Ammann, US
Charles B. Ammann, Tulsa, OK US
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20150106854 | SYSTEMS AND METHODS FOR PROVIDING AUDIO-BASED GUIDANCE - Systems and methods for providing audio-based guidance features are provided. A guidance application may provide listings displays having listings for audio-friendly content. The listings may be indicated as listings for audio-friendly content. The guidance application may provide displays dedicated to listings for audio-friendly content. The guidance application provides audio-prompts describing display screens. The guidance application may determine a user's identity from a voice command and provide personalized guidance features. | 04-16-2015 |
David Ammann, Richmond, VA US
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20090310950 | Capillary system with fluidic element - An aerosol generation system having an aerosol generator wherein a liquid formulation is at least partially vaporized in a capillary passage and discharged from the capillary passage to form an aerosol. The aerosol generation system includes a pumping unit adapted to supply a liquid formulation to the aerosol generator; and a fluidic element located between the pumping unit and the capillary passage of the aerosol generator, wherein the fluidic element increases the pressure of the liquid formulation as the liquid formulation enters the capillary passage of the aerosol generator. | 12-17-2009 |
20130068224 | CONTINUOUS HIGH PRESSURE DELIVERY SYSTEM - A drug delivery system, which includes an aerosol generator unit, a pumping unit, a flow tube, at least one condensate collector and an aerosol transition adapter. The aerosol generator forms an aerosol from a liquid formulation, which is partially vaporized. The pumping unit supplies the liquid formulation to the aerosol generator unit and a flow tube having an inlet end in fluid communication with an outlet of the aerosol generator unit and an outlet adapted for connection to a patient interface, which supplies ventilation to a patient's lungs. The system also includes at least one condensate collector adapted to collect condensed liquid or liquid produced by the aerosol generator unit, and a transition adapter arranged to mix aerosol produced by the aerosol generator unit with heated air and directs the mixed aerosol into the inlet end of the flow passage. | 03-21-2013 |
David Ammann, Alpharetta, GA US
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20140165999 | CAPILLARY SYSTEM WITH FLUIDIC ELEMENT - An aerosol generation system having an aerosol generator wherein a liquid formulation is at least partially volatilized in a capillary passage and discharged from the capillary passage to form an aerosol. The aerosol generation system includes a pumping unit adapted to supply a liquid formulation to the aerosol generator; and a fluidic element located between the pumping unit and the capillary passage of the aerosol generator, wherein the fluidic element increases backpressure of the liquid formulation as the liquid formulation enters the capillary passage of the aerosol generator. | 06-19-2014 |
Kathryn Ammann, Downey, CA US
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20110232672 | Hair Styling Tool - A hairstyling tool has a bowl having a plurality of bowl convex portions and bowl concave portions. The bowl concave portions form air channels. A plurality of openings is disposed on a bottom of the bowl. There are more than twenty openings. A handle is connected to the bowl. The handle has a handle connection with the bowl. A base extends from the bottom of the bowl. The base extends downward around the plurality of openings disposed on the bottom of the bowl. The base forms an air capture indent for directing airflow through the plurality of openings. The handle concave portions and handle convex portions may provide the handle a wavy shape. The handle may extend from a bowl convex portion between a pair of air channels. A palm rest can be at a free end of the handle. | 09-29-2011 |
Lisa Ammann, Simpsonville, SC US
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20140161585 | TURBO-MACHINE COMPONENT AND METHOD - A component, a component manufacturing process, and a component operation process are disclosed. The component has a diffuser permitting compressible fluid to flow throughout a first region and a second region of the diffuser at a decreasing velocity. The diffuser includes a coating collection feature. The component manufacturing process includes positioning the component and applying the coating to at least a surface of the component outside of the diffuser and to at least a portion of the second region, not to the first region, to the coating collection feature, or a combination thereof. The component operation process includes positioning the component and transporting the compressible fluid through the diffuser. | 06-12-2014 |
Lisa Kamdar Ammann, Simpsonville, SC US
