| 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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| 05/31/2006 | EP1662147A1 Control device for compressor |
| 05/31/2006 | EP1662117A2 Fuel supply system |
| 05/31/2006 | EP1662116A1 Multiple chamber combustion system for a gas turbine |
| 05/31/2006 | EP1662115A1 Cogeneration system |
| 05/31/2006 | EP1660762A2 Atomization and injection system, and method for operating the same |
| 05/31/2006 | EP1485289B1 Apparatus and method for variation of a wall skin |
| 05/30/2006 | US7052782 High-temperature protection layer |
| 05/30/2006 | US7052737 Determining a temperature range of the substrate subjected to a high temperature up to less than a critical substrate deterioration temperature; combining the indicator and the binder; collecting the indicator released from the binder into an exhaust gas stream passing over; protective devices; turbines |
| 05/30/2006 | US7052240 Rotating seal arrangement for turbine bucket cooling circuits |
| 05/30/2006 | US7052238 Hollow fan blade for gas turbine engine |
| 05/30/2006 | US7052235 Turbine engine shroud segment, hanger and assembly |
| 05/30/2006 | US7052231 Methods and apparatus for injecting fluids in gas turbine engines |
| 05/30/2006 | US7052017 Rotary machine with seal |
| 05/30/2006 | US7051956 Ejector device for direct injection fuel jet |
| 05/30/2006 | US7051746 Valve having pressure balancing piston and method involving same |
| 05/30/2006 | US7051659 Projectile structure |
| 05/30/2006 | US7051534 Gas turbine arrangement having an integrated filter housing and compressor bleed duct |
| 05/30/2006 | US7051533 Method and system for controlling gas turbine engine |
| 05/30/2006 | US7051531 Flow control body |
| 05/30/2006 | US7051530 Burner apparatus for burning fuel and air |
| 05/30/2006 | US7051509 Apparatus for reducing foreign object debris ingestion into aircraft engines |
| 05/30/2006 | US7051435 Process for repairing turbine components |
| 05/30/2006 | CA2338006C Remote monitoring diagnostic system and method thereof |
| 05/30/2006 | CA2207831C Injection system with very high degree of homogenization |
| 05/26/2006 | WO2006053866A1 Burner starting method |
| 05/26/2006 | WO2006025847A3 Fanned trailing edge teardrop array |
| 05/25/2006 | US20060107668 Airfoil with supplemental cooling channel adjacent leading edge |
| 05/25/2006 | US20060107647 Turbine, particularly useful for small aircraft |
| 05/24/2006 | EP1659339A1 Method of starting up a burner |
| 05/24/2006 | EP1659277A1 Device for water or steam injection into the working medium of a gas turbine |
| 05/24/2006 | EP1659264A2 Airfoil with supplemental cooling channel adjacent leading edge |
| 05/24/2006 | EP1658455A2 Fluid-cooled mechanical face seal rotor |
| 05/24/2006 | EP1658422A1 Revolving toroidal motor |
| 05/24/2006 | EP1442203B1 Method for controlling the cooling air mass flows of a gas turbine group |
| 05/24/2006 | EP1269094B1 Method and installation for generating energy |
| 05/24/2006 | EP1204532A4 One-step noble metal-aluminide coatings |
| 05/24/2006 | CN1777748A Anti-detonation fuel delivery system. |
| 05/24/2006 | CN1257656C Device for producing a plasma, ionisation method and use |
| 05/23/2006 | US7048782 Apparatus and process for power recovery |
| 05/23/2006 | US7048507 Axial-flow thermal turbomachine |
| 05/23/2006 | US7048501 Dust collecting filter, dust collecting device, and air intake device for gas turbine |
| 05/23/2006 | US7048500 Silencer for ventilation system and methods |
| 05/23/2006 | US7048497 Gas turbine stator |
| 05/23/2006 | US7048229 Low sonic boom inlet for supersonic aircraft |
| 05/23/2006 | US7047725 Assembly and method for aircraft engine noise reduction |
| 05/23/2006 | CA2491476C An arrangement for sealing a steam-cooled gas turbine |
| 05/23/2006 | CA2294620C Cooling device for a gas turbine speed reducer |
| 05/19/2006 | CA2527352A1 Turbine engine with a decoupling device common to the first and second drive shaft bearings, compressor including the decoupling device and the decoupling device |
| 05/18/2006 | WO2006009971A3 Heat exchanger with header tubes |
| 05/18/2006 | US20060102781 Dual action inlet door and method for use thereof |
| 05/18/2006 | US20060102779 Dual flow APU inlet and associated systems and methods |
| 05/18/2006 | US20060102776 Dual action inlet door and method for use thereof |
