| 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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| 08/13/2014 | EP2765304A2 Method for aircraft engine start using synchronous generator and constant speed drive |
| 08/13/2014 | EP2765295A2 A panel mounting arrangement |
| 08/13/2014 | EP2765283A1 Power generating unit and method for operating such a power generating unit |
| 08/13/2014 | EP2765282A1 Power generating unit and method for operating such a power generating unit |
| 08/13/2014 | CN203771456U 燃烧器、支承柱和燃料歧管 Burner, the support columns and fuel manifold |
| 08/13/2014 | CN203769944U 液态气体混合动力涡轮喷气发动机 Liquid gas hybrid turbojet |
| 08/13/2014 | CN203769943U 发动机结构件以及发散冷却结构 Structural parts and engine cooling structure divergence |
| 08/13/2014 | CN103987941A 基础齿轮系统结构 Basic gear system architecture |
| 08/13/2014 | CN103987624A 用于涡轮发动机机舱的进气口结构 Air intake structure for the turbine engine nacelle |
| 08/13/2014 | CN103982303A 一种基于微透镜阵列实现可燃气体多点激光等离子体点火的方法及装置 A realization of combustible gas multi-point laser plasma ignition method and apparatus based on a microlens array |
| 08/13/2014 | CN103982302A 用于燃气轮机发电机组的冷却机构及燃气轮机发电机组 Gas turbine generator sets for cooling mechanism and the gas turbine generator sets |
| 08/13/2014 | CN103982301A 发电单元及用于操作此类发电单元的方法 And a method of operating such a power generating unit for generating unit |
| 08/13/2014 | CN103982300A 航空发动机用离心分离装置 Aero engine with a centrifugal separation device |
| 08/13/2014 | CN102562300B 涡旋燃气蒸汽轮机 Vortex gas steam turbine |
| 08/13/2014 | CN101769202B 用于克服额定压力启动蒸汽轮机的装置 Means for overcoming the rated pressure steam turbine startup |
| 08/12/2014 | US8801825 Systems and methods for air intake filter assemblies |
| 08/12/2014 | US8800918 Hybrid engine accessory power system |
| 08/12/2014 | US8800300 Connection structure of exhaust chamber, support structure of turbine, and gas turbine |
| 08/12/2014 | US8800299 Jet engine nacelle having dampers for half-shells |
| 08/12/2014 | US8800297 Method for starting up a gas and steam turbine system |
| 08/12/2014 | US8800289 Apparatus and method for mixing fuel in a gas turbine nozzle |
| 08/12/2014 | US8800288 System for reducing vibrational motion in a gas turbine system |
| 08/12/2014 | US8800258 Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure |
| 08/12/2014 | US8800146 Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same |
| 08/12/2014 | CA2606860C Turbofan engine assembly and method of assembling same |
| 08/07/2014 | WO2014120598A1 Gas turbine offline compressor wash with buffer air from combustor |
| 08/07/2014 | WO2014120565A1 Bell mouth inlet for turbine blade |
| 08/07/2014 | WO2014120384A1 Spinner assembly with removable fan blade leading edge fairings |
| 08/07/2014 | WO2014120286A1 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine |
| 08/07/2014 | WO2014120285A1 Heat and energy recovery and regeneration assembly, system and method |
| 08/07/2014 | WO2014120125A1 Gas turbine engine with lower bifurcation heat exchanger |
| 08/07/2014 | WO2014120123A2 Thermoplastic nosecone for a turbine engine |
| 08/07/2014 | WO2014118058A1 Gas turbine inlet silencer |
| 08/07/2014 | WO2014118029A1 Method for starting a combustion system |
| 08/07/2014 | WO2014078003A3 Gas turbine engine with inlet particle separator and thermal management |
| 08/07/2014 | US20140220324 Thermal barrier coating having outer layer |
| 08/07/2014 | US20140219774 Turbomachine geared architecture support assembly |
| 08/07/2014 | US20140216056 Heat exchange module for a turbine engine |
| 08/07/2014 | US20140216054 Variable Volume Combustor with Aerodynamic Support Struts |
| 08/07/2014 | US20140216052 Ignition device and method for a turbomachine combustion chamber |
| 08/07/2014 | US20140216051 Variable Volume Combustor with an Air Bypass System |
| 08/07/2014 | US20140216050 Variable Volume Combustor with Nested Fuel Manifold System |
| 08/07/2014 | US20140216049 Variable Volume Combustor with Pre-Nozzle Fuel Injection System |
| 08/07/2014 | US20140216048 Variable Volume Combustor |
| 08/07/2014 | US20140216041 Variable Volume Combustor with Center Hub Fuel Staging |
| 08/07/2014 | US20140216040 Variable Volume Combustor with a Conical Liner Support |
| 08/07/2014 | US20140216039 Variable Volume Combustor with Aerodynamic Fuel Flanges for Nozzle Mounting |
| 08/07/2014 | US20140216038 Variable Volume Combustor with Cantilevered Support Structure |
| 08/07/2014 | US20140216037 Engine fuel control system |
| 08/07/2014 | US20140216004 Compressed air bleed supply for buffer system |
| 08/07/2014 | US20140216003 Gas turbine engine with geared turbofan and oil thermal management system |
