| 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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| 02/04/2015 | EP2831395A2 Gas turbine engine geared architecture axial retention arrangement |
| 02/04/2015 | EP2831394A1 Gas turbine with adjustable cooling air system |
| 02/04/2015 | EP2831393A1 Turbojet engine nacelle air intake structure of laminar type |
| 02/04/2015 | EP2831391A1 Torque frame bushing arrangement for gas turbine engine fan drive gear system |
| 02/04/2015 | EP2831382A1 Integration of parts of an afterbody of an aircraft engine |
| 02/04/2015 | EP2831377A2 Hybrid airfoil for a gas turbine engine |
| 02/04/2015 | CN204143971U 沿面点火电嘴用陶瓷绝缘子 Along the surface of the ignition spark plug ceramic insulator |
| 02/04/2015 | CN204140208U 一种管道减振装置 Damping device of a piping |
| 02/04/2015 | CN104335460A 航空器用发动机的齿轮箱一体型发电装置 Aircraft engines, gearboxes an integrated power plant |
| 02/04/2015 | CN104334972A 燃料喷射装置 Fuel injection device |
| 02/04/2015 | CN104334863A 叶片的连结部结构及使用该连结部结构的喷气式发动机 The blade connecting portion structure and use of the structure of the jet engine connecting portion |
| 02/04/2015 | CN104334857A 涡轮风挡 Turbo windshield |
| 02/04/2015 | CN104334856A 涡轮风挡 Turbo windshield |
| 02/04/2015 | CN104334855A 航空器用发动机的风扇罩 Aircraft engine fan cover |
| 02/04/2015 | CN104334850A 排气涡轮增压器 Exhaust turbocharger |
| 02/04/2015 | CN104329964A 一种用于微型燃气轮机的高效低成本管式回热器 A cost-efficient microturbine regenerator tube |
| 02/04/2015 | CN104329173A 一种燃气轮机燃料与空气混合比的控制方法及装置 A gas turbine fuel and air mixture ratio control method and apparatus |
| 02/04/2015 | CN104329172A 燃气轮机滑油组件 Oil gas turbine components |
| 02/04/2015 | CN104329171A 飞机及其发动机 Aircraft and their engines |
| 02/04/2015 | CN104329170A 燃气涡轮设备 Gas turbine equipment |
| 02/04/2015 | CN102686949B 燃烧器与涡轮部的连通结构及燃气轮机 Communication structure and a gas turbine combustor and a turbine section |
| 02/03/2015 | US8945255 Jet engine with deflector |
| 02/03/2015 | US8944765 Bellows type sealing device for partition penetration by a connecting rod of a turboprop fan blade orientation control system |
| 02/03/2015 | US8944754 Gas-turbine engine with bleed-air tapping device |
| 02/03/2015 | US8944400 Device for installing and removing an aircraft engine pre-cooler |
| 02/03/2015 | US8943876 Shaft break detection |
| 02/03/2015 | US8943840 Mounting assembly |
| 02/03/2015 | US8943839 Gas turbine engine generator switchable drive |
| 02/03/2015 | US8943827 Fuel air heat exchanger |
| 02/03/2015 | US8943826 Engine |
| 02/03/2015 | US8943791 Dirt particle separator device for use in a gas turbine engine |
| 02/03/2015 | CA2634986C Assembly of shaft in bearing with auto-extraction nut |
| 02/03/2015 | CA2615936C Integrated overboost protection gear |
| 02/03/2015 | CA2615038C Integrated overboost protection gear |
| 02/03/2015 | CA2602168C Gas turbine helicopter engine with noise emission reduced through acoustical treatment of an eductor |
| 02/02/2015 | CA2855800A1 Health monitoring of igniters |
| 01/29/2015 | WO2015013503A1 Trough seal for gas turbine engine |
| 01/29/2015 | WO2015012923A2 Turbofan engine front section |
| 01/29/2015 | WO2015012918A2 Gas turbine engine airfoil trailing edge suction side cooling |
| 01/29/2015 | WO2015012909A2 Preloaded aft vent area for low pressure fan ducts |
| 01/29/2015 | WO2015012908A2 Single-fitting, dual-circuit fuel nozzle |
| 01/29/2015 | WO2015011645A1 Apparatus for generating heat and electricity |
| 01/29/2015 | WO2015011413A1 Hub of an intermediate casing for an aircraft turbojet engine comprising doors with contoured geometry |
| 01/29/2015 | WO2015011395A1 Method of estimation on a curve of a relevant point for the detection of an anomaly of a motor and data processing system for the implementation thereof |
| 01/29/2015 | WO2015011392A1 Intermediate housing hub for an aircraft turbofan, including air guide deflectors |
| 01/29/2015 | US20150030440 Fireshield fastener hood |
| 01/29/2015 | US20150030435 Plasma flow control inlet particle separator system |
| 01/29/2015 | US20150028238 Valve Assembly for Switching and/or Regulating a Medium Flow of an Aerospace Engine and Aerospace Engine |
| 01/29/2015 | US20150028133 Enhanced Mixing Tube Elements |
| 01/29/2015 | US20150027811 Maintenance assembly adaptable within gas turbine engine |
| 01/29/2015 | US20150027545 Suppression of Shock-Induced Airflow Separation |
