Patent application number | Description | Published |
20080234294 | Cxcr4 Binding Molecules - This invention relates to the use of a CXCR binding molecules as described in the specification, in WHIM syndrome. | 09-25-2008 |
20090104149 | Compositions For HCV Treatment - The present invention concerns a pharmaceutical combination comprising a) a first agent which is a non-immunosuppressive cyclophilin-binding cyclosporin, e.g. a compound of formula I and b) a co-agent. | 04-23-2009 |
20090214464 | COMPOUNDS FOR FLAVIVIRIDAE TREATMENT - Disclosed are non-immunosuppressive cyclophilin-binding cyclosporins, e.g. of formula I, Ia or II as defined herein, having useful properties in the prevention or treatment of Flaviviridae infections and Flaviviridae induced disorders. | 08-27-2009 |
20090221598 | Use of Sanglifehrin in HCV - The present invention discloses the use of a cyclophilin-binding compound such as a sanglifehrin for the treatment and prevention of hepatitis C and related diseases such as liver fibrosis, liver cirrhosis and hepatocellular carcinoma. | 09-03-2009 |
Patent application number | Description | Published |
20100148005 | CURVED BEAM OF FIBER COMPOSITE MATERIAL - A curved beam of fiber composite material. The beam includes a first flange curved in a longitudinal direction, a second flange curved in a longitudinal direction and having a greater longitudinal extent than the first flange, and a web curved in a longitudinal direction and extending between the first flange and the second flange. The beam includes a fiber composite laminate including layers of fibers having different fiber directions, wherein a fiber density per unit of area of the second flange is lower than a fiber density per unit of area of the first flange, and wherein the first flange, the second flange and the web are seamless, continuous, and unfolded in a longitudinal direction. | 06-17-2010 |
20110250381 | METHOD OF FORMING A COMPOSITE ARTICLE - A method of forming an article on a tool and an article. The tool has one longitudinal direction and one transversal direction. A stack of plies including fibers is arranged so that when positioned on the tool a ply arranged closest to the tool and a ply arranged furthest away from the tool have fibers substantially orthogonal to the longitudinal direction of the tool. At least one ply is arranged having the fibers substantially in a same direction as the longitudinal direction of the tool between the plies having fibers substantially orthogonal to the longitudinal direction of the tool. The stack is conformed to the tool with a forming medium. The article is removed from the tool. | 10-13-2011 |
20110315300 | METHOD OF ATTACHING ELEMENTS BY BONDING - A method of attaching a first portion and a second portion to each other. An adhesive is exposed to a low temperature in order to obtain a non-tacky adhesive. The non-tacky adhesive is arranged between the two portions. The adhesive is cured. Use of adhesive according to the method. | 12-29-2011 |
20120003347 | METHOD AND DEVICE FOR SHAPING OF COMPOSITE MATERIAL - A device for shaping of an article of composite material. The device includes a tool including a top surface and side surface for shaping at least one blank of composite material into an article having a predetermined profile; and a air-tight foil. The device further includes at least one support arranged to be in supporting contact with the underside of the protruding part of the blank. | 01-05-2012 |
20120256076 | COMPOSITE STRUCTURE TOOL - A method of producing a forming tool and a forming tool for forming an article. The forming tool includes a composite face sheet having a forming surface and an inner surface opposite the forming surface. A support structure is attached to the inner surface of the composite face sheet. The support structure includes a support shell of composite having a first surface facing the inner surface of the composite face sheet and having a second surface opposite the first surface. The support structure further includes distance members. The support shell is fixed at a distance from the composite face sheet by the distance members. | 10-11-2012 |
20120292439 | ARTICLE WITH DE-ICING/ANTI-ICING FUNCTION - A structural article including an outer surface that serves as an aerodynamic surface when the structural article is subjected for an air stream. A resin matrix laminate includes an upper ply and a bottom ply. A heating element is arranged in contact with the bottom ply and coupled to a power supply unit in purpose to deice/anti-ice the outer surface. Each ply includes a thermally conductive filament structure having a filament orientation such that the prolongation of the filaments has an extension essentially perpendicular to the extension of the laminate. The thermally conductive filament structure of the upper ply is embedded in the upper ply in such way that at least a portion of the thermally conductive filament structure is exposed in the outer surface. | 11-22-2012 |
