| 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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| 12/11/2008 | WO2008149731A1 Integrated gasification combined cycle plant |
| 12/11/2008 | WO2008148999A2 Exhaust system for gas turbine |
| 12/11/2008 | US20080304958 Gas turbine engine with air and fuel cooling system |
| 12/11/2008 | US20080302107 Method of and power plant for generating power by oxyfuel combustion |
| 12/11/2008 | US20080302105 Combustor of a gas turbine engine |
| 12/11/2008 | US20080302082 Power transmission arrangement |
| 12/11/2008 | CA2635034A1 Connecting system including safety attachment means |
| 12/10/2008 | EP2000648A2 Cooling device for a gas turbine engine and corresponding gas turbine engine |
| 12/10/2008 | EP1999022A1 Air inlet shroud structure |
| 12/10/2008 | EP1999021A1 Air inlet lip for a pod with electric defrosting |
| 12/10/2008 | EP1999020A1 Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone |
| 12/10/2008 | CN101321940A Gas turbine engine auxiliary component mount |
| 12/10/2008 | CN101319633A Displacement-increased distribution apparatus used for backheating type air turbine and gas turbine |
| 12/10/2008 | CN100441740C Highly oxidation resistant component |
| 12/09/2008 | US7461815 Suspension system for a rotary wing aircraft engine |
| 12/09/2008 | US7461814 Dual action inlet door and method for use thereof |
| 12/09/2008 | US7461510 Gas turbine electric powerplant |
| 12/09/2008 | US7461509 Method and system for determining lean blow out condition for gas turbine combustion cans |
| 12/09/2008 | CA2538806C Annular acoustic panel |
| 12/09/2008 | CA2279558C Sealing arrangement with automatic clearance adjustment |
| 12/04/2008 | WO2008146818A1 Method of preparing through holes in tube body wall surfaces, and tube body structure |
| 12/04/2008 | WO2008146579A1 Gas turbine engine |
| 12/04/2008 | US20080295519 Turbine engine fuel injector with Helmholtz resonators |
| 12/04/2008 | DE102008002863A1 Dichtungsring mit Schwalbenschwanzformabschnitt Seal ring with dovetail section |
| 12/04/2008 | DE102007025131A1 Ladeeinrichtung Loader |
| 12/04/2008 | CA2818043A1 Gas turbine engine |
| 12/04/2008 | CA2682570A1 Gas turbine engine |
| 12/03/2008 | EP1998036A2 Resonance driven glow plug torch igniter and ignition method |
| 12/03/2008 | EP1998029A2 Nacelle for an aircraft engine with inlet flow control system and corresponding operating method |
| 12/03/2008 | EP1998028A2 Nacelle for an aircraft engine with inlet flow control system and corresponding operation method |
| 12/03/2008 | EP1998027A2 Gas turbine engine comprising a nacelle compartment plenum for bleed air flow delivery system |
| 12/03/2008 | EP1998005A2 Charging device |
| 12/03/2008 | EP1997923A1 Ni-BASE SUPERALLOY, METHOD FOR PRODUCING SAME, AND TURBINE BLADE OR TURBINE VANE COMPONENT |
| 12/03/2008 | EP1997548A1 Suction filter |
| 12/03/2008 | CN201159118Y Energy induction type complete combustion device |
| 12/03/2008 | CN101317000A Gas turbine enginge filter cleaning system and method of operation |
| 12/03/2008 | CN101315033A Shroud configuration having sloped seal |
| 12/03/2008 | CN100439657C Return blade rotary machinery using same |
| 12/03/2008 | CN100439567C Method for producing abrasive tips for gas turbine blades ` |
| 12/02/2008 | US7458773 Turbomachine with contrarotating fans |
| 12/02/2008 | US7458771 Retaining of centering keys for rings under variable angle stator vanes in a gas turbine engine |
| 11/27/2008 | WO2008142287A2 Method and system for starting a turboshaft engine by cold weather |
| 11/27/2008 | WO2008059371A3 Bearing structure of turbocharger |
| 11/27/2008 | US20080289342 Method and Apparatus for Spectroscopic Measurements in the Combustion Zone of a Gas Turbine Engine |
| 11/27/2008 | US20080289341 Combustor of Gas Turbine |
| 11/27/2008 | US20080289339 Method and apparatus for controlling the combustion in a gas turbine |
| 11/27/2008 | US20080289338 High Efficiency 2-Stage Fuel Pump and Control Scheme for Gas Turbines |
| 11/27/2008 | US20080289313 Direct heating organic rankine cycle |
| 11/27/2008 | DE102008023426A1 Verfahren und Vorrichtung für den Betrieb von Gasturbinentriebwerken Method and apparatus for operating gas turbine engines |
| 11/27/2008 | DE102005060628B4 Verfahren zur Erzeugung eines Prozessstromes A method for producing a process stream |
| 11/27/2008 | CA2681929A1 Method and system for starting a turboshaft engine by cold weather |
| 11/26/2008 | EP1994269A1 Integration of a starter/generator module in a gas turbine transmission housing |