| 01/29/2015 | US20150027129 Gas turbine with adjustable cooling air system |
| 01/29/2015 | US20150027126 System for providing fuel to a combustor |
| 01/29/2015 | US20150027101 Geared gas turbine engine architecture for enhanced efficiency |
| 01/29/2015 | US20150027100 System for performing staging control of a multi-stage combustor |
| 01/29/2015 | US20150027099 Gas turbine facility |
| 01/29/2015 | DE112013002463T5 Abgasturbolader Exhaust gas turbocharger |
| 01/29/2015 | DE102013214487A1 Brennkammerschindel einer Gasturbine A gas turbine combustion chamber tile |
| 01/29/2015 | DE102013214389A1 Gehäusecontainment Housing containment |
| 01/29/2015 | CA2852436A1 Acoustic panel |
| 01/28/2015 | EP2829805A1 System for performing staging control of a multi-stage combustor |
| 01/28/2015 | EP2829735A1 Axial compressor |
| 01/28/2015 | EP2829721A2 Method and apparatus for detecting performance of an APU starter |
| 01/28/2015 | EP2829707A1 A fuel manifold and fuel injector arrangement for a combustion chamber |
| 01/28/2015 | EP2829706A1 Bleed air systems for use with aircrafts and related methods |
| 01/28/2015 | EP2829689A1 Insulating structure for a thermal gas turbine, coresponding thermal gas turbine and method of manufacturing |
| 01/28/2015 | EP2829688A1 Method and device for monitoring an APU turbine |
| 01/28/2015 | EP2829686A1 Method and apparatus for monitoring turbine efficiency of an aircraft auxiliary power unit |
| 01/28/2015 | EP2829475A1 Auxiliary power unit inlet apparatus and method |
| 01/28/2015 | EP2828514A1 Trailing edge cooling |
| 01/28/2015 | EP2828508A1 Ignition unit for turbojet engine |
| 01/28/2015 | EP2828507A1 Method for determining at least one firing temperature for controlling a gas turbine and gas turbine for performing the method |
| 01/28/2015 | EP2828506A1 Gas turbine power plant with non-homogeneous input gas |
| 01/28/2015 | EP2828505A2 Planetary gear system arrangement with auxiliary oil system |
| 01/28/2015 | EP2828483A1 Cooled wall |
| 01/28/2015 | CN204126731U 一种液态燃料与空气混合比的控制装置 A liquid fuel and air mixture ratio control device |
| 01/28/2015 | CN204126730U 一种回转体布局的燃气轮机回热器 One kind of gas turbine rotor layout regenerator |
| 01/28/2015 | CN104321513A 用于涡轮增压器的压缩机盖件 A compressor for a turbocharger of the cover member |
| 01/28/2015 | CN104314692A 一种微波表面波点火助燃装置 A microwave wave ignition combustion device |
| 01/28/2015 | CN104314691A 燃气轮机压气机进气升温方法及升温系统 Gas turbine compressor inlet temperature method and heating systems |
| 01/28/2015 | CN104314690A 一种等离子体相变控制进气道及控制方法 A plasma phase control method and variable inlet control |
| 01/28/2015 | CN103089451B 一种隔热罩 One kind of heat shield |
| 01/28/2015 | CN102612592B 用于绝热压缩空气能量储存系统的增强热能储存压力容器 Enhanced thermal insulation compressed air energy storage system for the storage pressure vessel |
| 01/28/2015 | CN102121420B 用于燃气涡轮的温度启动阀 Temperature for a gas turbine startup valve |
| 01/28/2015 | CN101861451B 在涡轮发动机燃料供给回路中监测高压泵的方法和设备 Methods and apparatus to monitor the high-pressure pump in turbine engine fuel supply circuit |
| 01/28/2015 | CN101743391B 燃气轮机的排气部的结构及燃气轮机 Structure and the portion of the gas turbine exhaust gas turbine |
| 01/28/2015 | CN101725985B 多管预混合装置 Multiple pre-mixing device |
| 01/27/2015 | US8942886 System for detecting an impact on an aircraft engine impeller wheel |
| 01/27/2015 | US8939714 Method of assembly for gas turbine fan drive gear system |
| 01/27/2015 | US8939398 Hinging cradle for fan cowls supported by said cowls in closed position |
| 01/27/2015 | US8939253 System and method for suppression of unwanted noise in ground test facilities |
| 01/27/2015 | US8938976 Structural frame for gas turbine combustion cap assembly |
| 01/27/2015 | US8938975 Control of axial thrust by guidance of the air drawn off from a centrifugal compressor |
| 01/27/2015 | US8938968 Burner of a gas turbine |
| 01/27/2015 | US8938944 Aircraft gas-turbine engine with oil cooler in the engine cowling |
| 01/27/2015 | CA2828313C Turbine comprising a sealing device between the stator blade carrier and the housing |
| 01/27/2015 | CA2686368C Torsional mode damping apparatus |
| 01/24/2015 | CA2857795A1 Method for monitoring performance of the lubricant cooler in aircraft auxiliary power unit |
| 01/24/2015 | CA2857791A1 System and method for detecting addition of engine lubricant |
| 01/24/2015 | CA2857787A1 Method and apparatus for monitoring turbine efficiency of aircraft auxiliary power unit |