| 05/18/2006 | US20060101804 Aircraft engine arrangement |
| 05/18/2006 | CA2526717A1 Multiform film cooling holes |
| 05/17/2006 | EP1656295A1 Device for stabilizing the engine inlet flow in static tests of engines |
| 05/17/2006 | EP1534878B1 Highly oxidation resistant component |
| 05/17/2006 | EP1320664B1 Compressed air steam generator for use in cooling a combustion turbine transition section |
| 05/17/2006 | CN1773092A Device for lubrication of a turbine engine component |
| 05/17/2006 | CN1773079A High efficiency rotor for the first phase of a gas turbine |
| 05/17/2006 | CN1256464C Chemical cleaning solution for gas turbine blades |
| 05/16/2006 | US7044434 High recovery sonic gas valve |
| 05/16/2006 | US7043924 Turbine power plant, installation process and removal process of the turbine power plant |
| 05/16/2006 | US7043922 Method of forming a fuel feed passage in the feed arm of a fuel injector |
| 05/16/2006 | US7043811 Method of removing studs |
| 05/16/2006 | CA2344137C Steam control apparatus for turbine |
| 05/11/2006 | WO2006047991A1 Acoustic absorber for aircraft engines |
| 05/11/2006 | WO2006047854A1 Aspherical dimples for heat transfer surfaces and method |
| 05/11/2006 | US20060096292 Method for determination of the temperature, mass-averaged over a flow cross-section, of a gas flow in a gas turbine |
| 05/11/2006 | US20060096291 Gas turbine engine fuel injector |
| 05/11/2006 | DE10319014B4 Vorrichtung zum Fortbewegen von Gasturbinen oder Modulen einer Gasturbine, insbesondere bei der Wartung A device for displacing gas turbines or modules of gas turbines, especially during maintenance |
| 05/11/2006 | DE102004025692B4 Brazing construction for abradable sealing material used in turbine, includes infiltration prevention agent which is filled on non-brazing side upto specific depth so as to restrict infiltration of brazing filler metals |
| 05/11/2006 | CA2583126A1 Aspherical dimples for heat transfer surfaces and method |
| 05/11/2006 | CA2583103A1 Acoustic absorber for aircraft engines |
| 05/10/2006 | EP1655457A1 Gas turbine engine and method of assembling same |
| 05/10/2006 | EP1474610B1 Warning before pump limit or in case of blade failure on a turbomachine |
| 05/10/2006 | CN1771385A Method of operating a gas turbine group |
| 05/10/2006 | CN1769655A Gas turbine power generating plant |
| 05/10/2006 | CN1769654A Effervescent aerodynamic system for injecting an air/fuel mixture into a turbomachine combustion chamber |
| 05/10/2006 | CN1769653A Element of turbomachinery with cool unit |
| 05/10/2006 | CN1769652A Unit for sealing transition region between two parts cool passage of turbomachinery |
| 05/10/2006 | CN1255623C Gas collecting pipe for transporting hot gas |
| 05/09/2006 | USRE39092 Gas turbine with water injection |
| 05/09/2006 | US7040857 Flexible seal assembly between gas turbine components and methods of installation |
| 05/09/2006 | US7040578 Locking the cowl doors of a turbojet |
| 05/09/2006 | US7040576 Fire shield apparatus and method |
| 05/09/2006 | US7040098 Provision of sealing for the cabin-air bleed cavity of a jet engine using strip-type seals acting in two directions |
| 05/09/2006 | US7040097 Gas turbine and associated cooling method |
| 05/09/2006 | US7040083 Gas turbine having water injection unit |
| 05/09/2006 | US7040082 Assistance and emergency drive for electrically-driven accessories |
| 05/09/2006 | CA2525283A1 Methods and apparatus for cooling gas turbine engine components |
| 05/09/2006 | CA2525189A1 Gas turbine engine fuel injector |
| 05/09/2006 | CA2317681C High-efficiency power generating method |
| 05/04/2006 | WO2006047257A1 Dual-rotor, single input/output starter-generator |
| 05/04/2006 | WO2006046976A2 Turbine system with exhaust gas recirculation and absorption refrigeration system |
| 05/04/2006 | WO2005007509A3 Partitioned exciter system |
| 05/04/2006 | US20060091243 Device for sound attenuation in a flow duct |
| 05/04/2006 | US20060090472 System and method for heating an air intake of turbine engine |
| 05/04/2006 | US20060090471 Method and apparatus for identification of hot and cold chambers in a gas turbine combustor |
| 05/04/2006 | DE102004053383A1 Akustischer Absorber für Flugtriebwerke Acoustic absorber for aircraft engines |
| 05/03/2006 | EP1653074A2 Rocket-ramjet propelled missile |