| 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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| 07/31/2014 | WO2014081492A3 Cooling for combustor liners with accelerating channels |
| 07/31/2014 | WO2014077922A3 Nacelle scoop inlet |
| 07/31/2014 | WO2014058509A3 Casting cores and manufacture methods |
| 07/31/2014 | US20140212276 Variable outer air seal fluid control |
| 07/31/2014 | US20140209408 Exhaust cone |
| 07/31/2014 | US20140208771 Gas turbine engine component cooling arrangement |
| 07/31/2014 | US20140208770 Component having insert for receiving threaded fasteners |
| 07/31/2014 | US20140208769 Integrated inducer heat exchanger for gas turbines |
| 07/31/2014 | US20140208768 Coolant supply system |
| 07/31/2014 | US20140208766 Waste Heat Recovery Fuel Gas Heater Control Method and Algorithm |
| 07/31/2014 | US20140208762 Compressor wash with air to bearing buffering system |
| 07/31/2014 | US20140208761 Bi-directional ventilation systems for use with aircraft and related methods |
| 07/31/2014 | US20140208760 Gas turbine engine with transmission |
| 07/31/2014 | US20140208759 Apparatus and method for reducing oil mist ingestion in a heavy duty gas turbine engine |
| 07/31/2014 | US20140208755 Gas Turbine Air Mass Flow Measuring System and Methods for Measuring Air Mass Flow in a Gas Turbine Inlet Duct |
| 07/31/2014 | US20140208712 Component having a heat protection system |
| 07/31/2014 | DE102014100825A1 Turbolader, System und Verfahren zum Ausleiten von Fluid aus einem Turbolader Turbocharger system and method for discharging fluid from a turbocharger |
| 07/31/2014 | DE102014100481A1 Systeme und Verfahren zur Messung eines Strömungsprofils im Strömungsweg einer Turbine Systems and methods for measuring a flow profile in the flow path of a turbine |
| 07/31/2014 | DE102014100479A1 Systeme und Verfahren zur Nutzungsdauerverlängerung von Heißgaspfadteilen mit Ladeluftstrombypass Systems and methods for life extension of hot gas path parts with charge air flow bypass |
| 07/31/2014 | DE102013201232A1 Brenner mit einer zentralen Brennstoffzufuhranordnung Burner with a central fuel supply arrangement |
| 07/31/2014 | DE102013001617A1 Triebwerk mit Schutzeinrichtung Engine and Protection System |
| 07/31/2014 | DE102013001216A1 Antriebsaggregat zum Antreiben eines Kraftwagens Drive unit for driving a motor vehicle |
| 07/30/2014 | EP2758648A1 Heat shield for a turbocharger and arrangement of a heat shield between two housing parts of a turbocharger |
| 07/30/2014 | CN203743040U 燃气轮机的压缩机端支座的连接装置 Connection means the end of the gas turbine compressor bearing |
| 07/30/2014 | CN203742793U 转轴轴承组件及燃气轮机的封油装置 Gas turbine shaft bearing assembly and seal oil system |
| 07/30/2014 | CN203742792U 燃气轮机中导叶的驱动机构及其燃气轮机 Gas turbine vanes and turbine drive mechanism |
| 07/30/2014 | CN103958949A 密封结构及具备该密封结构的旋转机械 Sealing structure and the seal structure includes a rotating machine |
| 07/30/2014 | CN103958857A 贫燃料吸入燃气轮机 Inhalation of the gas turbine fuel lean |
| 07/30/2014 | CN103958856A 使用双压力高速离心泵装置的燃料系统 High-speed centrifugal device using a dual pressure fuel system |
| 07/30/2014 | CN103958855A 重型结构物的支持机构 Heavy structure of the support organization |
| 07/30/2014 | CN103953449A 一种基于各向异性材料的航空发动机的降噪方法 A noise reduction method for anisotropic materials based aeroengine |
