Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
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)
12/2012
12/06/2012US20120304650 Injection system for a turbomachine combustion chamber, including air injection means improving the air-fuel mixture
12/06/2012US20120304649 Fuel injector
12/06/2012US20120304648 Integrated late lean injection on a combustion liner and late lean injection sleeve assembly
12/06/2012US20120304646 Method and apparatus for repairing an engine component
12/06/2012DE102011103731A1 Verfahren zum Aufbringen einer Schutzschicht, mit einer Schutzschicht beschichtetes Bauteil und Gasturbine mit einem solchen Bauteil A method for applying a protective layer, coated with a protective layer component and gas turbine with such a component
12/06/2012DE102011103163A1 Gasturbinentriebwerk mit teleskopartigem Lufteinlass der Triebwerksverkleidung Gas turbine engine with telescopic air intake of the engine cowling
12/06/2012DE102011103158A1 Flight gas turbine for aircraft, has bearing element with ring encompassing picollo tube elements and elastically deformed in axial direction relative to engine axis, and carrier element extended parallel to axis of tube elements
12/06/2012DE102010007567B4 Kerndiffusor Core diffuser
12/06/2012DE102009032685B4 Vormontierte Ventilbaugruppe zur Verwendung in einem Turbolader Preassembled valve assembly for use in a turbocharger
12/06/2012DE102005019652B4 Turbulator auf der Unterseite einer Turbinenschaufelspitzenumleitbiegung Turbulator on the underside of a Turbinenschaufelspitzenumleitbiegung
12/06/2012CA2837258A1 Turbomachine fan case
12/06/2012CA2778592A1 Clamping system and method for thrust reverser attachment
12/05/2012EP2530282A1 Dual drive of an accessory drive gearbox
12/05/2012EP2530281A2 Gearbox mount bracket
12/05/2012EP2530280A2 Fuel air heat exchanger
12/05/2012EP2530279A1 Split ring cooling structure and gas turbine
12/05/2012EP2529923A1 Polymer composite materials and processes therefor
12/05/2012EP2529877A1 Method and apparatus for repairing an engine component
12/05/2012EP2529084A2 Turbine including seal air valve system
12/05/2012DE202012011308U1 Lagergehäuse eines Abgasturboladers An exhaust gas turbocharger bearing housing
12/05/2012CN202578915U 冷却装置 Cooling device
12/05/2012CN1467407B Gas turbine engine combustor can with trapped vortex cavity
12/05/2012CN102809389A Instrumentation rake assembly
12/05/2012CN102808698A Formed flexible seal
12/05/2012CN102808697A System for mounting combustor transition piece to frame of gas turbine engine
12/05/2012CN101691848B Radial work rotor engine
12/05/2012CN101265842B Improved system and method for reducing NOx emission
12/04/2012US8324746 Variable drive gas turbine engine
12/04/2012US8322982 Vane fixing apparatus and method
12/04/2012US8322146 Transition duct assembly
12/04/2012US8322145 Systems and methods for providing surge protection to a turbine component
12/04/2012US8322126 Gas turbine exhaust assembly
12/04/2012US8322125 Turbo-engine compressor tip comprising de-icing means
12/04/2012CA2601934C Gas turbine combustor exit duct and hp vane interface
12/04/2012CA2550885C Process for controlling the profile of the blend between the cylindrical part and the relief of a roll to offset the bearing of a turbine engine
12/04/2012CA2511844C Aircraft engine low-pressure compressor stiffener
12/04/2012CA2500970C Protection system for main motor shaft with integrated bearing
11/2012
11/30/2012CA2778521A1 Aircraft engine cowl and process therefor
11/30/2012CA2776637A1 Dual input drive agb for gas turbine engines
11/30/2012CA2776162A1 Integrated fuel nozzle and ignition assembly for gas turbine engines
11/29/2012WO2012161905A2 Thermally compliant support for a combustion system
11/29/2012WO2012161142A1 Hollow curved plate, method for manufacturing same, and burner for gas turbine
11/29/2012WO2012160819A1 Turbine rotor blade and steam turbine
11/29/2012WO2012160586A1 Casing shroud for turbo machine
11/29/2012WO2012160375A1 A structural element of an air vehicle air intake composed of an array of passages with a hexagonal cross section
11/29/2012WO2012160294A1 Method for rationalising a chain of electric components of an aircraft, implementation architecture and corresponding aircraft
11/29/2012US20120297793 Gas turbine engine
11/29/2012US20120297792 Thermocouple well for a turbomachine
11/29/2012US20120297790 Integrated ceramic matrix composite rotor disk geometry for a gas turbine engine
