate pieces, which are joined together. The blade includes a seal, which is a mechanically decoupled seal, interposed between the airfoil and platform in a position closer to a hot gases path than a joint. | 03-10-2011 |
| 20110058940 | GAS TURBINE - A gas turbine is provided including a compressor, a combustion chamber, a guide vane row and a rotor airfoil row. The guide vane row includes a plurality of guide vane airfoils having a blade and an inner platform. The ratio between the pitch and the leading edge diameter of the guide vane airfoils is between 6.3-7.6 and the ratio between the platform length and the leading edge diameter of the guide vane airfoils is between 4.0-5.5. | 03-10-2011 |
| 20110056648 | HOLLOW-CAST CASTING - A hollow-cast casting is provided, which includes at least one core opening that is caused by the production technique and which has a closure device that closes the core opening. The closure device can be inserted into the core opening axially in relation to the core opening and provides at least one surface region which, in axial projection in relation to the core opening, can be made to abut a surface region of the casting that is facing toward the casting. The surface region lies radially outside a cross-sectional area predetermined by the core opening. | 03-10-2011 |
| 20110056205 | BURNER ARRANGEMENT AND USE OF SAME - A burner arrangement is provided including a swirl-generating premix burner for providing a fuel/air mixture produced with a first fuel as well as a mixing pipe adjoining the premix burner downstream thereof and extending into a combustion chamber. In the case of such a burner arrangement, safer operation with highly reactive, in particular H | 03-10-2011 |
| 20110056200 | POWER PLANT WITH CO2 CAPTURE AND COMPRESSION - Power plant characteristics are operated in a flexible manner by controlling the power consumption of a CO | 03-10-2011 |
| 20110052401 | JOINED TURBINE ROTOR COMPONENTS AND METHOD THEREOF - A method is disclosed for joining steel and nickel alloy turbine rotor components as is a joined turbine rotor combination produced by the method. The method includes: providing a steel rotor component; providing (e.g., laying down) a nickel alloy butter layer on the steel component; providing a nickel alloy rotor component; and welding the nickel alloy butter layer to the nickel alloy component using a nickel alloy weld filler so as to join together the components. The butter layer, laid first to the steel component, can enable reliable testing, for defects, of a nickel alloy/steel fusion line. | 03-03-2011 |
| 20110050183 | STATIC EXCITER OF A FIELD WINDING AND METHOD FOR OPERATING THE SAME - A static exciter of a field winding includes a rectifier connected to an electric grid and to the field winding; a unidirectional electronic switch connected in series with the rectifier; a capacitor bank; and a further switch disposed between the unidirectional electronic switch and the capacitor bank. Exciter also includes a control unit connected to the further switch and configured to close the further switch when a grid voltage drops below a first prefixed voltage value so as to connect the capacitor bank to the field winding and configured to open the further switch when the grid voltage exceeds a second prefixed voltage value so as to disconnect the capacitor bank from the field winding and so as to supply energy to the field winding from the capacitor bank for a time period. | 03-03-2011 |
| 20110048296 | PROCESS FOR USING A FACILITY FOR COMBUSTING CARBONACEOUS MATERIALS - A process for using a facility having a first reactor ( | 03-03-2011 |
| 20110048239 | CHILLED AMMONIA BASED CO2 CAPTURE SYSTEM WITH WATER WASH SYSTEM - A method and system for reducing an amount of ammonia in a flue gas stream. The system | 03-03-2011 |
| 20110048018 | COMBUSTION DEVICE OF A GAS TURBINE - A combustion device for a gas turbine that includes a portion having first and second walls that defines an inside of the combustion device, a zone between the first and second walls and an outside of the combustion device. A plurality of first passages connect the inside of the combustion device to the zone between the first and second walls and a plurality of second passages connect the zone between the first and second walls to the outside of the combustion device. A plurality of chambers are defined within the zone between the first and second walls, each chamber being connected with one first passage and at least one second passage. Each chamber defining a Helmholtz damper. | 03-03-2011 |
| 20110048015 | POWER PLANT WITH CO2 CAPTURE AND COMPRESSION - A power plant frequency response characteristic is implemented by controlling the power consumption of a CO | 03-03-2011 |
| 20110048010 | APPARATUS AND METHOD FOR CLOSE COUPLING OF HEAT RECOVERY STEAM GENERATORS WITH GAS TURBINES - A heat recovery steam generator (“HRSG”) | 03-03-2011 |
| 20110045422 | OPTICAL FLUE GAS MONITOR AND CONTROL - A plurality of optical monitoring systems | 02-24-2011 |
