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)
06/2014
06/26/2014WO2014099102A1 Airfoil member and composite platform having contoured endwall
06/26/2014WO2014098961A1 Two spool gas generator with improved pressure split
06/26/2014WO2014098936A1 Gas turbine engine inner case including non-symmetrical bleed slots
06/26/2014WO2014096647A1 Intermediate casing extension of improved design
06/26/2014US20140174056 Gas turbine engine with low stage count low pressure turbine
06/26/2014US20140174055 Turbine section of high bypass turbofan
06/25/2014EP2745223A1 Method of determining the performance of at least one propeller of a turbomachine in an air stream under gyration
06/25/2014EP2744637A1 Panels and processes therefor
06/25/2014CN103883427A 组合式喷气发动机 Combined jet engine
06/24/2014US8756911 Turbine exhaust cylinder and strut cooling
06/19/2014WO2014092909A1 Multi-piece blade for gas turbine engine
06/19/2014WO2014092778A1 Dual filtration particle separator
06/19/2014WO2014092777A1 Gas turbine engine with plural accessory air paths
06/19/2014WO2014092750A1 Gas turbine engine with cooling scheme for drive gear system and pitch control
06/19/2014WO2013122713A8 Geared turbofan engine low noise compressor rotor
06/19/2014US20140165584 Cryogenic pump system for converting fuel
06/19/2014US20140165534 Gas turbine engine compressor arrangement
06/19/2014US20140165533 Gas turbine engine mounting ring
06/18/2014CN203655469U 液态气体加力喷气发动机 Liquid gas afterburning jet engine
06/18/2014CN103867337A Variable cycle engine with high bypass ratio
06/18/2014CN103867336A Jet propulsion and power output integrated system
06/12/2014US20140157757 Gas turbine engine compressor arrangement
06/12/2014US20140157756 Gas turbine engine compressor arrangement
06/12/2014US20140157755 Gas turbine engine compressor arrangement
06/12/2014US20140157754 Gas turbine engine compressor arrangement
06/12/2014US20140157753 Gas turbine engine compressor arrangement
06/12/2014US20140157752 Gas turbine engine compressor arrangement
06/11/2014CN203640864U 涡轮发动机用增压装置 Turbo engine with supercharging device
06/10/2014US8745966 Mobile thrust reverser cowl and thrust reverser provided with such a cowl
06/10/2014CA2632716C Brazed joint between a metal part and a ceramic part
06/05/2014WO2014083256A1 Turbine engine cowl capable of covering a fan cone
06/04/2014EP2737193A1 Aircraft propulsion unit including at least one turbojet engine and a nacelle
06/04/2014CN103835836A Bypass-ratio controllable gas turbine
06/03/2014US8739514 Low shock strength propulsion system
05/2014
05/30/2014WO2014081509A1 Composite articles and methods
05/30/2014WO2014031197A3 Gas turbine engine with a counter rotating fan
05/30/2014WO2013122713A3 Geared turbofan engine low noise compressor rotor
05/28/2014DE102004026367B4 Turbomaschine Turbomachine
05/28/2014CN102317608B 最优化低环境影响背景信息的对旋风扇设计和可变叶片列间隔 Optimization of low environmental impact of background information on the design and variable fan blades spin column spacing
05/22/2014WO2014078157A1 Gas turbine engine with mount for low pressure turbine section
05/22/2014WO2014042735A3 Gas turbine engine component with discharge slot having oval geometry
05/22/2014US20140137540 Engine and thrust reverser actuation system
05/22/2014US20140137538 Fast Response Bypass Engine
05/21/2014CN203604064U 一种涡轮喷气发动机 One kind of turbojet
05/20/2014US8726670 Ejector purge of cavity adjacent exhaust flowpath
05/20/2014US8726634 Nacelle for an aircraft engine with variable cross-section nozzle having a rack and pinion actuator assembly
05/20/2014US8726633 Gas turbine engine systems and related methods involving multiple gas turbine cores
05/20/2014CA2602172C Blowing conduit for a turbine engine
05/15/2014WO2014074135A1 Reverse core turbine engine mounted above aircraft wing
05/15/2014WO2014035531A3 Micro thruster uses and improvements
05/15/2014WO2014031199A3 Protecting operating margin of a gas turbine engine