11/29/2012US20120297789 Flade duct turbine cooling and power and thermal management
11/29/2012US20120297787 Flow straightener and mixer
11/29/2012US20120297785 System and method for flow control in gas turbine engine
11/29/2012US20120297780 Active fuel temperature control
11/29/2012US20120297777 Reheat burner injection system with fuel lances
11/29/2012DE102012208535A1 Motorbaugruppe mit turbolader Motor assembly with turbocharger
11/29/2012DE102011102598A1 Method for manufacturing honeycomb seal for turbo engine for sealing radial gap between rotor and stator, involves manufacturing piece as forging part by multiple sealing segments
11/29/2012DE102011102458A1 Enteisungsvorrichtung eines Fluggasturbinentriebwerks The de-icer of an aircraft gas turbine engine
11/29/2012DE102011076587A1 Abgasturbolader mit einem Kugelhahn-Wastegate-Ventil mit spannungsentlastetem Kurbelarm Turbocharger with a ball valve wastegate valve with stress-relieved crank arm
11/29/2012CA2836027A1 Method for rationalising a chain of electric components of an aircraft, implementation architecture and corresponding aircraft
11/28/2012EP2527619A1 Insert removal device for gas turbine stationary blade and insert removal method for gas turbine stationary blade
11/28/2012EP2527253A1 De-icing device for an aviation gas turbine engine
11/28/2012EP2527077A1 Method for repairing wall member with passage
11/28/2012EP2526302A1 Turbine inlet flow modulator
11/28/2012CN202560376U Novel gas turbine rectification support
11/28/2012CN102803682A Filter element support assembly, quick installation system, and methods
11/28/2012CN102803660A Optical monitoring system for a turbine engine
11/28/2012CN102803528A Nickel-base Single-crystal Superalloy And Turbine Wing Using Same
11/28/2012CN102797565A Vortex composite heat engine
11/28/2012CN101626862B Method of repair
11/27/2012US8316648 Method and apparatus for controlling a heating value of a low energy fuel
11/27/2012US8316647 System and method employing catalytic reactor coatings
11/27/2012CA2512375C Turbojet with means of protection for a fuel injection unit, the injection unit and the turbojet undershield
11/22/2012WO2012159067A1 Lean direct fuel injector
11/22/2012WO2012157527A1 Turbine stator vane
11/22/2012WO2012157498A1 Gas turbine engine
11/22/2012WO2012156637A1 Device for de-icing a turbomachine separator
11/22/2012WO2012156520A1 A gas turbine system and corresponding method for assembling this system
11/22/2012WO2012155521A1 Substrate for air intake throttle and air intake throttle comprising the substrate
11/22/2012WO2011163289A3 Secondary water injection for diffusion combustion systems
11/22/2012US20120292862 Turbine seals
11/22/2012US20120292861 Turbine combustion system transition piece side seals
11/22/2012US20120292860 Turbine combustion system transition seals
11/22/2012US20120291452 Thermally compliant support for a combustion system
11/22/2012US20120291451 Structural frame for gas turbine combustion cap assembly
11/22/2012US20120291450 Auxiliary power unit mounting feature
11/22/2012US20120291448 Flexible Combustor Fuel Nozzle
11/22/2012US20120291447 Combustor nozzle and method for supplying fuel to a combustor
11/22/2012US20120291446 Combustor
11/22/2012US20120291445 Method for operating a gas turbine power plant with exhaust gas recirculation
11/22/2012US20120291438 Burner system and method for damping such a burner system
11/22/2012DE102012104283A1 System und Verfahren zur Sicherung von Gasturbinenluftfiltern System and method for securing the gas turbine air filters
11/22/2012DE102011076229A1 Support structure for e.g. supercharger for internal combustion engine of motor vehicle, has resilient deformable prop portion that is elastically deformed due to axial compression stress across preset direction
11/22/2012DE102011075865A1 Brennkammerseitig verschraubte Brennereinsatzplatte Combustion chamber side burner insert screw-plate
11/22/2012CA2836047A1 Gas turbine engine
11/22/2012CA2835341A1 A gas turbine system and corresponding method for assembling this system
11/21/2012EP2525063A1 Seal structure and gas turbine engine provided therewith
11/21/2012EP2524867A2 Method for powering standalone travel motors of an aircraft
11/21/2012CN202545021U Fuel oil spraying device of combustion gas turbine
11/21/2012CN102787914A System and method for securing gas turbine air filters
11/21/2012CN101059102B Variable power nozzle ejector for turbine system
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