| 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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| 07/08/2009 | CN201269139Y Engine of miniature thermal aerosol sprayer |
| 07/08/2009 | CN101479455A Turboreactor for aircraft |
| 07/08/2009 | CN101479454A Gas turbine power generation system and method of detecting its calorie abnormality |
| 07/08/2009 | CN100510369C Methods and apparatus for operating gas turbine engines |
| 07/08/2009 | CN100510153C Method of repairing a Ni-based alloy part |
| 07/07/2009 | US7556474 Turbomachine, for example a turbojet for an airplane |
| 07/07/2009 | US7556473 Control unit for compressor |
| 07/07/2009 | US7555906 Mounting system for a flame pipe or liner |
| 07/07/2009 | US7555892 Cooling system for a gas turbine |
| 07/07/2009 | US7555890 Fast start-up combined cycle power plant |
| 07/07/2009 | CA2514480C Configuration and process for carbonyl removal |
| 07/07/2009 | CA2338619C Modified fuel gas turbo-expander for oxygen blown gasifiers and related method |
| 07/04/2009 | CA2648907A1 Composite mating element with machined portion |
| 07/02/2009 | WO2009080904A1 Aircraft nacelle guidance system installation |
| 07/02/2009 | WO2009080142A1 Sealing segment and sealing-segment arrangement |
| 07/02/2009 | US20090169363 Plasma Enhanced Stator |
| 07/02/2009 | US20090166988 Gas turbine with a gap blocking device |
| 07/02/2009 | US20090165995 Air-oil heat exchanger placed at the location of the air separator nose of a turbojet, and a turbojet including such an air-oil heat exchanger |
| 07/02/2009 | US20090165864 Supersonic inlet |
| 07/02/2009 | US20090165464 Jet engine with detachably arranged generator unit |
| 07/02/2009 | US20090165463 Fixing System for a Component of a Turbojet Pod |
| 07/02/2009 | US20090165436 Premixed, preswirled plasma-assisted pilot |
| 07/02/2009 | US20090165435 Dual fuel can combustor with automatic liquid fuel purge |
| 07/02/2009 | DE202009006490U1 Abgasturbolader Exhaust gas turbocharger |
| 07/02/2009 | DE102008055589A1 Duplex-Turbinenleitapparat Duplex turbine nozzle |
| 07/02/2009 | DE102007062699A1 Brennkammerauskleidung Combustor liner |
| 07/02/2009 | CA2705598A1 Aircraft nacelle guidance system installation |
| 07/02/2009 | CA2701748A1 Sealing segment and sealing-segment arrangement |
| 07/01/2009 | EP2075439A2 Modular architecture of gas turbine front end |
| 07/01/2009 | EP2075438A1 Gas turbine |
| 07/01/2009 | EP2075437A2 Multi-source gas turbine cooling |
| 07/01/2009 | EP2075436A2 Ferry flight engine fairing kit |
| 07/01/2009 | EP2075420A2 Method of preparing an engine for transportation |
| 07/01/2009 | EP2075419A2 Gas turbine oil supply system and method for operating a gas turbine store oil supply |
| 07/01/2009 | EP2075194A1 Air-oil exchanger arranged at the air separator nozzle of a jet engine and jet engine including such an air-oil exchanger |
| 07/01/2009 | EP2074298A1 Variable area nozzle assisted gas turbine engine restarting |
| 07/01/2009 | EP2074288A1 Turbofan engine with variable area fan nozzle and low spool generator for emergency power generation and method for providing emergency power. |
| 07/01/2009 | EP1730444B1 Method for the operation of a heat engine, preferably a gas turbine plant |
| 07/01/2009 | CN100507240C 改进的燃料输送系统 Improved fuel delivery system |
| 07/01/2009 | CN100507239C Hybrid engine accessory power system |
| 07/01/2009 | CN100507238C Turbomachine frame structure |
| 07/01/2009 | CN100507237C Gas turbine and associated cooling method |
| 07/01/2009 | CN100507236C Methods and apparatus for injecting fluids in gas turbine engines |
| 07/01/2009 | CN100507235C Method of operating a gas turbine group |
| 07/01/2009 | CN100507234C Turbine shroud asymmetrical cooling elements |
| 07/01/2009 | CN100507233C Cooling system for nozzle segment platform edges |
| 07/01/2009 | CN100507217C Center-located cutter teeth on shrouded turbine blades |
| 06/30/2009 | US7552647 Turbine blade fatigue life evaluating method |
| 06/30/2009 | US7552591 Twin spool turbine engine with power take-off means on the low-pressure and high-pressure rotors, and power take-off module for the turbine engine |
| 06/30/2009 | US7552590 Tube-type vortex reducer |
| 06/30/2009 | CA2398319C Bladed rotor disc side-plate and corresponding arrangement |
| 06/30/2009 | CA2363201C Internal casing for stator |
| 06/28/2009 | CA2647758A1 Method of preparing an engine for ferry flight |
| 06/28/2009 | CA2647753A1 Ferry flight engine fairing kit |
| 06/27/2009 | CA2648866A1 Air/oil exchanger placed at the air separator nose of a turbojet and a turbojet including said air/oil exchanger |