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20100050873 | FILTRATION SYSTEM FOR GAS TURBINES - A system for use with an inlet of a gas turbine through which airflow toward the gas turbine proceeds is provided and includes a first stage to remove primary aerosol droplets from the airflow by coalescing the primary aerosol droplets into secondary aerosol droplets, which are larger than the primary aerosol droplets, and to remove solid particulates from the airflow, a second water tight stage, disposed downstream from the first stage, to prevent the secondary aerosol droplets and aqueous solutions of deliquesced particulates, which are not removed by the first stage and which are re-released into the airflow from the first stage, from proceeding along the airflow and to remove solid particulates not removed by the first stage from the airflow, and a third water removal stage, disposed downstream from the second stage, to remove from the airflow the remaining secondary aerosol droplets leaking from the first and second stages. | 03-04-2010 |
20100054919 | FILTRATION SYSTEM FOR GAS TURBINES - A system for use with an inlet of a gas turbine through which an airflow toward the gas turbine proceeds is provided and includes a first self-cleaning stage to remove dust, snow and ice from the airflow, a second water tight stage, disposed downstream from the first stage, to prevent aerosol droplets and aqueous solutions of deliquesced particulates, which include at least portions of the dust not removed by the first stage and which are re-released into the airflow from the first stage, from proceeding along the airflow and to remove solid particulates not removed by the first stage from the airflow, and a third water removal stage, disposed downstream from the second stage, to remove from the airflow aerosol droplets leaking from the second stage. | 03-04-2010 |
20110173947 | SYSTEM AND METHOD FOR GAS TURBINE POWER AUGMENTATION - A gas turbine power augmentation system and method are provided. The system includes a chiller, a controller, a heat exchanger, and a gas turbine inlet air flow. The chiller may be operable to chill a coolant flow using energy from a heat source. The controller may be operably connected to the chiller and configured to regulate operation of the chiller in relation to at least one environmental condition. The heat exchanger may be in fluid communication with the chiller and configured to allow the coolant flow to pass through the heat exchanger. The gas turbine inlet air flow may be directed through the heat exchanger before entering a gas turbine inlet, allowing the air flow to interact with the coolant flow, thereby cooling the air flow. | 07-21-2011 |
20120031596 | HEAT EXCHANGER MEDIA PAD FOR A GAS TURBINE - A media sheet for a heat exchanger is disclosed. The media sheet includes a first layer having a first outer surface and a second layer having a second outer surface. The first and second layers define a plurality of passages extending therebetween. At least one of the first and second outer surfaces comprises a plurality of depressions. The plurality of depressions further define the plurality of passages therebetween. The media sheet is polymer fiber-based and wettable. | 02-09-2012 |
Luke J. Ammann, Simpsonville, SC US
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20100215501 | APPARATUS FOR BUCKET COVER PLATE RETENTION - In one embodiment, a system includes a turbine engine that includes a turbine stage including a turbine rotor having multiple blades disposed in a first annular arrangement. The turbine engine also includes multiple cover plates disposed in a second annular arrangement along interfaces between the turbine rotor and the blades. The turbine engine further includes multiple lugs coupled to the turbine stage and a first ring coupled to the lugs to hold the cover plates to the turbine stage. | 08-26-2010 |
20100232940 | TURBINE ENGINE SHROUD RING - In one embodiment, a system includes a turbine engine that includes a rotor including multiple blades. The turbine engine also includes a shroud disposed about the blades. The shroud includes multiple segments engaged with one another via mating teeth. The mating teeth are oriented in an axial direction along a longitudinal axis of the turbine engine. | 09-16-2010 |
Luke J. Ammann, Greenville, SC US
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20100172760 | Non-Integral Turbine Blade Platforms and Systems - In one embodiment, a turbine blade platform may be disposed between two turbine blades. The platform may include a first exterior side configured to interface with a first turbine blade. The platform also may include a second exterior side disposed generally opposite the first exterior side and configured to interface with a second turbine blade. | 07-08-2010 |
Luke John Ammann, Simpsonville, SC US