| 07/30/2014 | CN103953448A 一种高超声速进气道 Hypersonic Inlet |
| 07/30/2014 | CN102937050B 一种应用于车用燃气轮机燃油稳燃的高压空气路系统 Applied to high-pressure air path system vehicle steady combustion turbine fuel |
| 07/30/2014 | CA2849372A1 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine |
| 07/30/2014 | CA2841407A1 Gas turbine engine with transmission |
| 07/30/2014 | CA2841405A1 Gas turbine engine with transmission |
| 07/29/2014 | US8789377 Gas turbine engine with liquid metal cooling |
| 07/29/2014 | US8789376 Flade duct turbine cooling and power and thermal management |
| 07/29/2014 | US8789372 Injector with integrated resonator |
| 07/29/2014 | US8789353 Fuel system |
| 07/24/2014 | WO2014113752A1 Component mount integrated with tube fitting |
| 07/24/2014 | WO2014113747A1 Adjustable floating oil channel for gas turbine engine gear drive |
| 07/24/2014 | WO2014113662A1 Turbine engine hybrid power supply |
| 07/24/2014 | WO2014113468A1 Seal for dual fuel nozzle of a gas turbine engine |
| 07/24/2014 | WO2014113300A1 Oil pump transfer plate |
| 07/24/2014 | WO2014113258A1 Dual pump/dual bypass fuel pumping system |
| 07/24/2014 | WO2014113043A1 Compound fillet for guide vane |
| 07/24/2014 | WO2014113007A1 Gas turbine engine combustor liner assembly with convergent hyperbolic profile |
| 07/24/2014 | WO2014112988A1 Heat shield for gas turbine engine gearbox |
| 07/24/2014 | WO2014099076A9 Gas turbine engine combustor with integrated combustor vane |
| 07/24/2014 | WO2014070436A3 Temperature control within a cavity of a turbine engine |
| 07/24/2014 | WO2014051888A3 Spring carrier and removable seal carrier |
| 07/24/2014 | WO2014037652A3 Speed-reducing unit having an epicyclic gear train, in particular for a turbine engine |
| 07/24/2014 | US20140205447 Purge and cooling air for an exhaust section of a gas turbine assembly |
| 07/24/2014 | US20140205446 Regulated oil cooling system for a turbine engine with deicing of the nacelle |
| 07/24/2014 | US20140205443 Seal assembly including grooves in an aft facing side of a platform in a gas turbine engine |
| 07/24/2014 | US20140205442 Sealing device for a turbomachine turbine nozzle |
| 07/24/2014 | US20140205441 Seal assembly including grooves in a radially outwardly facing side of a platform in a gas turbine engine |
| 07/24/2014 | US20140205439 Gas turbine engine shaft bearing configuration |
| 07/24/2014 | US20140205438 Relationship between fan and primary exhaust stream velocities in a geared gas turbine engine |
| 07/24/2014 | US20140202186 Zoned Evaporative Cooling Media for Air Intake House of Gas Turbine |
| 07/24/2014 | US20140202170 Composite Articles and Methods |
| 07/24/2014 | US20140202169 Assembly formed by a turbine engine and a system for attaching it to an aircraft structure |
| 07/24/2014 | US20140202165 Oxidizing fuel in multiple operating modes |
| 07/24/2014 | US20140202163 Effusion plate using additive manufacturing methods |
| 07/24/2014 | US20140202160 Gas turbine system with manifold |
| 07/24/2014 | US20140202158 Gas turbine engine heat exchangers and methods of assembling the same |
| 07/24/2014 | US20140202130 Multi-color pyrometry imaging system and method of operating the same |
| 07/24/2014 | US20140202121 Conical light fod momentum particle separator protector |