| 11/26/2008 | EP1250555B1 Thermal shield for a component carrying hot gases, especially for structural components of gas turbines |
| 11/26/2008 | CN101311509A Methods and apparatus for operating gas turbine engines |
| 11/26/2008 | CN100438162C Hybrid fuel cell-pulse detonation power system |
| 11/26/2008 | CN100436945C Fuel pre-evaporation and premix perforated pipe |
| 11/26/2008 | CN100436755C Perimeter-cooled turbine bucket airfoil cooling hole location, style and configuration |
| 11/25/2008 | US7455150 Rotating shaft scavenging scoop |
| 11/25/2008 | US7454894 Supplemental oil cooler airflow for gas turbine engine |
| 11/25/2008 | CA2430654C Further cooling of pre-swirl flow entering cooled rotor aerofoils |
| 11/20/2008 | WO2008140410A1 Integrated burner and heat exchanger in a combined heat and power system |
| 11/20/2008 | WO2008139536A1 Natural gas liquefaction plant and method of operating the same |
| 11/20/2008 | WO2008139095A2 Method for assembling end to end two parts having different thermal expansion coefficients and assembly thus obtained |
| 11/20/2008 | WO2008138797A2 Pressure dynamics reduction within a gas turbine engine |
| 11/20/2008 | WO2008138221A1 Intercooling equipressure heat-of-absorption type air turbine |
| 11/20/2008 | US20080282703 Interface between a combustor and fuel nozzle |
| 11/20/2008 | US20080282667 Method and apparatus to facilitate cooling turbine engines |
| 11/20/2008 | DE102008023428A1 Verfahren und Vorrichtung zur Kühlung von Turbinentriebwerken Method and apparatus for cooling turbine engines |
| 11/20/2008 | DE102007023380A1 Gasturbine Gas turbine |
| 11/20/2008 | DE102007023142A1 Exhaust gas compressor for automotive exhaust gas turbocharger has spiral wall incorporating cooling duct |
| 11/20/2008 | CA2683372A1 Assistance device for transient acceleration and decelaration phases |
| 11/19/2008 | EP1992810A2 Variable contraction ratio nacelle assembly for a gas turbine engine |
| 11/19/2008 | EP1992807A2 Variable geometry nacelle for an aircraft engine and corresponding operating method |
| 11/19/2008 | EP1992790A1 Casing and fluid machine |
| 11/19/2008 | EP1692420B1 Air turbine starter having a low differential check valve |
| 11/19/2008 | CN201152198Y Coal fines two-phase stream material feeding device of coal fines gas turbine |
| 11/19/2008 | CN101307724A Gas engine heat pump noise reduction system |
| 11/19/2008 | CN101307723A Method and apparatus to facilitate cooling turbine engines |
| 11/19/2008 | CN101307721A Motor drive rotating combustion-chamber assembly outer compression double-modes runner engine |
| 11/19/2008 | CN101307442A Method for making high-temperature articles |
| 11/19/2008 | CN100434686C Anti-detonation fuel delivery system. |
| 11/18/2008 | US7451947 Engine mounting structure under an aircraft wing |
| 11/18/2008 | US7451753 Pre-heating of a liquid in an aircraft reservoir |
| 11/18/2008 | US7451599 Fuel manifold inlet tube |
| 11/18/2008 | CA2629043A1 Stress reduction feature to improve fuel nozzle sheath durability |
| 11/18/2008 | CA2425743C Sealing device for connection of a pipe in a hole |
| 11/18/2008 | CA2302245C Performance-based control system |
| 11/16/2008 | CA2625133A1 Redundant mounting system for an internal fuel manifold |
| 11/13/2008 | WO2008136122A1 Gas turbine equipment and method of altering the same |
| 11/13/2008 | WO2008136119A1 Gas turbine utilizing cold heat of lng and operating method of gas turbine utilizing cold heat of lng |
| 11/13/2008 | WO2008135699A2 Device for diverting and retaining aircraft engine debris |
| 11/13/2008 | WO2008134856A1 Method of starting turbine engine from low engine speed |
| 11/13/2008 | WO2008113931A3 Acoustic panel |
| 11/13/2008 | WO2008104714A3 Coating for acoustic treatment having a hot air icing processing function |
| 11/13/2008 | US20080279688 Heated engine nose cone using spiral channels |
| 11/13/2008 | US20080276622 Fuel nozzle and method of fabricating the same |
| 11/13/2008 | US20080276621 Catenary mid-turbine frame design |
| 11/13/2008 | US20080276617 Configurations and Methods For Thermal Integration of Lng Regasification and Power Plants |
| 11/13/2008 | DE102008022669A1 Brennstoffdüse und Verfahren für deren Herstellung Fuel nozzle, and methods for their preparation |
| 11/13/2008 | DE102007013727A1 Bearing for shaft of turbocharger, comprises rotor of turbine, which is mounted at one end of bearing, rotor of compressor, which is connected at another end of bearing, and spacer ring formed by elongated inner ring |