| 06/25/2009 | WO2009077666A2 Piezoelectric de-icing of an air inlet |
| 06/25/2009 | US20090158746 Method of Regulation of the Temperature of Hot Gas of a Gas Turbine |
| 06/25/2009 | DE102008060429A1 Rotationsbewegliche Lufteinlassklappe für APU-Einheit Rotation Movable air inlet flap for APU unit |
| 06/25/2009 | DE102008055545A1 Verfahren und Vorrichtung zum Hochfahren eines Kombinationszyklus-Stromerzeugungssystems Method and apparatus for booting a combined cycle power generation system |
| 06/25/2009 | DE102007061290A1 Method for removing a coating from a component comprises preparing the relative movement between the component and a high pressure water jet so that layer removal occurs along first and second parallel processing units |
| 06/25/2009 | CA2700187A1 Piezoelectric de-icing of an air inlet |
| 06/24/2009 | EP2072781A2 Method for the controlled purging of the fuel feeding system in the combustor of a gas turbine engine |
| 06/24/2009 | EP2072780A2 A fuel distribution apparatus |
| 06/24/2009 | EP2072779A2 Fan nacelle flow control and method of controlling a boundary layer at the inlet of a fan nacelle |
| 06/24/2009 | EP2072397A2 Intermediate casing extension for an aircraft jet engine, comprising a sectorised annular groove for receiving nacelle covers |
| 06/24/2009 | EP2072396A2 Intermediate casing for an aircraft jet engine with improved design |
| 06/24/2009 | CN101463764A High-energy plasma igniter of gas turbine |
| 06/24/2009 | CN101463763A Magnetically stabilized plasma flow ignition generator |
| 06/24/2009 | CN101463762A Continuous plasma flow ignition exciter |
| 06/23/2009 | US7549282 Multi-slot inter-turbine duct assembly for use in a turbine engine |
| 06/23/2009 | CA2397455C Preferential multihole combustor liner |
| 06/21/2009 | CA2647570A1 Heat exchange system in a turbomachine |
| 06/21/2009 | CA2647179A1 Process and system for characterizing and counting overshoots by an operating parameter of an aircraft engine |
| 06/21/2009 | CA2646685A1 Method for controlling the consumption and for detecting leaks in the lubrication system of a turbine engine |
| 06/21/2009 | CA2646663A1 Recirculation valve in an aircraft engine |
| 06/20/2009 | CA2647351A1 Method for controlling the load variations in a gas turbine |
| 06/20/2009 | CA2647262A1 Method for the controlled purging of the fuel feeding system in the combustor of a gas turbine |
| 06/18/2009 | WO2009075897A2 Methods and systems for generating power from a turbine using pressurized nitrogen |
| 06/18/2009 | WO2009075721A2 Sequential combustion firing system for a fuel system of a gas turbine engine |
| 06/18/2009 | WO2009075335A1 Gas turbine controlling method, and gas turbine power generating apparatus |
| 06/18/2009 | WO2008105831A3 Turbine engine, seal therefor and method of removing a seal from a turbine engine |
| 06/18/2009 | WO2008045051A3 Gas turbine nacelle comprising a passive boundary lazer bleed system and method of controlling turbulent airflow |
| 06/18/2009 | US20090155053 Turbine cooling flow modulation |
| 06/18/2009 | US20090155051 Duplex turbine shroud |
| 06/18/2009 | US20090151362 Motor drive architecture for high frequency ac bus |
| 06/18/2009 | US20090151361 Device for guiding an element in an orifice in a wall of a turbomachine combustion chamber |
| 06/18/2009 | US20090151359 Turbomachine combustion chamber |
| 06/18/2009 | US20090151358 Turbine Engine Combustor |
| 06/18/2009 | US20090151314 Fluid system |
| 06/18/2009 | DE102007060226A1 Axiallager Thrust bearings |
| 06/18/2009 | DE102007060043A1 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine |
| 06/17/2009 | EP2071156A1 Fuel distribution system for a gas turbine with multistage burner arrangement |
| 06/17/2009 | EP2071155A2 Nacelle assembly with turbulators |
| 06/17/2009 | EP2071141A1 Watertigh fixing of a bearing support in a turbomachine |
| 06/17/2009 | EP2071140A2 On-demand lubrication system and method for improved flow management and containment |
| 06/17/2009 | EP2071139A2 Bearing mounting system in a low pressure turbine |
| 06/17/2009 | EP2069625A2 Device for improving the effectiveness of acoustic treatments in an aircraft drive duct |
| 06/17/2009 | EP2069624A1 Removable air intake structure for turbojet engine nacelle |
| 06/16/2009 | US7547478 Article including a substrate with a metallic coating and a protective coating thereon, and its preparation and use in component restoration |
| 06/16/2009 | US7546742 Gas turbine engine assembly and method of assembling same |