| 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) |
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| 03/20/2008 | CA2602168A1 Gas turbine helicopter engine with noise emission reduced through acoustical treatment of an eductor |
| 03/20/2008 | CA2602141A1 Integrated propellant system that includes a by-pass engine |
| 03/19/2008 | EP1899648A2 Molding compound for producing a refractory lining |
| 03/19/2008 | EP1899593A1 System for defrosting the leading edge sheath of an air inlet hood for a turboengine |
| 03/19/2008 | EP1392957A4 Abradeable seal system |
| 03/19/2008 | CN101146991A Method of operating a gas engine plant and fuel feeding system of a gas engine |
| 03/19/2008 | CN101146930A Surface treatment method and repair method |
| 03/19/2008 | CN101146652A Jig |
| 03/19/2008 | CN101144430A Tower type flame holder for rotor engine |
| 03/19/2008 | CN101144429A Thermoelectrically cooled components for distributed electronics control system for gas turbine engines |
| 03/19/2008 | CN101143283A Method of processing volatile organic compound, adsorption and desorption apparatus, and system for processing volatile organic compound |
| 03/18/2008 | US7344107 Dual flow APU inlet and associated systems and methods |
| 03/18/2008 | US7343746 Method of chilling inlet air for gas turbines |
| 03/18/2008 | US7343745 Gas turbine combustor and operating method thereof |
| 03/18/2008 | US7343676 Method of restoring dimensions of an airfoil and preform for performing same |
| 03/18/2008 | CA2351281C Link component for aircraft engine mounting systems |
| 03/13/2008 | WO2008028274A1 Thrust bearing housing for a gas turbine engine |
| 03/13/2008 | US20080060346 Method for Removing and Recovering Co2 from an Exhaust Gas |
| 03/13/2008 | US20080060341 Turbine engine with semi-fixed turbine driving a receiver controlled so as to preserve a roughly constant rotation speed |
| 03/13/2008 | US20080060325 Single/multiple guard(s)/cap(s) and/or screen(s) with engine attached apparatus and/or pole with rotational system(s) - centrifuge chamber/manifold particle collector |
| 03/13/2008 | US20080060324 Single/multiple guards(s)cap(s) and/or screen(s) with engine attached apparatus and/or pole with rotational system(s) centrifuge chamber/manifold particle collector |
| 03/13/2008 | CA2661874A1 Device for improving the effectiveness of acoustic treatments in an aircraft drive duct |
| 03/12/2008 | EP1898073A2 Assembly for extracting energy from a double-shaft engine |
| 03/12/2008 | EP1898072A1 Drive device for the rotor of an auxiliary equipment of a turbine engine |
| 03/12/2008 | EP1898071A2 Generator-starter assembly for a multi-shaft driving mechanism |
| 03/12/2008 | EP1898070A2 System and apparatus for enclosing equipment |
| 03/12/2008 | EP1898069A2 Turbofan bypass duct air cooled fluid cooler installation |
| 03/12/2008 | EP1898068A2 Gas turbine engine with particulate matter removal |
| 03/12/2008 | EP1898066A2 Gas turbine system |
| 03/12/2008 | EP1897806A2 System for washing an aero gas turbine engine |
| 03/12/2008 | EP1896708A1 Method for increasing aerodynamic stability of a working fluid of a compressor |
| 03/12/2008 | EP1896157A2 Particle separator for a gas turbine engine |
| 03/12/2008 | EP1797284B1 Method and module for a predicted start-up of steam turbines |
| 03/12/2008 | EP1759103B1 Method for operating a gas turbine compressor while cooling the compressor intake air by evaporation |
| 03/12/2008 | CN100374697C Turbocharger |
| 03/12/2008 | CA2599786A1 Combustor with enhanced cooling access |
| 03/11/2008 | US7341380 Installation layout for two coaxial shaft lines |
| 03/11/2008 | US7340903 Scalable power generation using a pulsed detonation engine |
| 03/11/2008 | US7340902 Method for operating an air-breathing engine |
| 03/11/2008 | US7340901 Control logic for fuel controls on APUs |
| 03/11/2008 | US7340882 Turbomachine with means for axial retention of the rotor |
| 03/11/2008 | US7340881 Gas turbine combustor |
| 03/11/2008 | CA2598326A1 Seal system for an interturbine duct within a gas turbine engine |
| 03/08/2008 | CA2600823A1 Integral tandem bearing for high speed flexible shafts |
| 03/08/2008 | CA2598329A1 Rim seal for a gas turbine engine |
| 03/06/2008 | WO2008006960A3 Turbine engine for aircraft |
| 03/06/2008 | WO2008003571A3 Method for operating a gas turbine and gas turbine for carrying out said method |
| 03/06/2008 | WO2007127329A3 Turbine generator |
| 03/06/2008 | WO2007051137A8 Methods and apparatus for a fluid inlet |
| 03/06/2008 | US20080057254 Turbine element repair |
| 03/06/2008 | US20080054739 Generator-starter arrangement for a gas-turbine engine |