| 20110045420 | BURNER MONITOR AND CONTROL - A monitoring and control apparatus ( | 02-24-2011 |
| 20110044870 | SYSTEM AND METHOD FOR FLUE GAS SCRUBBING - An apparatus | 02-24-2011 |
| 20110042035 | HEAT TRANSFER ELEMENT FOR A ROTARY REGENERATIVE HEAT EXCHANGER - A rotary regenerative heat exchanger [ | 02-24-2011 |
| 20110038733 | BLADE FOR A ROTATING THERMAL MACHINE - A blade for a rotating thermal machine, such as a stator blade for a low-pressure turbine of a gas turbine with sequential combustion, includes a blade airfoil which extends essentially in the radial direction, is exposed to circumflow by an operating medium in a flow direction, and is delimited by a leading edge and a trailing edge in the flow direction. The concurring fluidic and constructional demands on the blade with sharp inclination of the flow are met by the blade airfoil being structured in such a way that an angle which the flow lines form with the trailing edge of the blade airfoil deviates from a right angle within a limited range. | 02-17-2011 |
| 20110037276 | METHOD FOR CONTROLLING A GAS TURBINE IN A POWER STATION, AND A POWER STATION FOR CARRYING OUT THE METHOD - A method is provided for operating a gas turbine in a power station in which limits of the operating concept, which provide limits for optimization of the power station operation in respect of efficiency, service life consumption, emissions and power provision to the grid system, are adapted during operation. In particular, temperature limits and compressor inlet guide vane position limits are varied as a function of the optimization aims. A gas turbine power station is also provided for carrying out the method. | 02-17-2011 |
| 20110033351 | SYSTEM AND METHOD FOR CALCINING GYPSUM | 02-10-2011 |
| 20110027732 | BURNER OF A GAS TURBINE - The burner of a gas turbine includes two or more part cone shells arranged offset with respect to one another and defining a cone shaped chamber with longitudinal tangential slots for feeding air therein. A lance carrying a liquid fuel nozzle arranged centrally in the cone shaped chamber is also provided. A portion of the nozzle facing the cone shaped chamber is divergent in shape. A diffuser angle (α) between the wall of the nozzle and a longitudinal axis of the cone shaped chamber is less than 5°. A diverging portion of the nozzle has a diffuser length to nozzle diameter ratio comprised between 2-6. The nozzle diameter is the smaller diameter of the diverging portion. | 02-03-2011 |
| 20110016876 | METHOD FOR THE CONTROL OF GAS TURBINE ENGINES - A method for operating a gas turbine engine system under baseload and/or a high part load conditions is disclosed, the gas turbine engine system includes a gas turbine engine with at least one compressor with at least one row of adjustable variable vanes for control of the inlet air mass flow; at least one combustor; at least one turbine. A control system is provided, which, on the basis of and as a function of at least one measured temperature value measured upstream of the compressor or a measurable quantity directly functionally related thereto, controls the position of the variable vanes such that at least one measured pressure value varying with the angular position of the variable vanes is at a predefined target pressure which is a function of said first temperature. | 01-27-2011 |
| 20110016875 | GUIDE VANE HAVING HOOKED FASTENER FOR A GAS TURBINE - A stator vane for a gas turbine includes a vane airfoil which extends in the longitudinal direction of the vane and which is delimited by a leading edge and a trailing edge, and also an outer platform, the inner side of which is exposed to the hot gas which flows through the gas turbine, and on which provision is made for a hook-like fastening element, projecting outwards in the region of the trailing edge, for fastening the stator vane on a casing of the gas turbine, which fastening element, on its side facing the trailing edge, has a locating slot above the trailing edge for the fixing of a heat shield which adjoins the outer platform of the stator vane in the flow direction of the hot gas. With such a stator vane, the service life can be extended by provision being made on the outer platform of the stator vane between the locating slot and the trailing edge of structure for reducing the thermal and mechanical stresses in the region of the transition between trailing edge and outer platform. | 01-27-2011 |
| 20110014054 | GUIDE VANE OF A GAS TURBINE AND METHOD FOR REPLACING A COVER PLATE OF A GUIDE VANE OF A GAS TURBINE - The guide vane of a gas turbine comprises a blade having an outer platform connectable to a guide vane carrier or gas turbine casing, and at the opposite end an inner platform that carries a cover plate. The inner platform has a dovetail housing to which the cover plate is connected. The method for replacing the cover plate consists in separating the cover plate from the inner platform by cutting along the profile of the dovetail housing, then making the cover plate to slide out of the dovetail housing, thus inserting a new or refurbished cover plate into the dovetail housing. | 01-20-2011 |