05/15/2014WO2014021981A3 Vortex generators for improved film effectiveness
05/15/2014US20140130479 Gas Turbine Engine With Mount for Low Pressure Turbine Section
05/15/2014DE102012013622A1 Rocket engine, particularly liquid rocket engine, has thrust chamber and pump unit, where thrust chamber is supplied to fuel component by pump unit, in which thrust chamber has aero spike nozzle
05/14/2014EP2730766A1 Heat exchange arrangement for a gas turbine
05/14/2014CN102395772B 设置有轴间轴承的双主体气体涡轮引擎 Is provided between the main shaft bearing twin gas turbine engine
05/13/2014US8720208 Aircraft gas turbine engine
05/13/2014US8720183 Thrust reverser translating sleeve assembly
05/13/2014CA2697741C Combined acoustic absorber and heat exchanging outlet guide vanes
05/13/2014CA2507977C Method and apparatus for operating an intercooler for a gas turbine engine
05/08/2014WO2014068261A1 Turbomachine casing
05/08/2014WO2014021982A3 Turbomachinery component cooling scheme
05/08/2014DE112012003380T5 Paneele und Produktionsverfahren dafür Panels and production for
05/07/2014CN103775245A 旋转式燃烧室喷气发动机 Rotary jet engine combustion chamber
05/06/2014US8713911 System and method for operating a thrust reverser for a turbofan propulsion system
05/06/2014US8713910 Integrated thrust reverser/pylon assembly
05/01/2014WO2014066515A1 Vane assembly for an unducted thrust producing system
05/01/2014WO2014066503A1 Unducted thrust producing system
05/01/2014WO2014066210A1 Gas turbine engine variable bleed valve for ice extraction
05/01/2014US20140119885 Turbine engine assembly and methods of assembling same
05/01/2014US20140117152 Twin Tip Turbine Propulsors Powered by a Single Gas Turbine Generator
04/2014
04/30/2014CN103758661A Small turbine jet engine
04/24/2014WO2014062220A1 Structural guide vane circumferential load bearing shear pin
04/24/2014WO2014060681A1 Device and method for controlling the pitch of blades
04/24/2014US20140109548 High pressure rotor disk
04/23/2014EP2721260A1 Dual-flow turbine engine having a decoupling device
04/23/2014EP2720941A2 Blade, particularly variable-pitch blade, propellor comprising such blades and corresponding turbomachine
04/23/2014CN103742295A Turbojet engine and method for mixing liquid gas during operation of turbojet engine
04/23/2014CN103742294A Liquid gas afterburner jet engine and method for realizing afterburning flying of jet plane
04/22/2014US8701386 Aircraft nacelle that incorporates a thrust reversal device
04/17/2014WO2014058718A1 Bi-directional compression fan rotor for a gas turbine engine
04/17/2014WO2014058466A1 Geared turbofan engine with optimized diffuser case flange location
04/17/2014WO2014058463A1 Geared turbofan engine with inter-shaft deflection feature
04/17/2014WO2014025427A3 Turbomachine geared architecture support assembly
04/17/2014WO2014018137A3 Aircraft engine driveshaft vessel assembly and method of assembling the same
04/17/2014US20140102076 Turbine Section of High Bypass Turbofan
04/16/2014CN103726953A Turbofan engine with reverse ducts
04/16/2014CN103726952A Divided-flow type gas turbine engine
04/16/2014CN102124197B Inner wall for the nacelle of a turbine engine
04/15/2014US8696306 Bypass duct of a turbofan engine
04/15/2014US8695324 Multistage tip fan
04/15/2014CA2567533C Externally fueled trapped vortex cavity augmentor
04/15/2014CA2531741C Methods and apparatus for operating gas turbine engines
04/10/2014WO2014055499A1 Sheath with extended wings
04/10/2014WO2014055301A1 Reduced height ligaments to minimize non-integral vibrations in rotor blades
04/10/2014WO2014055299A1 Aluminum based abradable material with reduced metal transfer to blades
04/10/2014WO2014055124A1 Method of defining gas turbine engine control ratings
04/10/2014WO2014055122A1 Geared turbofan high gearbox power density
04/10/2014WO2014055116A1 Combustor with grommet having projecting lip
04/10/2014WO2014055114A1 Geared turbofan engine with high compressor exit temperature
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