| 03/06/2008 | US20080053107 Slidable spring-loaded transition-to-turbine seal apparatus and heat-shielding system, comprising the seal, at transition/turbine junction of a gas turbine engine |
| 03/06/2008 | US20080053106 Methods and systems for removably securing reusable parts to replaceable parts |
| 03/06/2008 | DE102006041325A1 Generator-Starter-System für ein Mehrwellentriebwerk Generator-starter system for a multi-shaft engine |
| 03/06/2008 | DE102006041323A1 Generator-Starter-Anordnung für ein Gasturbinentriebwerk Generator-starter assembly for a gas turbine engine |
| 03/06/2008 | DE102006041321A1 Housing section, particularly fan housings, for gas-turbine engine, has endangered section seperated by shovel or rotor parts in which flexible protective cover arranged is arranged at periphery of matrixes |
| 03/05/2008 | EP1895141A2 Splitter for a turbo-fan engine |
| 03/05/2008 | EP1895125A2 Generator-starter assembly for gas turbine driving mechanism |
| 03/05/2008 | EP1895124A2 Oil cooling apparatus in fan cowling and method therefor |
| 03/05/2008 | EP1895123A2 De-icing of turbine engine inlet and cooling of lubricant |
| 03/05/2008 | EP1895122A1 Modular turbine engine |
| 03/05/2008 | EP1893862A2 Particle separators for a gas turbine engines |
| 03/05/2008 | EP1893858A2 Reformer and reforming process for production of hydrogen from hydrocarbon fuel |
| 03/05/2008 | EP1893857A2 Clustered inlet particle separator |
| 03/05/2008 | EP1893484A2 Anti-icing and de-icing system for aircraft engine pod with resistive mat |
| 03/05/2008 | EP1646776B1 Aircraft turbine engine arrangement |
| 03/05/2008 | EP1633935A4 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 03/05/2008 | CN101135462A Method and apparatus for cooling gas turbine engine combustors |
| 03/05/2008 | CN101135268A Heat pipe-based cooling apparatus and method for turbine engine |
| 03/05/2008 | CN101135250A Heat pipe-based cooling apparatus and method for turbine engine |
| 03/05/2008 | CN101134508A Fan exhaust nozzle for turbofan engine |
| 03/04/2008 | US7340319 Method and system for maintaining an aircraft engine |
| 03/04/2008 | US7338259 High modulus metallic component for high vibratory operation |
| 03/04/2008 | US7337875 High admittance acoustic liner |
| 03/04/2008 | US7337761 Fuel system |
| 03/04/2008 | US7337614 Engine fueling method |
| 03/04/2008 | US7337605 Thermal management for aircraft auxiliary power unit compartment |
| 02/29/2008 | CA2599816A1 Improved fuel injection system and method of assembly |
| 02/29/2008 | CA2599039A1 Device for driving the rotor of a turbine engine ancillary |
| 02/29/2008 | CA2598738A1 Bypass lip seal |
| 02/29/2008 | CA2598261A1 Sleeve and housing assembly and method of adhesively bonding sleeve to housing |
| 02/29/2008 | CA2598260A1 Repairable labyrinth seal |
| 02/29/2008 | CA2598259A1 Simple axial retention feature for abradable members |
| 02/29/2008 | CA2597658A1 Heat transfer system and method for turbine engine using heat pipes |
| 02/29/2008 | CA2597454A1 Heat pipe-based cooling apparatus and method for turbine engine |
| 02/28/2008 | WO2007146246A3 Dual starter/generator for aircraft engine |
| 02/28/2008 | US20080051977 Method of controlling a recuperated turbine engine |
| 02/28/2008 | US20080047275 Methods and systems for operating a gas turbine |
| 02/28/2008 | US20080047238 Single/multiple guard(s)/cap(s) and/or screen(s) with engine attached apparatus and/or pole with rotational system(s) - centrifuge chamber/manifold particle collector |
| 02/28/2008 | DE10325311B4 Kraftstoffkreiselpumpe Fuel centrifugal pump |
| 02/27/2008 | CN101131123A Multifunctional air inlet of turbine engine |
| 02/27/2008 | CN100371580C Long service life jet deflection plate for turbine jet motor of aircraft |
| 02/27/2008 | CN100371560C Low-pressure turbine casing and cover assembly |
| 02/27/2008 | CN100371126C Repairing method of turbine inlet guiding section |
| 02/26/2008 | US7335999 Fluid actuated rotating device including a low power generator |
| 02/26/2008 | US7335616 Target for vaporizing under an electron beam, a method of fabricating it, a thermal barrier and a coating obtained from a target, and a mechanical part including such a coating |
| 02/26/2008 | US7334413 Apparatus, system and method for observing combustion conditions in a gas turbine engine |
| 02/26/2008 | US7334412 Cooling air and injected liquid system for gas turbine blades |
| 02/26/2008 | US7334411 Gas turbine heat exchanger assembly and method for fabricating same |
| 02/26/2008 | US7334408 Combustion chamber for a gas turbine with at least two resonator devices |