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20100183446 | TURBINE BLADE OR VANE WITH IMPROVED COOLING - Disclosed is a turbine blade or vane including a blade or vane body including a leading edge and a trailing edge, a plurality of cooling openings disposed along the trailing edge, a first width of the trailing edge, the first width being disposed across the cooling openings, and a second width of the trailing edge the second width being disposed between the cooling openings, wherein the second width is smaller than the first width. | 07-22-2010 |
20100196167 | ROTOR CHAMBER COVER MEMBER HAVING APERTURE FOR DIRT SEPARATION AND RELATED TURBINE - A cover member defining a rotor chamber adjacent to a rotor wheel that supports a rotating blade in a turbine includes a first aperture for introducing a cooling gas stream into the rotor chamber, and a second aperture positioned in a radially outward portion of the cover member for allowing a portion of the cooling gas stream to exit the rotor chamber. The portion of the cooling gas stream exiting the rotor chamber carries dirt particles to purge the rotor chamber. | 08-05-2010 |
20110176929 | SYSTEM FOR COOLING TURBINE BLADES - A system, in one embodiment, includes a turbine blade having a radial blade tip. The system further includes a trailing edge trench that is formed in the radial blade tip and which extends towards a trailing edge of the turbine blade. The trailing edge trench further includes a first set of cooling passages, each of which includes a first slot formed along a first sidewall of the trailing edge trench, whereby the slot is coupled to a first respective hole extending through a floor of the trailing edge trench. | 07-21-2011 |
20120070305 | SHANK CAVITY AND COOLING HOLE - A turbine bucket is provided and includes a shank defining a cavity therein, which is connectible with a rotor such that wheelspace air having an initial pressure is permitted to flow into the cavity and a platform coupled to the shank and defining a cooling hole therein, the shank and the platform each further defining the cavity and the cooling hole, respectively, as being fluidly communicative with one another, such that the wheelspace air permitted to flow into the cavity is deliverable from the cavity and through the cooling hole at a second pressure greater than the initial pressure. | 03-22-2012 |
20120087798 | TURBINE BUCKET LOCKWIRE ROTATION PREVENTION - A retention system for a plurality of turbine buckets located in respective mating slots in a turbine rotor wheel includes a plurality of first circumferentially-oriented retention slots formed in outer peripheral portions of the turbine wheel; a plurality of second circumferentially-oriented retention slots formed in wheel mounting portions of said buckets, the first and second circumferentially-oriented retention slots aligned to form an annular lockwire retention slot; and a lockwire located within the annular lockwire retention slot. A first surface feature on one or both of the turbine rotor wheel and one or more of said plurality of turbine buckets is adapted to engage a second surface feature on the lockwire for preventing rotation of the lockwire beyond predetermined limits. | 04-12-2012 |
20120156045 | METHODS, SYSTEMS AND APPARATUS RELATING TO ROOT AND PLATFORM CONFIGURATIONS FOR TURBINE ROTOR BLADES - A rotor blade assembly for a turbine engine, the rotor blade assembly including: a turbine blade that includes a shank situated between attachment means and an airfoil, the shank having a forward portion and an aft portion; and a platform comprising a platform pressure side and a platform suction side, each of which comprising non-integral components to the other and the turbine blade. The platform may comprise an interface between the platform pressure side and the platform suction side. And, the platform may be configured such that the interface aligns with at least one of the forward portion and the aft portion of the shank. | 06-21-2012 |
Luke John Ammann, Greenville, SC US
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20130078094 | Systems and Methods for Mode Shape Identification - Embodiments of the present application can provide systems and methods for mode shape identification of turbine buckets. According to one embodiment, a system can be provided. The system can include a turbine bucket having numerous trigger patterns disposed at a distal end of the turbine bucket. A sensor is disposed adjacent to the distal end of the turbine bucket for detecting the trigger patterns. The trigger patterns are patterned to identify at least one mode shape of the turbine bucket. | 03-28-2013 |
Paul Ammann, Olathe, KS US
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20130305661 | VACUUM PACKAGING MACHINE - The invention relates to a vacuum packaging machine for producing an evacuated packaging of a product, which is disposed between an upper film and a lower film, and which can also be reliably used for thicker cover films or hard packaging. | 11-21-2013 |