Patents
Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889)
12/2007
12/27/2007WO2007147216A1 Power generation
12/27/2007WO2006091379A3 Gas turbine fuel preparation and introduction method
12/27/2007US20070298931 Gas turbine braking apparatus and method
12/27/2007US20070295011 Regenerative Turbine Blade and Vane Cooling for a Tip Turbine Engine
12/27/2007DE102007028583A1 Air bypass system for gas turbine inlet filter housing, surrounds internal cooling system increasing performance and includes butterfly valve for throttling
12/27/2007CA2656922A1 System, method, and apparatus of video processing and applications
12/27/2007CA2644042A1 Apparatus and method for controlling engine windmilling
12/26/2007EP1870581A1 Gas turbine combustor and its ignition method
12/26/2007EP1869289A1 Guide vane support
12/26/2007CN200996324Y Supporting cartridge receiver
12/26/2007CN101092910A Injector mixer of gas and fluid fuels
12/26/2007CN101092907A Method and device for controlling cooling air temperature of gas turbine engine
12/26/2007CN100357569C Equipment for fixing supporting blades of disributor component arround circumferential curved line
12/26/2007CN100357568C Cooled turbine nozzle
12/26/2007CN100357567C Method and device for cooling gas turbine spray nozzles
12/26/2007CN100357466C Nickel base alloy
12/25/2007US7311981 Gas turbine part provided with a protective coating
12/25/2007US7311493 Metal sheet, including means for fixing it to a support and a gasket seal
12/25/2007US7310951 Steady-state detonation combustor and steady-state detonation wave generating method
12/25/2007US7310949 Method and apparatus for arresting a crack within a body
12/21/2007WO2007144207A1 A gas turbine engine and a method of operating a gas turbine engine
12/21/2007CA2684483A1 Dual structured aircraft engine starter/generator
12/20/2007US20070292719 Component comprising a masking layer
12/20/2007US20070292710 Method for repairing components using environmental bond coatings and resultant repaired components
12/20/2007US20070289312 Low-cost frangible cable for gas turbine engine
12/20/2007US20070289311 Combustion apparatus using pilot fuel selected for reduced emissions
12/20/2007US20070289285 Compressed-Air Generating System
12/20/2007DE102006027728A1 Wärmedämmschicht Thermal barrier coating
12/19/2007EP1867843A1 Method of operating a gas turbine combined plant
12/19/2007EP1867842A1 A gas turbine engine and a method of operating a gas turbine engine
12/19/2007EP1866532A1 Method and apparatus for utilising fugitive gases as a supplementary fuel source
12/19/2007EP1755952B1 System for washing an aero gas turbine engine
12/19/2007CN200993050Y Thermoelectric combined production heat engine
12/19/2007CN101091400A Wireless terminal location using apparatus and methods employing carrier diversity
12/19/2007CN101091044A Gas calorie variation suppressor, fuel gas supply facility, gas turbine facility and boiler facility
12/19/2007CN100355922C Nickel-base alloy
12/18/2007CA2418289C Laminated heat resistant alloy plate and manufacturing method therefor
12/18/2007CA2378908C One-step noble metal-aluminide coatings
12/18/2007CA2276544C Particle traps for turbo-prop engine
12/13/2007WO2007141101A1 Method of operating a gas turbine, application of the method in a combined cycle power plant, and combined cycle power plant for carrying out the method
12/13/2007WO2006125210A3 Improved plasma torch for ignition, flameholding and enhancement of combustion in high speed flows
12/13/2007US20070287013 Aluminizing slurry Compositions Free of Hexavalent Chromium, and Related Methods and Articles
12/13/2007DE202007012458U1 Shuttersystem für eine Gasturbine Shutter system for a gas turbine
12/12/2007EP1865262A1 Gas turbine combustor
12/12/2007EP1865172A2 Method and apparatus for starting a gas turbine engine
12/12/2007CN101087928A Static gas turbine component and method for repairing such a component
12/11/2007US7306826 Orientation of the first warp direction of a preselected number of plies lie in the direction of maximum tensile stress during normal operation; rigidizing the shape with a layer of BN and a layer of SiC using chemical vapor infiltration; densifying using a carbon slurry; further densifying with silicon
12/11/2007US7306670 Method for producing monocrystalline structures
