| 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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| 04/16/2008 | CN100381677C Gas turbine pressurizing air supply system |
| 04/15/2008 | US7356994 Alignment and positioning system for installing a fuel injector in a gas turbine engine |
| 04/13/2008 | CA2606069A1 Gearbox drive shaft of turbojet accessory machines; modular supplementary machine |
| 04/10/2008 | WO2008041478A1 Method and device for starting and stopping gas turbine |
| 04/10/2008 | WO2008040877A1 Removable air intake structure for turbojet engine nacelle |
| 04/10/2008 | WO2008040118A1 Multi-channel fuel manifold |
| 04/10/2008 | US20080083229 Combustor nozzle for a fuel-flexible combustion system |
| 04/10/2008 | DE102007025006A1 Double shaft gas turbine, has bars arranged along circumference of bearing housing and extend via circular intermediate channel into space between outer circumference surface of housing and inner circumference surface of housing wall |
| 04/10/2008 | DE102006039608A1 Anordnung zur Energieentnahme bei einem Zwei-Wellen-Triebwerk Arrangement for energy extraction in a two-shaft engine |
| 04/10/2008 | DE102004002712B4 Turbinenschaufel-Ermüdungslebensdauer-Bewertungsverfahren und Turbinenschaufel-Kriechdehnungsverformungs-Messvorrichtung Turbine blade fatigue life assessment procedures and turbine blade Kriechdehnungsverformungs measuring device |
| 04/10/2008 | CA2665353A1 Multi-channel fuel manifold |
| 04/10/2008 | CA2664034A1 Removable air intake structure for turbojet engine nacelle |
| 04/09/2008 | EP1908942A2 Gas turbine engine assembly and method of assembling same |
| 04/09/2008 | EP1908941A2 Gas turbine engine assembly and method of assembling same |
| 04/09/2008 | EP1908940A2 Multi-conduit fuel manifold |
| 04/09/2008 | EP1908939A2 Adaptive inertial particle separator |
| 04/09/2008 | EP1908938A2 Gas turbine engine shaft assembly |
| 04/09/2008 | EP1907281A1 Propulsion unit for aircraft and aircraft comprising at least one such propulsion unit |
| 04/09/2008 | EP1529181B1 Gas turbine combustion chamber |
| 04/09/2008 | CN100380046C Gasifying combined power generating apparatus |
| 04/09/2008 | CN100379958C Temperature adjusting method of hot gas of a gas turbine |
| 04/09/2008 | CN100379949C Uniaxial combined circulation power-plant |
| 04/09/2008 | CN100379947C Structure for connecting or space sealing members with different thermal expansion coefficients |
| 04/09/2008 | CN100379946C Rotor insert assembly and method of retrofitting |
| 04/09/2008 | CN100379944C Method and apparatus for turbine nozzle locking piece |
| 04/09/2008 | CA2604630A1 Method and system for reducing power plant emissions |
| 04/08/2008 | US7353656 Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 04/08/2008 | US7353655 Method and apparatus for achieving power augmentation in gas turbine using wet compression |
| 04/08/2008 | US7353654 Method and apparatus for achieving power augmentation in gas turbines using wet compression |
| 04/08/2008 | US7353647 Methods and apparatus for assembling gas turbine engines |
| 04/06/2008 | CA2605952A1 Fuel injector for a gas turbine engine combustion chamber |
| 04/06/2008 | CA2605108A1 An oil distributing unit |
| 04/05/2008 | CA2603494A1 Air seal arrangement for a gas turbine engine |
| 04/03/2008 | WO2008038497A1 Gas turbine |
| 04/03/2008 | US20080078183 Liquid fuel enhancement for natural gas swirl stabilized nozzle and method |
| 04/03/2008 | US20080078182 Premixing device, gas turbines comprising the premixing device, and methods of use |
| 04/03/2008 | US20080078181 Methods and apparatus to facilitate decreasing combustor acoustics |
| 04/03/2008 | US20080078180 Methods and apparatus for injecting fluids into a turbine engine |
| 04/03/2008 | US20080078159 Wet Active Chevron Nozzle For Controllable Jet Noise Reduction |
| 04/03/2008 | DE102007044727A1 Verfahren und Geräte für die Herstellung von Turbinenantrieben Methods and apparatus for the manufacture of turbine engines |
| 04/03/2008 | DE102006044968A1 Eintrittskonus für ein Strahltriebwerk Inlet cone for a jet engine |
| 04/02/2008 | EP1906091A2 Flow divider valve |
| 04/02/2008 | EP1906008A2 Engine starter-generator optimized for start function |
| 04/02/2008 | EP1905985A2 Internal fuel manifold having temperature reduction feature |
| 04/02/2008 | EP1905984A2 Components for a gas turbine engine |
| 04/02/2008 | EP1905948A1 Power recovery machine |
| 04/02/2008 | EP1904731A1 Gas and steam turbine installation and method for operating the same |
| 04/02/2008 | CN101153559A Gas turbine engine assembly and method of assembling same |
| 04/02/2008 | CN101153558A Premixing device, gas turbines comprising the premixing device, and methods of use |
| 04/02/2008 | CN100378308C Impeller-pressurizing rotor-injection type steam turbine |
| 04/02/2008 | CA2602994A1 Annular gas turbine engine case and method of manufacturing |