20130129968 | COMPOSITE ARTICLE COMPRISING PARTICLES AND A METHOD OF FORMING A COMPOSITE ARTICLE - A composite article having a longitudinal direction and a transversal direction. The article includes a stack of plies wherein one ply is a bottom ply and one ply is a top ply. Most or all of the plies include fibers. A plurality of plies have fibers substantially in an orthogonal direction and substantially in a same direction as the longitudinally direction of the article. The bottom ply and the top ply have fibers in a substantially orthogonal direction to the longitudinal direction of the article. At least one ply has the fibers substantially in the same direction as the longitudinal direction of the article. At least one of the plies having fibers substantially in the longitudinal direction includes particles selected from the group of thermoplastic tougheners, nano particles, micro particles, elastic particles, elastomer particles and polymer particles or a combination. Also a method of forming an article on a tool. | 05-23-2013 |
20130240110 | SMOOTH SURFACE FORMING TOOL AND MANUFACTURE THEREOF - An aircraft article composite forming tool and a method for producing the tool. The aircraft article to be formed includes a composite material including an outer surface. The aircraft article composite forming tool includes a matrix laminate made of at least an upper ply including a forming surface for forming the aircraft article and outer surface. The upper ply includes a nano filament structure embedded therein. | 09-19-2013 |
Patent application number | Description | Published |
20090025448 | Method and apparatus for manufacture of a profile element - A method and an apparatus for manufacturing of a profile element including a web portion, a first and second flange portion, which extend from the web portion and are disposed essentially opposite each other. The method includes folding a blank of composite material about a first and second flange forming surface of a forming tool. The method includes setting at least one flange forming surface of a forming tool a distance from another flange forming surface greater than a desired distance between inner surfaces of the flange portions of a finished profile element. The folded blank is cured and a gradual decrease of the distance between the flange forming surfaces is simultaneously controlled. The cured profile element is removed from the forming tool. | 01-29-2009 |
20090025865 | Method and apparatus for manufacturing of a wing spar profile element - A method and an apparatus for manufacture of an elongated beam profile element including a recess configured to accommodate a support element. The method includes forming the blank into the web portion with at least one first protrusion formed to extend across the web portion and to protrude outward from the web portion's outer surface; and into the first flange portion with at least one second protrusion formed to extend across the first flange portion and to protrude inward from the first flange portion's inner surface, wherein this second protrusion merges into the first protrusion and constitutes the recess for accommodating the support element under a wing. | 01-29-2009 |
20090057948 | Method and apparatus for manufacturing a curved elongated structural element - A method and an apparatus for manufacturing of a curved elongated structural element of composite material. The curved elongated structural element includes a first elongated portion and a second elongated portion in an angled relation. A substantially flat blank of composite material including a first and second elongated edge is provided. The blank is folded over a first portion forming surface and a second portion forming surface of a forming tool's flexible tool body for forming the first elongated portion and the second elongated portion. The forming tool's tool body is bent such that its bending moment center prevails essentially adjacent the first portion forming surface. | 03-05-2009 |
20090091063 | METHOD AND DEVICE FOR SHAPING OF COMPOSITE MATERIAL - A method and device for shaping of an article of composite material. The method includes arranging a blank of composite material on a top surface of a forming tool. A portion of the blank is arranged to protrude outside the top surface of the tool. At least one support is arranged in contact with an underside of the protruding portion of the blank. An air-tight foil is arranged over the arrangement. The air-tight foil is forced towards the blank. The support is lowered until the blank is shaped over the tool. The support is stopped and/or removed. The device includes a tool including a top surface and side surface for shaping at least one blank of composite material into an article having a predetermined profile; and a air-tight foil. The device further includes at least one support arranged to be in supporting contact with the underside of the protruding part of the blank. | 04-09-2009 |
20090110836 | METHOD OF FORMING A COMPOSITE STRUCTURE - The present invention relates to a method of manufacturing a composite structure ( | 04-30-2009 |
20090152775 | METHOD AND APPARATUS FOR MANUFACTURING OF AN ARTICLE INCLUDING AN EMPTY SPACE - A tool assembly including a male tool including an inner shape tool including a bag having a connection connectable to a depressurization source for providing a vacuum in the bag such that beads therein form a body of firm cohesion providing the inner shape tool rigid. The male tool further includes a flexible, hollow curing support arranged around the rigid inner shape tool, the inner shape tool is arranged to be removable from the flexible, hollow curing support by rupturing the vacuum. | 06-18-2009 |