12/11/2007US7306432 Apparatus and method of balancing a shaft
12/11/2007US7306024 Refractory metal core wall thickness control
12/11/2007US7305998 Mobile flushing unit and process
12/11/2007US7305832 Work extraction arrangement
12/11/2007US7305831 Gas turbine having exhaust recirculation
12/11/2007US7305830 Fuel manifold inlet tube
12/11/2007CA2372928C Cast on-board injection nozzle with adjustable flow area
12/11/2007CA2312977C Cooling arrangement for turbine rotor
12/10/2007CA2591249A1 Aspirating labyrinth seal
12/06/2007WO2007138802A1 Axial flow fluid device
12/06/2007WO2007137398A1 Starting a gas turbine engine
12/06/2007WO2007137370A1 Power generation
12/06/2007US20070281205 Fluid Separation Device
12/06/2007US20070277531 Secondary Fuel Injection From Stage One Nozzle
12/06/2007DE102007023916A1 Turbocharger for a vehicle comprises a bearing housing with a bearing arrangement having a bushing arranged around a rotor shaft forming an annular chamber between the shaft and bushing
12/06/2007DE102006026287A1 Zwei-Wellen-Triebwerk für Flugzeuge mit hohem Bedarf an elektrischer Leistung Two-shaft engine for aircraft with a high demand for electrical power
12/06/2007CA2653904A1 Axial flow fluid device
12/06/2007CA2643764A1 Starting a gas turbine engine
12/05/2007EP1863166A1 Double-spool engine for aircraft with high consumption of electrical power
12/05/2007EP1862644A1 Air-flow guiding device at the inlet of the combustor of a turbomachine
12/05/2007EP1862639A1 Device for optimizing cooling in gas turbines
12/05/2007EP1861610A1 Method of operating a gas engine plant and fuel feeding system of a gas engine
12/05/2007EP1861601A2 Gas turbine fuel preparation and introduction method
12/05/2007CN101084367A Ventilating air intake arrangement
12/05/2007CN101084366A Ventilating air intake arrangement with mobile closing device
12/05/2007CN101082345A Bolt-on radial bleed manifold
12/05/2007CN101082307A Device for optimizing cooling in gas turbines
12/05/2007CN100353117C Methods and apparatus for cooling gas turbine combustors
12/05/2007CN100353036C Refrigeration power plant
12/05/2007CN100353035C System for reducing fuel consumption in gas turbine engine
12/05/2007CN100353033C Electrical power generation system and method
12/05/2007CN100353032C Open-cooled component for a gas turbine, combustion chamber, and gas turbine
12/04/2007US7303638 Cold-forming a predetermined, pretreated Ti alloy into a cold-formed shape; subjecting the cold-formed shape to a post-forming annealing cycle comprising: heating the cold-formed shape, holding, cooling the cold-formed shape to room temperature
12/04/2007US7303377 Apparatus and method of balancing a shaft
12/04/2007US7302990 Method of forming concavities in the surface of a metal component, and related processes and articles
12/04/2007CA2479142C Helicopter tactile exceedance warning system
12/04/2007CA2333936C Film cooling strip for gas turbine engine combustion chamber
12/01/2007CA2590113A1 Device for optimizing cooling in gas turbines
12/01/2007CA2590081A1 Thermal-acoustic enclosure
11/2007
11/29/2007WO2007134886A1 Gas turbine engine starting method and control device
11/29/2007WO2007134596A1 Method for treating surfaces of titanium-aluminum alloys with fluoride or fluoride compounds
11/29/2007WO2007134568A1 Modular fuel supply device for a gas turbine
11/29/2007US20070275820 Drive Train With Exhaust Gas Utilization and Control Method
11/29/2007US20070274823 Method For Reducing The Noise Of Turbo Engines
11/29/2007US20070272176 Cylinder Head Cover With Oil Separator
11/29/2007US20070271930 Gas turbine having cooling-air transfer system
11/29/2007US20070271928 Fuel heating system for turbine engines
11/29/2007US20070271927 Method and apparatus for actively controlling fuel flow to a mixer assembly of a gas turbine engine combustor
11/29/2007US20070271900 High humidity gas turbine equipment
11/29/2007DE102006024644A1 Verfahren zur extremen Erhitzung eines Arbeitsfluids unter hohem Druck zum Betreiben einer Wärmekraftmaschine Method for extreme heat a working fluid under high pressure for operating a heat engine
11/29/2007DE102006024085A1 Turboverdichter in Axialbauweise Turbo compressor in axial flow
11/29/2007CA2649330A1 Modular fuel supply device for a gas turbine