Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan
Patents for F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580)
09/2014
09/25/2014US20140283500 Thrust efficient turbofan engine
09/23/2014US8840064 Stub frame for a cascade thrust reverser structure
09/23/2014US8839805 Passive boundary layer bleed system for nacelle inlet airflow control
09/18/2014WO2014143290A1 Off-cambered vanes for gas turbine engines
09/18/2014WO2014143248A1 Ultra high bypass ratio turbofan engine
09/18/2014WO2014143224A1 Turbine engine repair methods
09/18/2014WO2014143210A1 Gas turbine engine flow duct having two rows of integrated heat exchangers
09/18/2014WO2014143188A1 Fan track liner designed to yield next to fan case hook
09/18/2014WO2014143074A1 Geared architecture with inducer for gas turbine engine
09/18/2014WO2014140483A1 Turbine engine, such as an airplane turbofan or turboprop engine
09/18/2014US20140260180 Gas Turbine Engine with Stream Diverter
09/18/2014DE102014103020A1 Systeme und Vorrichtungen zur stromabwärtigen Brennstoff- und Luftinjektion bei Gasturbinen Systems and devices for the downstream fuel and air injection in gas turbines
09/17/2014EP2776677A1 Gas turbine engine compressor arrangement
09/16/2014US8834599 Method and device for operating a smelting reduction process
09/16/2014US8834108 Running-gap control system of an aircraft gas turbine
09/16/2014US8833721 Gas turbine engine systems and related methods involving thermally isolated retention
09/14/2014CA2846520A1 Aerodynamically active stiffening feature for gas turbine recuperator
09/12/2014WO2014137451A1 Ram air thermal management system for an aircraft engine
09/12/2014WO2014137446A1 Hybrid fan blades for jet engines
09/12/2014WO2014137431A1 Brush seal repair method
09/12/2014WO2014137424A1 Gas turbine engine
09/12/2014WO2014137411A1 Fan track liner assembly with a spring element
09/12/2014CA2845455A1 Gas turbine engine exhaust mixer with aerodynamic struts
09/11/2014US20140250862 Reverse flow gas turbine engine airflow bypass
09/11/2014DE112012005550T5 Kompressorführungsschaufel und Vorsteuerung für einen Gasturbinenmotor Compressor guide vane and feedforward control for a gas turbine engine
09/09/2014US8827633 Gas turbine engine fan drive gear system damper
09/09/2014US8826641 Thermal management system integrated pylon
09/09/2014CA2656137C Turbine engine for aircraft
09/09/2014CA2570604C Shrouded turbofan bleed duct
09/04/2014WO2014133645A2 Gas turbine engine having configurable bypass passage
09/04/2014US20140245715 Primary cowl of a turbofan comprising a rotating ring having micro-jets
08/2014
08/28/2014WO2014130494A1 Gas turbine engine core utilized in both commercial and military engines
08/28/2014WO2014130361A1 Turbofan engine including third flowpath exhaust nozzle
08/28/2014WO2014130158A1 Liner apparatus for a gas turbine engine
08/28/2014WO2014130102A1 Distributed spark ignition system for a combustor
08/28/2014WO2014105701A3 Non-integral fan blade platform
08/28/2014WO2014088673A3 Gas turbine engine fan spacer platform attachments
08/28/2014DE102013101791A1 Fluggasturbine mit einer ersten drehbaren Welle Aircraft gas turbine with a first rotatable shaft
08/27/2014EP2770191A2 Aircraft gas turbine engine with a first rotatable shaft
08/26/2014US8814512 Fan disk apparatus and method
08/26/2014US8813907 Noise reduction system with chamber
08/21/2014WO2014126565A1 Gas turbine engine component having surface indicator
08/21/2014WO2014105237A3 Geared turbofan primary and secondary nozzle integration geometry
08/21/2014US20140230403 Gas turbine engine shaft bearing configuration
08/21/2014DE102013202786A1 Vorrichtung und Verfahren zum Abblasen von Verdichterluft in einem Turbofantriebwerk Apparatus and method for blow-off of air compressor in a turbofan engine
08/19/2014CA2620782C Discharge device for a jet turbine engine, and jet turbine engine comprising same
08/14/2014WO2014123796A1 Elongated geared turbofan with high bypass ratio
08/14/2014US20140223884 Ultra-efficient propulsor with an augmentor fan circumscribing a turbofan
08/13/2014CN203769944U 液态气体混合动力涡轮喷气发动机 Liquid gas hybrid turbojet
08/13/2014CN103987949A 一种涡轮发动机的缩放喷嘴 A turbine engine nozzle scaling