20100148005 | CURVED BEAM OF FIBER COMPOSITE MATERIAL - A curved beam of fiber composite material. The beam includes a first flange curved in a longitudinal direction, a second flange curved in a longitudinal direction and having a greater longitudinal extent than the first flange, and a web curved in a longitudinal direction and extending between the first flange and the second flange. The beam includes a fiber composite laminate including layers of fibers having different fiber directions, wherein a fiber density per unit of area of the second flange is lower than a fiber density per unit of area of the first flange, and wherein the first flange, the second flange and the web are seamless, continuous, and unfolded in a longitudinal direction. | 06-17-2010 |
20120003347 | METHOD AND DEVICE FOR SHAPING OF COMPOSITE MATERIAL - A device for shaping of an article of composite material. The device includes a tool including a top surface and side surface for shaping at least one blank of composite material into an article having a predetermined profile; and a air-tight foil. The device further includes at least one support arranged to be in supporting contact with the underside of the protruding part of the blank. | 01-05-2012 |
20120074265 | NANO-REINFORCED RADIUS FILLER FOR AN AIRCRAFT STRUCTURE AND A METHOD OF PRODUCING AN AIRCRAFT STRUCTURE COMPRISING SUCH FILLER - A composite radius filler for use in an aircraft structure. The aircraft structure includes structural composite parts assembled together to form the aircraft structure. The composite radius filler is arranged between rounded sections of the structural composite parts for filling a gap formed between the structural composite parts. The composite radius filler is made structural by a nanostructure arranged within the composite radius filler for the reinforcement of the interface between the radius filler and the structural composite part. A method for producing an aircraft structure including a nano-reinforced radius filler. | 03-29-2012 |
20120088056 | STRUCTURAL LONGITUDINAL COMPOSITE JOINT FOR AIRCRAFT STRUCTURE - A structural composite part made of pre-impregnated fiber plies. The edges of two adjacent fiber plies are connected via a longitudinal composite joint made structural by a nanostructure arranged within the composite joint. A method of producing a structural composite part made of pre-impregnated fiber plies. The edges of two adjacent fiber plies are connected via a longitudinal composite joint made structural by a nanostructure and an aircraft structure comprising such structural composite parts. | 04-12-2012 |
20130129968 | COMPOSITE ARTICLE COMPRISING PARTICLES AND A METHOD OF FORMING A COMPOSITE ARTICLE - A composite article having a longitudinal direction and a transversal direction. The article includes a stack of plies wherein one ply is a bottom ply and one ply is a top ply. Most or all of the plies include fibers. A plurality of plies have fibers substantially in an orthogonal direction and substantially in a same direction as the longitudinally direction of the article. The bottom ply and the top ply have fibers in a substantially orthogonal direction to the longitudinal direction of the article. At least one ply has the fibers substantially in the same direction as the longitudinal direction of the article. At least one of the plies having fibers substantially in the longitudinal direction includes particles selected from the group of thermoplastic tougheners, nano particles, micro particles, elastic particles, elastomer particles and polymer particles or a combination. Also a method of forming an article on a tool. | 05-23-2013 |
20130240110 | SMOOTH SURFACE FORMING TOOL AND MANUFACTURE THEREOF - An aircraft article composite forming tool and a method for producing the tool. The aircraft article to be formed includes a composite material including an outer surface. The aircraft article composite forming tool includes a matrix laminate made of at least an upper ply including a forming surface for forming the aircraft article and outer surface. The upper ply includes a nano filament structure embedded therein. | 09-19-2013 |
20150290845 | SMOOTH SURFACE FORMING TOOL AND MANUFACTURE THEREOF - A method of manufacture of a composite aircraft article aerodynamic surface by forming the composite aircraft article aerodynamic surface on an aircraft article composite forming tool. The aircraft article composite forming tool includes a matrix laminate including an upper ply including a forming surface for forming the composite aircraft article aerodynamic surface. The upper ply of the aircraft article composite forming tool includes a nano filament structure embedded therein. A blank is conformed onto the aircraft article composite forming tool. The aircraft article is formed on the upper ply of the forming surface. The forming surface of the aircraft article composite forming tool is adapted to form an aerodynamic surface of the aircraft article. The blank is cured into the aircraft article. The composite aircraft article is finished. | 10-15-2015 |
Patent application number | Description | Published |