| 20110012637 | METHOD FOR DETECTION OF INTERLAMINAR SHEET SHORT CIRCUITS IN THE STATOR SHEET CORE OF ELECTROMACHINES - A method and an apparatus are described for detection of interlaminar laminate shorts in the laminated stator core of electrical machines, in which the laminated stator core ( | 01-20-2011 |
| 20110008177 | GAS TURBINE VANE WITH IMPROVED COOLING - The disclosure relates to a hollow gas turbine vane that is cooled by an arrangement configured to sequential cooling an endwall of the vane and its airfoil and, at the same time, the two endwalls of the vane. This arrangement can reduce cooling air demand, which can have a positive effect on the turbines efficiency. | 01-13-2011 |
| 20110005054 | ALIGNMENT OF MACHINE COMPONENTS WITHIN CASINGS - A method and device are provided to accurately align a machine component of generally circular cross-section within a surrounding machine casing that includes bottom and top halves of the casing. The bottom half and top half, in use, are bolted together at a split line occupying a horizontal plane. The component and the bottom half of the casing include complementary interdigitating members at three circumferentially spaced-apart locations, which include first and second locations at the split line on respective first and second horizontally opposed sides of the component, and a third location at bottom dead center. After lowering the component into the bottom half to engage the interdigitating members at the three locations, jacking apparatus is operated independently at each location to incrementally reposition the component within the bottom half. Shims are then inserted between the interdigitating members at the three locations to maintain the jacked position of the component. | 01-13-2011 |
| 20100330282 | SLURRY FORMULATION FOR THE PRODUCTION OF THERMAL BARRIER COATINGS - A slurry formulation for production of a patch or a strip of a thermal barrier coating includes 20-60 dry weight percent of alkali metal silicate binder, 40-80 dry weight percent of ceramic fillers including at least one ceramic filler selected from the group consisting of yttria-stabilized zirconia and magnesia, 0-20 dry weight percent of additives, wherein the dry weight percent of the alkali metal silicate binder, the ceramic fillers and the additives add up to 100%, and one of a solvent and suspension agent. | 12-30-2010 |
| 20100327094 | FORCE MONITOR FOR PULVERIZER INTEGRAL SPRING ASSEMBLY - A pulverizer | 12-30-2010 |
| 20100319949 | ELECTRICAL CONNECTION OF A SEALED ELECTRICAL MACHINE AND METHOD FOR COOLING AN ELECTRICAL CONNECTION OF A SEALED ELECTRICAL MACHINE - The electrical connection of a sealed electrical machine is provided and includes a casing containing lead conductors each connected to a bushing via an electrical connector. The casing has at least an inlet and an outlet for a cooling fluid. The electrical connector includes at least a permeable element defining a chamber such that during operation the cooling fluid, passing through the chamber and the permeable element, cools the permeable element. A method is also provided for cooling an electrical connection. | 12-23-2010 |
| 20100316964 | SOLIDS FLOW METER FOR INTEGRATED BOILER CONTROL SYSTEM - A combustion control system [ | 12-16-2010 |
| 20100314021 | METHOD FOR THE IMPROVED MANUFACTURE OF THE INSULATION OF A CONDUCTOR ELEMENT FOR AN ELECTRICAL MACHINE - A method is provided for the manufacture of an insulation of a conductor element of an electrical machine. The insulation includes an insulating strip with a filler contained in it, which is wound around the conductor element. At least one electrode plate is arranged adjacent to the outside of the insulation, and an amount of heat being introduced into the insulation by applying a voltage between the conductor element and the electrode plate in order to cause an effect on the filler. | 12-16-2010 |
| 20100313571 | GAS TURBINE - In a gas turbine, a plurality of burners, which are arranged concentrically to the rotational axis in a regular arrangement, each directing hot gas through an associated combustion chamber outlet into a turbine, at the inlet of which a second plurality of stator blades are arranged in a ring, uniformly spaced apart around the rotational axis. Cooling openings are provided, which are distributed over the circumference, through which cooling air is injected into the hot gas flow at the combustion chamber outlet. An improvement of the flow conditions in the hot gas is achieved by the cooling openings being divided into first cooling opening groups and second cooling opening groups. The arrangement of the first cooling opening groups corresponds to the arrangement of the stator blades, and in that the arrangement of the second cooling opening groups corresponds to the regular arrangement of the burners. | 12-16-2010 |