| 04/02/2008 | CA2602981A1 Annular gas turbine engine case and method of manufacturing |
| 04/02/2008 | CA2601659A1 Annular gas turbine engine case and method of manufacturing |
| 04/01/2008 | US7351030 Connection device for making a connection between a turbomachine nozzle and a feed enclosure for feeding cooling fluid to injectors |
| 04/01/2008 | US7350747 Engine mounting structure under an aircraft wing |
| 04/01/2008 | CA2363306C Process for increasing the life of rotor blade attachments |
| 04/01/2008 | CA2329715C Containment system for containing blade burst |
| 04/01/2008 | CA2284363C Thermal barrier coating systems and materials |
| 03/28/2008 | CA2604455A1 Self-contained electrostatic air/oil separator for aircraft engine |
| 03/28/2008 | CA2604453A1 Oil scavenge system for gas turbine engine bearing cavity |
| 03/28/2008 | CA2600171A1 Labyrinth seal repair |
| 03/27/2008 | WO2008034425A1 Intake cone for a jet engine |
| 03/27/2008 | WO2008034227A1 Internal fuel manifold having temperature reduction feature |
| 03/27/2008 | US20080075879 metal substrate, metal bonding layer, ceramics thermal barrier; columnar structure of stabilized zirconia, or ZrO2-HfO2 solid solution; simultaneously melting two ZrO2 deposition and Lanthanum oxide deposition materials by electron beam physical vapor deposition; low thermal conductivity; durability |
| 03/27/2008 | US20080072606 Adaptive inertial particle separators and methods of use |
| 03/27/2008 | US20080072605 Method for control of thermoacoustic instabilities in a combustor |
| 03/27/2008 | DE19821889B4 Verfahren und Vorrichtung zur Durchführung von Reparatur- und/oder Wartungsarbeiten im Innengehäuse einer mehrschaligen Turbomaschine Method and apparatus for performing repair and / or maintenance in the inner casing of a multi-layered turbomachine |
| 03/27/2008 | DE102007045138A1 Laufschaufel-Rückhaltesystem für ein Gasturbinentriebwerk A blade retention system for a gas turbine engine |
| 03/27/2008 | DE102007045053A1 Mischlochanordnung und Verfahren zur Verbesserung der Homogenität eines Brennstoff-Luft-Gemisches in einer Brennkammer Mixing hole arrangement and method for improving the homogeneity of a fuel-air mixture in a combustion chamber |
| 03/27/2008 | DE102007042530A1 Dehnungsverbindung für Gasturbinen Expansion joint for gas turbines |
| 03/27/2008 | CA2664107A1 Inlet cone for a jet engine |
| 03/27/2008 | CA2604367A1 Bleed holes oriented with gaspath and flared for noise reduction |
| 03/27/2008 | CA2604365A1 Oil feed assembly |
| 03/27/2008 | CA2602325A1 Gas turbine engine assembly and method of assembling same |
| 03/27/2008 | CA2602322A1 Gas turbine engine assembly and method of assembling same |
| 03/27/2008 | CA2602313A1 Gas turbine engine assembly and method of assembling same |
| 03/27/2008 | CA2601652A1 Adaptive inertial particle separators and methods of use |
| 03/26/2008 | EP1903212A2 Starter-generator operable with multiple variable frequencies and voltages |
| 03/26/2008 | EP1903188A2 System and method for augmenting turbine power output |
| 03/26/2008 | EP1902953A1 Device for soundproofing a gas turbine helicopter engine and engine obtained using same |
| 03/26/2008 | EP1902948A1 Gas turbine helicopter engine with reduced sound emissions due to acoustic treatment of a jet pump |
| 03/26/2008 | EP1753938B1 A support structure in a turbine or compressor device and a method for assembling the structure |
| 03/26/2008 | CN101149019A Gas turbine helicopter engine soundproofing device and the resulting engine |
| 03/26/2008 | CN101149018A Pulsation type turbine shaft engine |
| 03/26/2008 | CA2604278A1 Method of manufacturing a heat shield for a fuel manifold |
| 03/26/2008 | CA2604272A1 Heat shield for fuel manifold |
| 03/25/2008 | US7347661 Casing arrangement |
| 03/25/2008 | US7347052 Methods and systems for processing uncalcined coke |
| 03/25/2008 | US7347050 Fuel metering unit |
| 03/25/2008 | CA2604106A1 Tower shaft (uts) shielding |
| 03/25/2008 | CA2430106C Gas turbine and method of bleeding gas therefrom |
| 03/22/2008 | CA2603595A1 Heat shield with stress relieving feature |
| 03/20/2008 | WO2008032806A1 Heat resistant member |
| 03/20/2008 | WO2008031195A1 Access housing for gas turbine engine |
| 03/20/2008 | US20080069959 Thermal barrier composition, a superalloy machine part provided with a coating having such a composition, a ceramic coating, and a method of fabricating the coating |
| 03/20/2008 | US20080066470 Advanced hydrogen auxiliary power unit |
| 03/20/2008 | US20080066443 Gas turbine plant for a working medium in the form of a carbon dioxide/water mixture |
| 03/20/2008 | CA2663247A1 Power recovery machine |
| 03/20/2008 | CA2602179A1 Gas turbine helicopter engine soundproofing device and the resulting engine |
| 03/20/2008 | CA2602172A1 Blowing conduit for a turbine engine |