20080315102 | INFRARED SPECTROMETER - Method and apparatus for detecting, by absorption spectroscopy, an isotopic ratio of a sample, by passing first and second laser beams of different frequencies through the sample. Two IR absorption cells are used, a first containing a reference gas of known isotopic ratio and the second containing a sample of unknown isotopic ratio. An interlacer or reflective chopper may be used so that as the laser frequencies are scanned the absorption of the sample cell and the reference cell are detected alternately. This ensures that the apparatus is continuously calibrated and rejects the baseline noise when phase sensitive detection is used. | 12-25-2008 |
20120274929 | DETECTING SPECIES IN A DILUTE MEDIUM - Method and apparatus for detecting a species in a dilute medium, the species having a spectral feature, the apparatus comprising: a beam source arranged to generate a first laser beam and a second laser beam coherent with each other, and having a matching chirp pattern. Beam guide arranged to pass at least the first laser beam through the dilute medium; a beam mixer arranged to mix the first and the second laser beams to form a mixed beam. Detector arranged to detect, during the chirp pattern, the mixed beam and to measure changes in the mixed beam caused by refractive index variations in the dilute medium across a spectral feature. Output providing a signal that changes in response to the measured changes. | 11-01-2012 |
20150014543 | HETERODYNE DETECTION SYSTEM AND METHOD - An active heterodyne detection system comprises a continuously tuneable laser source ( | 01-15-2015 |
20150260574 | VAPOUR PHASE SPECTROSCOPY - A method is provided of obtaining a vapour phase spectrum of a compound. The method comprises providing an isolated condensed phase sample of the compound, vaporising the sample and supplying the vapour to an absorption cell of a spectrometer. A rate at which vapour enters the absorption cell is determined and a steady state concentration of vapour in the absorption cell is established. The spectrum of the vapour is then measured. | 09-17-2015 |
20150260832 | METHOD AND APPARATUS FOR REDUCING SPECKLE NOISE IN AN OPTICAL SYSTEM - The invention relates to a method and apparatus for reducing speckle noise in a system comprising a sensor for detecting electro-magnetic radiation backscattered from a target, comprising: illuminating the target with a first illuminating beam having a first optical path; illuminating the target with a second illuminating beam having a second optical path different to the first optical path; capturing at the sensor first and second backscattered radiation components associated with respectively the first and second illuminating beams, each of the backscattered radiation components comprising a speckle pattern; and taking a time-averaged measurement of the intensities of the first and second backscattered radiation components; wherein the capturing step is carried out within an integration time t of the sensor, such that the time-averaged intensity measurement results in a decrease in speckle noise present in a signal representing the backscattered radiation. | 09-17-2015 |
Patent application number | Description | Published |
20100218558 | Method for Temperature Manipulation of a Melt - For permitting temperature manipulation of a melt even at a conductivity below 10 | 09-02-2010 |
20110034316 | Device and method for the continuous fining of glasses with high purity requirements - The present invention relates to a device and to a method for the continuous fining or homogenizing of inorganic matter, preferably low-viscosity glass melts in an apparatus. The device and method are distinguished in that the inclusion of bubbles and the occurrence of striations in the glass end product are significantly reduced or even entirely avoided when the melt contact surface of the apparatus has iridium or a high-iridium alloy as its material. | 02-10-2011 |
20130279532 | ENERGY EFFICIENT HIGH-TEMPERATURE REFINING - An energy-efficient device for refining a glass melt to produce a glass and/or a glass ceramic is provided. The device includes a refining crucible defined at least by lateral walls with a metallic lining as a melt contact surface, so that a melt refining volume is defined by a base surface, a top surface and a circumferential surface; at least one heating device that conductively heats the lining by an electric current in the lining, so that the melt is heated through the lining, the heating device and the lining are connected to one another by a feeding device. The feeding device establishes contact with the lining so that an electric current runs from the top surface to the base surface or from the base surface to the top surface, at least in sections of the lining. | 10-24-2013 |
20150070907 | OPTICAL CONVERTER FOR HIGH LUMINANCES - An optical converter for producing colored or white light from blue excitation light is provided. The converter has good scattering properties to be able to produce nearly white light from the scattered blue light components and the scattered, converted yellow light components. The optical converter includes material including one or more of a YAG ceramic, a LuAG ceramic, and a magnesium-aluminum ceramic exhibiting strong scattering. | 03-12-2015 |
