| 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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| 08/03/2010 | US7765810 Method for obtaining ultra-low NOx emissions from gas turbines operating at high turbine inlet temperatures |
| 08/03/2010 | CA2449497C A method of combustor cycle airflow adjustment |
| 07/30/2010 | CA2690665A1 Gas turbine engine assembly and methods of assembling same |
| 07/29/2010 | WO2010084573A1 Gas turbine facility |
| 07/29/2010 | WO2010084023A1 Device for large-scale media conditioning |
| 07/29/2010 | WO2009060137A3 Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure |
| 07/29/2010 | US20100189551 Systems and Methods of Reducing Heat Loss from a Gas Turbine During Shutdown |
| 07/29/2010 | US20100187818 Multi-process method of combined heat and power generation, biodiesel production, ethanol production, town gas production and methane production |
| 07/29/2010 | US20100187180 Method and apparatus for separating air and oil |
| 07/29/2010 | US20100186419 Heat transfer augmentation in a compact heat exchanger pedestal array |
| 07/29/2010 | US20100186417 Use of inert gases for shielding oxidizer and fuel |
| 07/29/2010 | US20100186414 Magnetic ion plasma annular injection combustor |
| 07/29/2010 | US20100186413 Bundled multi-tube nozzle for a turbomachine |
| 07/29/2010 | US20100186412 Annular fuel and air co-flow premixer |
| 07/29/2010 | US20100186411 Gas turbine |
| 07/29/2010 | US20100186368 Ignition/ chemical reaction promotion/ flame holding device, speed-type internal combustion engine, and furnace |
| 07/29/2010 | US20100186365 Heat Shield Element, in Particular for Lining a Combustion Chamber Wall |
| 07/29/2010 | DE102009055614A1 Exhaust gas turbocharger for use in internal combustion engine of motor vehicle, has snap ring provided as fastening unit for connecting housing upper and lower parts with one another in form-fit manner, where housing is made from plastic |
| 07/29/2010 | DE102009006198A1 Vorrichtung zur großtechnischen Medienkonditionierung Device for large-scale media conditioning |
| 07/29/2010 | DE102009005938A1 Ladeeinrichtung Loader |
| 07/29/2010 | DE102009005163A1 Sound absorber for flow channel of gas turbine, has passive absorber layer of absorption layer applied on flow channel wall and acoustically permeable covering layer |
| 07/29/2010 | DE102005046679B4 Montageanordnung für einen Luftabscheider und Gasturbine Mounting assembly for an air separator and gas turbine |
| 07/29/2010 | CA2690780A1 Dual channel regulated fuel-oil heat exchanger |
| 07/28/2010 | EP2211039A2 Methods and device for augmenting power output of a gas turbine plant |
| 07/28/2010 | EP2211016A2 Systems, Methods, and Apparatus for Controlling Gas Leaking in a Turbine |
| 07/28/2010 | EP2209976A2 Surveillance device of a high pressure pump in a fuel system of a turbomachine |
| 07/28/2010 | EP2209716A2 Method for controlling thermal effluents generated by an aircraft and cooling device for an aircraft implementing said method |
| 07/28/2010 | CN201535201U 涡喷发动机离合器 Turbojet engine clutch |
| 07/28/2010 | CN201535200U 涡喷发动机轴承润滑装置 Turbojet engine bearing lubrication device |
| 07/28/2010 | CN101787930A Thermal circulation process of gas turbine based on pure oxygen or oxygen-enriched combustion |
| 07/28/2010 | CN101787929A Externally adjustable impingement cooling manifold mount and thermocouple housing |
| 07/27/2010 | US7762087 Rotatable integrated segmented mid-turbine frames |
| 07/27/2010 | US7762086 Nozzle extension assembly for ground and flight testing |
| 07/27/2010 | US7762083 Gas turbine plant and gas turbine power generator plant |
| 07/27/2010 | US7762082 Apparatus and method of recovering vapors |
| 07/27/2010 | US7762070 Pilot nozzle heat shield having internal turbulators |
| 07/27/2010 | US7761992 Process for machining axial blade slots in turbine disks for jet engines |
| 07/27/2010 | CA2451495C Thermal barrier coating material, method of production thereof, and gas turbine member and gas turbine applying said thermal barrier coating material |
| 07/27/2010 | CA2389529C Variable cycle propulsion device employing compressed air bleed for supersonic aircraft |
| 07/27/2010 | CA2338347C Quasi-isothermal brayton cycle engine |
| 07/22/2010 | WO2010082632A1 Ni-based single crystal superalloy |
| 07/22/2010 | WO2010082360A1 Engine |
| 07/22/2010 | WO2010082359A1 Engine |
| 07/22/2010 | WO2010081697A1 Connection assembly of a turbine housing to a bearing housing and exhaust gas turbocharger |
| 07/22/2010 | WO2010059301A3 Integrated inlet design |
| 07/22/2010 | WO2010051143A3 Perforated composite structures and methods therefore |