| 07/24/2014 | DE102012222671B4 Vorrichtung sowie Verfahren zur Nutzung von Abwärme eines Verbrennungsmotors sowie Turbinenaggregat für eine solche Vorrichtung An apparatus and method for utilizing waste heat of an internal combustion engine and the turbine assembly for such a device |
| 07/23/2014 | EP2757236A1 System for monitoring the start of a rotary wing aircraft, aircraft and method implementing this system |
| 07/23/2014 | EP2756193A2 Method for monitoring the volumetric efficiency of an hp pump of a hydraulic regulation system for a turbomachine |
| 07/23/2014 | CN203730770U 涡轮旋转机械用自动调整密封件 Turbo rotary machine automatically adjusts the seals |
| 07/23/2014 | CN203730137U 用于控制来自燃气涡轮机的压缩器部段的冷却流动的系统 For controlling the flow of cooling gas from the compressor section of the turbine section of the system |
| 07/23/2014 | CN203730136U 一种涡轮爆震发动机 A turbine engine knock |
| 07/23/2014 | CN103946516A 阀控制装置、燃气涡轮机以及阀控制方法 Valve control means, a gas turbine, and a valve control method |
| 07/23/2014 | CN103946489A 消音装置及具备该消音装置的旋转机械 And provided with the silencing device silencing device rotating machine |
| 07/23/2014 | CN103946488A 旋转机械的密封结构及具备该密封结构的燃气轮机 Seal structure of rotating machinery and gas turbine equipped with the sealing structure |
| 07/23/2014 | CN103946484A 包括电激活燃料供给泵的涡轮发动机和涡轮发动机燃料供应方法 Electrical activation of the fuel supply pump includes a turbine engine and a turbine engine fuel supply method |
| 07/23/2014 | CN103946483A 具有冷却通路的翼 Wing having a cooling passage |
| 07/23/2014 | CN103945972A 接合部件 Engaging members |
| 07/23/2014 | CN103939626A 双闸门风扇空气调节阀 Double gate fan air valve |
| 07/23/2014 | CN103939218A 涡轮风扇发动机进口部件鸟弹撞击装置 Turbofan engines imported components bird bombs striking device |
| 07/23/2014 | CN103939217A 矩形截面高超声速变几何进气道及设计方法与工作方式 Rectangular section Hypersonic variable geometry inlet and design methods and ways of working |
| 07/23/2014 | CN103939216A 采用组合式口面旋涡控制方法的埋入式进气道 A modular control method orofacial vortex Submerged Inlet |
| 07/23/2014 | CN103939214A 一种原动机的半闭式定压内燃热力循环方法及系统 Semi-closed thermodynamic cycle constant pressure combustion method and system of the prime mover |
| 07/23/2014 | CN103038486B 发电设备 Power Equipment |
| 07/23/2014 | CN102341588B 通过周转齿轮传动链用于一对反向旋转螺旋桨的驱动机构 Drive mechanism through revolving gear train for a pair of counter-rotating propellers |
| 07/23/2014 | CN102112703B 燃气轮机设备 Gas Turbine Equipment |
| 07/23/2014 | CN101981277B 一种在涡轮喷气发动机轴承外壳内平衡压力的方法和装置 A method and apparatus to balance the pressure within the bearing housing turbojet |
| 07/23/2014 | CN101713549B 用于在燃气涡轮机中混合空气-燃料的系统 For mixing the air in a gas turbine - a fuel system |
| 07/22/2014 | US8783412 Sound absorber for a gas turbine exhaust cone, and method for the production thereof |
| 07/22/2014 | US8783044 Turbine stator nozzle cooling structure |
| 07/22/2014 | US8783009 Method and system for enhancing start of a turbine engine, and ignition module |
| 07/22/2014 | US8782865 Combustor liner and flow sleeve tool |
| 07/22/2014 | CA2764342C Side-fed shielded internal fuel manifold inlet tube |
| 07/22/2014 | CA2714826C Bleed air transfer tube |
| 07/22/2014 | CA2622006C Emergency fuel shutoff system and method |
| 07/22/2014 | CA2548138C Methods and apparatus for operating gas turbine engines |
| 07/22/2014 | CA2508418C Methods and apparatus for low emission gas turbine energy generation |