20150241046 | COOLING OF A CONVERTER ARRANGEMENT FOR LIGHT SOURCES WITH HIGH LUMINANCE - A converter arrangement for light sources with high luminance is provided that includes an axially pivotable carrying wheel and a converter fixed on one side of the carrying wheel. The converter includes fluorescent materials that convert impinging light into light having a different wave length and emits the light having the different wavelength. The ratio of the total area of the converter arrangement to the area enclosed by the outer boundary curve of the converter is at least 3, preferably at least 3.5, particularly preferably at least 4.5. | 08-27-2015 |
Patent application number | Description | Published |
20080240481 | HEARING DEVICE WITH EMBEDDED CHANNEL - A hearing device having at least one of an acoustical/electrical converter and an electrical/acoustical converter respectively with an acoustical input or output. The input or output, as the case may be, is linked to a coupling opening at the outer surface of the device via a channel. At least a part of the outer surface of the device is formed by a one-part shell. The shell defines an inner space of the device, with the channel being provided within and along the part of the shell and being formed within the material of the shell. | 10-02-2008 |
20080300703 | HEARING DEVICE WITH EMBEDDED CHANNEL - A hearing device having at least one of an acoustical/electrical converter and an electrical/acoustical converter respectively with an acoustical input or output. The input or output, as the case may be, is linked to a coupling opening at the outer surface of the device via a channel. At least a part of the outer surface of the device is formed by a one-part shell. The shell defines an inner space of the device, with the channel being provided within and along the part of the shell and being formed within the material of the shell. | 12-04-2008 |
20080301944 | HEARING DEVICE WITH EMBEDDED CHANNEL - A hearing device having at least one of an acoustical/electrical converter and an electrical/acoustical converter respectively with an acoustical input or output. The input or output, as the case may be, is linked to a coupling opening at the outer surface of the device via a channel. At least a part of the outer surface of the device is formed by a one-part shell. The shell defines an inner space of the device, with the channel being provided within and along the part of the shell and being formed within the material of the shell. | 12-11-2008 |
Patent application number | Description | Published |
20090028712 | TURBOMACHINE HAVING AXIAL ROTOR BLADE SECURING - A rotor of a turbine machine having several rotor blade rings positioned in succession in the axial direction, is disclosed. Each rotor blade ring has a rotor base body with several rotor blades anchored by blade footings in axial grooves of the rotor base body that extend essentially in the axial direction and, in their anchored position in the rotor base body, are secured against displacement in the axial direction. The rotor blades of at least one rotor blade ring have hook-like securing elements, which, in the anchored position on a low-pressure side of the rotor blade ring, abut the rotor base body. The hook-like securing elements, between the rotor base body and a sealing element, which extends between the rotor base body and a rotor base body of a rotor blade ring that connects on the low-pressure side, are fixed in the axial direction on both sides. | 01-29-2009 |
20100104418 | GAS TURBINE - A gas turbine having a rotor which includes a turbine rotor, a shaft and a compressor rotor, the turbine rotor having at least one rotor disk and a rotor cone leading from the or a rotor disk to the shaft, the downstream end of the shaft being rotatably supported in a bearing having a bearing chamber, the interior space of the shaft being designed as a flow channel for bearing-chamber sealing air, and the space surrounding the rotor cone upstream of the same being designed as a flow space for cooling air is disclosed. In the region of the rotor connection, the shaft exhibits an expanded portion, at whose upstream end, openings are provided to allow cooling air to enter, and, at whose downstream end, openings are provided to allow cooling air to exit into the space between the bearing chamber and the rotor cone, a wall separating the streams of the cooling air and of the sealing air in the shaft interior from one another. | 04-29-2010 |
20100202872 | MULTILAYER SHIELDING RING FOR A FLIGHT DRIVING MECHANISM - A shielding ( | 08-12-2010 |
20120141253 | TURBOMACHINE - A turbomachine is disclosed. The turbomachine includes a housing and a guide blade ring. An outer shroud of the guide blade ring is divided into segments by joints, where the outer shroud is fastened to the housing by a first fastening element for absorbing axial force and a second fastening element independent of the first fastening element for absorbing circumferential force. The first fastening element and the second fastening elements enable play in a radial direction for the segments of the outer shroud. | 06-07-2012 |
20130183149 | HOUSING-SIDE STRUCTURE OF A TURBOMACHINE - A housing-side structure of a turbomachine, in particular of a gas turbine, including an in particular segmented jacket ring ( | 07-18-2013 |