| 07/22/2010 | US20100185377 System and method for starting a gas turbine engine with inoperable exhaust gas turbine temperature sensor |
| 07/22/2010 | US20100183429 Turbine blade with multiple trailing edge cooling slots |
| 07/22/2010 | US20100183428 Modular serpentine cooling systems for turbine engine components |
| 07/22/2010 | US20100183426 Fluidic rim seal system for turbine engines |
| 07/22/2010 | US20100181420 Coating for acoustic treatment that integrates the function of hot-air treatment of frost |
| 07/22/2010 | US20100181138 Turbine auxiliary power unit with a fuel fired burner |
| 07/22/2010 | US20100180605 Structural Attachment System for Transition Duct Outlet |
| 07/22/2010 | US20100180604 Method for starting premixed combustion in combustor for two-shaft gas turbine |
| 07/22/2010 | US20100180603 Fuel nozzle for a turbomachine |
| 07/22/2010 | US20100180602 Combustor assembly and cap for a turbine engine |
| 07/22/2010 | US20100180600 Nozzle for a turbomachine |
| 07/22/2010 | US20100180598 Burner and method for operating a burner |
| 07/22/2010 | US20100180573 A gas turbine engine |
| 07/22/2010 | US20100180569 Lead Arrangement for a Combustor Unit |
| 07/22/2010 | US20100180568 Heat regeneration for a turbofan, a Velarus Propulsion |
| 07/22/2010 | US20100180566 Bird and debris deflector for aircraft jet engines |
| 07/22/2010 | DE10392247B4 Brennkammer für Gasturbine Combustion chamber for gas turbine |
| 07/22/2010 | DE102009005438A1 Axial bearing for use in exhaust gas turbocharger for supporting rotatable shaft, has connecting edge extended like arc, provided between wedge and locking surfaces and formed in radial direction and/or circumferential direction |
| 07/22/2010 | DE102009005386A1 Ladeeinrichtung für eine Brennkraftmaschine Charging device for an internal combustion engine |
| 07/22/2010 | CA2749755A1 Ni-based single crystal superalloy |
| 07/21/2010 | CN201531279U Air bearing turbine cooler low-pressure starting device |
| 07/21/2010 | CN1908405B Inlet guide vane control device of gas turbine |
| 07/21/2010 | CN101785069A Closed cycle plant |
| 07/21/2010 | CN101784841A Gas turbine combustor |
| 07/21/2010 | CN101784776A Gas turbine combustor |
| 07/21/2010 | CN101780352A Gas turbine inlet air filtration filter element |
| 07/21/2010 | CN101503975B Main pipe type micro turbine group of dual-air compressor |
| 07/20/2010 | US7758301 Arrangement for detection of a shaft break in a gas turbine as well as gas turbine |
| 07/20/2010 | US7758296 Method for reducing the noise of turbo engines |
| 07/20/2010 | US7757495 Turbine engine annular combustion chamber with alternate fixings |
| 07/20/2010 | US7757494 Device for feeding fuel to a combustion chamber in a turbomachine |
| 07/20/2010 | US7757475 Gas turbine equipment utilizing high humidity |
| 07/20/2010 | CA2453759C Manufacturing cell using tooling apparatus |
| 07/15/2010 | WO2010051453A3 Turbine blade including a seal pocket |
| 07/15/2010 | US20100178158 Turbine wash port for a gas turbine engine |
| 07/15/2010 | US20100178152 Compressor Clearance Control System Using Turbine Exhaust |
| 07/15/2010 | US20100175389 Apparatus For Filtering Gas Turbine Inlet Air |
| 07/15/2010 | US20100175388 Inlet bleed heat system thermal lag mitigation using compressor interstage bleeds |
| 07/15/2010 | US20100175386 Premixed partial oxidation syngas generation and gas turbine system |
| 07/15/2010 | US20100175384 Optical Flame Holding And Flashback Detection |
| 07/15/2010 | US20100175382 Gas turbine burner |
| 07/15/2010 | US20100175380 Traversing fuel nozzles in cap-less combustor assembly |
| 07/15/2010 | US20100175364 Integrated coal gasification combined cycle facility |
| 07/15/2010 | DE102009046630A1 Wärmemanagement für Kraftstoffeinspritzeinrichtungen Thermal Management for fuel injectors |
| 07/15/2010 | CA2690216A1 Turbine wash port for a gas turbine engine |
| 07/14/2010 | EP2206967A2 Gas turbine engine late lean injection system |
| 07/14/2010 | EP2206966A2 Gas turbine engine late lean injection for fuel injection flexibility |
| 07/14/2010 | EP2206965A2 Late lean injection with expanded fuel flexibility |
| 07/14/2010 | EP2206964A2 Late lean injection fuel injector configurations |
| 07/14/2010 | EP2206963A2 Late lean injection fuel staging configurations |
| 07/14/2010 | EP2206962A2 Late lean injection control strategy |
| 07/14/2010 | EP2206961A2 Gas turbine engine late lean injection with adjustable air splits |
| 07/14/2010 | EP2206902A2 Turbine cooling air from a centrifugal compressor |
| 07/14/2010 | EP2206893A2 Combined Surface Cooler and Acoustic Absorber for Turbomachines |