08/12/2014US8800261 Gas turbine engine with noise attenuating variable area fan nozzle
08/07/2014WO2014120115A1 Reverse-flow core gas turbine engine with a pulse detonation system
08/07/2014US20140219773 Internal Mixing Of A Portion Of Fan Exhaust Flow And Full Core Exhaust Flow In Aircraft Turbofan Engines
08/06/2014CN103967840A 将轴流涡轮压缩机的叶片连接至压缩机鼓 The axial flow turbine compressor blades connected to a compressor drum
08/06/2014CN103967651A 用于设置燃气涡轮发动机的风扇驱动齿轮系统的齿轮比的方法 For setting a gas turbine engine fan drive gear system gear ratio method
08/06/2014CN103967650A 涡轮风扇发动机 Turbofan engines
08/06/2014CN103967649A 涡轮喷气发动机 Turbojet
08/06/2014CN102239323B 利用压缩空气提高燃料驱动的涡轮发电机的效率的方法和设备 Methods and apparatus to improve the efficiency of the fuel with compressed air driven turbine generator
08/05/2014US8793973 Thrust reverser for a dual-flow turbine engine nacelle
07/2014
07/31/2014WO2014116308A2 Geared turbine engine with a d-duct and a thrust reverser
07/31/2014WO2014116243A1 Reverse core gas turbine engine with high temperature third steam
07/31/2014WO2014116242A1 Reverse flow gas turbine engine core
07/31/2014US20140208714 Thermal Management for Gas Turbine Engine
07/31/2014DE102013001617A1 Triebwerk mit Schutzeinrichtung Engine and Protection System
07/30/2014CN103953458A 一种变循环发动机可调机构中的同步驱动式后涵道引射器 A variable cycle engine adjustable synchronous mechanism driven ducted after ejector
07/29/2014US8789355 Support structure and mounting componet for a thrust inverter
07/29/2014US8789354 Gas turbine engine with separate core and propulsion unit
07/24/2014WO2014113372A1 Engine architecture with reverse rotation integral drive and vaneless turbine
07/24/2014WO2014113043A1 Compound fillet for guide vane
07/24/2014WO2014113038A1 Relationship between fan and primary exhaust stream velocities in a geared gas turbine engine
07/24/2014US20140205439 Gas turbine engine shaft bearing configuration
07/24/2014US20140202133 Gas turbine engine mid turbine frame with flow turning features
07/23/2014EP2756182A2 Guide vane assembly for a gas turbine engine
07/23/2014CN203730649U 一种大型机匣用减震支撑 A large, casing with shock-absorbing support
07/23/2014CN103939236A 外燃推进发动机 External combustion propulsion engines
07/23/2014CN102341588B 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
07/17/2014WO2014109785A1 Below wing reverse core gas turbine engine with thrust reverser
07/17/2014WO2014066508A3 Unducted thrust producing system architecture
07/16/2014EP2753813A1 Turbofan engine with convergent - divergent exhaust nozzle
07/15/2014US8777577 Hybrid fan blade and method for its manufacture
07/15/2014US8777554 Intermediate fan stage
07/08/2014US8769958 Device for attaching a flame-holder arm to an afterburner housing
07/08/2014US8769925 Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle
07/08/2014US8769924 Gas turbine engine assembly including accessory components within the nacelle
07/08/2014CA2635049C Dual flow turbine engine equipped with a precooler
07/03/2014WO2014105515A1 Cooling architecture for turbine exhaust case
07/03/2014WO2014105394A1 Geared gas turbine engine exhaust nozzle with chevrons
07/03/2014WO2014105392A1 Gas turbine engine serpentine cooling passage with chevrons
07/03/2014WO2014105109A1 Gas turbine engine component having vascular engineered lattice structure
07/03/2014WO2014105104A1 Blade underroot spacer with hook removal
07/03/2014WO2014035531A9 Micro thruster uses and improvements
07/03/2014US20140183296 Gas Turbine Engine Having Fan Rotor Driven by Turbine Exhaust and With a Bypass
07/03/2014US20140182304 System and method for a turbine combustor
07/02/2014CN103906910A 具有可变总压力比的燃气涡轮发动机 Having a variable total pressure ratio gas turbine engine
07/01/2014US8764387 Aggregate vane assembly
07/01/2014US8763361 Propulsion system with movable thermal choke
06/2014
06/26/2014WO2014100087A1 Gas turbine engine including a pre-diffuser heat exchanger
06/26/2014WO2014099221A1 High pressure turbine speed calculation from fuel system hydraulic pressures
06/26/2014WO2014099160A1 Closure of cooling holes with a filling agent
06/26/2014WO2014099156A1 Composite ducts and methods
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