| 08/07/2014 | US20140215997 Flexible Shield for Fluid Connectors |
| 08/07/2014 | DE102014201547A1 Turbolader Turbocharger |
| 08/07/2014 | DE102013002192A1 Turbine für einen Abgasturbolader Turbine for an exhaust gas turbocharger |
| 08/07/2014 | DE102013001978A1 Ventileinheit für ein Wastegatesystem und Abgasturbolader Valve unit for a wastegate system and turbocharger |
| 08/07/2014 | DE102011002869B4 Reflektionsschalldämpfer Reflection silencer |
| 08/06/2014 | EP2762711A2 Engine fuel control system |
| 08/06/2014 | EP2762710A1 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine |
| 08/06/2014 | EP2762709A2 Method of operating a fuel heating system |
| 08/06/2014 | EP2762708A1 Combustor tail pipe, gas turbine with tail pipe, and method for manufacturing tail pipe |
| 08/06/2014 | EP2762707A2 Method of controlling a cooling system |
| 08/06/2014 | EP2762705A2 Fuel supply system, scramjet engine and method for operating the same |
| 08/06/2014 | EP2762687A1 Method for starting a combustion system |
| 08/06/2014 | EP2762685A1 Gas turbine engine integrated heat exchanger |
| 08/06/2014 | EP2762682A2 Axial turbine with meridionally divided turbine housing |
| 08/06/2014 | EP2762677A2 Two-shaft gas turbine |
| 08/06/2014 | EP2762408A1 Bi-directional ventilation systems for use with aircraft and related methods |
| 08/06/2014 | CN203756516U 一种可用于航改燃机新型燃油泵 Which can be used aeroderivative gas turbine new fuel pump |
| 08/06/2014 | CN103975199A 具有内部热隔离涂覆层的燃烧器谐振器部段及其制作方法 Burner resonator section and its production method has an internal coating of thermal isolation |
| 08/06/2014 | CN103975144A 贫燃料吸入燃气轮机的控制方法及控制装置 Lean fuel intake gas turbine control method and control device |
| 08/06/2014 | CN103975143A 燃气涡轮冷却系统及燃气涡轮冷却方法 Gas turbine cooling system and a gas turbine cooling method |
| 08/06/2014 | CN103975142A 安装用凸台以及风扇壳 Attachment boss and the fan case |
| 08/06/2014 | CN103975131A 用于从邻接的外部容积密封油室的系统以及提供有这种密封系统的涡轮机组 From an external volume for the sealing oil chamber adjacent systems and providing such a sealing system has turbomachinery |
| 08/06/2014 | CN103975129A 冲击冷却机构、涡轮翼以及燃烧器 Impingement cooling means, the turbine blade and the combustor |
| 08/06/2014 | CN103967622A 微型燃气轮机的起动供油控制方法及系统 Microturbine start fueling control method and system |
| 08/06/2014 | CN103967621A 具有微小斜肋-凹陷复合结构的冷却装置 With a slight slant ribs - the composite structure of the cooling apparatus recessed |
| 08/06/2014 | CN103967620A 一种用于大型燃气轮机的进气整流装置 Rectifier means for the intake of large gas turbines |
| 08/06/2014 | CN103967616A 火力发电系统 Thermal systems |
| 08/06/2014 | CN101725414B 使用排气再循环系统加热燃料的系统和方法 System and method for using exhaust gas recirculation system of heating fuel |
| 08/06/2014 | CN101451467B 气-油分离器 Air - oil separator |
| 08/06/2014 | CN101382087B 用于降低涡轮机偏心率和不圆度的设备和方法 Apparatus and method for reducing turbine eccentricity and roundness |
| 08/05/2014 | US8796871 Turbine engine starter/generator, and method for the control thereof |
| 08/05/2014 | US8794912 Strut and a gas turbine structure comprising the strut |
| 08/05/2014 | US8794633 Leaf seal |
| 08/05/2014 | US8794008 Methods of operation of a gas turbine with improved part load emissions behavior |
| 08/05/2014 | US8794007 Rocket propulsion device and method for assembling rocket propulsion device |
| 08/05/2014 | US8793972 Gas turbine installation with flue gas recirculation dependent on oxygen content of a gas flow |
| 08/05/2014 | US8793971 Fuel pumping system for a gas turbine engine |
| 08/05/2014 | CA2791191C Gas turbine engine |
| 08/05/2014 | CA2786321C Sealing arrangement and gas turbine engine with the sealing arrangement |
| 08/05/2014 | CA2763088C System and devices for collecting and treating waste water from engine washing |
| 08/05/2014 | CA2551219C Systems and methods for power generation with carbon dioxide isolation |
| 08/04/2014 | CA2841679A1 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine |
| 07/31/2014 | WO2014116842A1 Structures and methods for forcing coupling of flow fields of adjacent bladed elements of turbomachines, and turbomachines incorporating the same |
| 07/31/2014 | WO2014116626A2 Purge and cooling air for an exhaust section of a gas turbine assembly |
| 07/31/2014 | WO2014116585A1 Filter system and method for leak identification |
| 07/31/2014 | WO2014116475A1 Gas turbine engine component having contoured rib end |
| 07/31/2014 | WO2014116342A2 Carrier interlock |
| 07/31/2014 | WO2014116330A2 Gas turbine engine rotor seal |
| 07/31/2014 | WO2014105256A3 Gas turbine engine component platform cooling |