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)
01/2015
01/07/2015EP2820279A2 High order shaped curve region for an airfoil
01/07/2015EP2820278A1 Hybrid turbofan engine
01/07/2015EP2820270A1 Geared gas turbine engine with reduced fan noise
01/07/2015EP2820267A2 Counter rotating low pressure compressor and turbine each having a gear system
01/07/2015EP2820266A2 Counter-rotating low pressure turbine with gear system mounted to turbine exhaust case
01/07/2015EP2820265A2 Counter rotating low pressure turbine with splitter gear system
01/07/2015EP2820246A2 Debris detection in turbomachinery and gas turbine engines
01/06/2015US8926279 Propeller hub
01/06/2015US8926277 Fan casing for a turbofan engine
01/06/2015US8926263 Turbomachine casing assembly
01/06/2015US8925330 Flow discharge device
01/06/2015US8925295 Air discharging device for an aircraft double-flow turbine engine
01/01/2015US20150000865 Heat exchanger for aircraft engine
01/01/2015US20150000251 System, Method and Apparatus for Lean Combustion with Plasma from an Electrical Arc
12/2014
12/30/2014US8919668 Thrust reverser having a lockable variable nozzle section
12/30/2014US8919135 Turbojet engine with an element of the nacelle attached to the intermediate casing
12/30/2014US8919133 Double-body gas turbine engine provided with an inter-shaft bearing
12/25/2014US20140373927 Low shock strength propulsion system
12/24/2014CN104246197A 燃气涡轮发动机的风扇驱动齿轮传动系统的阻尼器 Gas turbine engine fan drive gear system damper
12/24/2014CN104246176A 包括温差发电机的涡轮发动机 Including thermal generator turbine engine
12/24/2014CN104246139A 具有断裂、自由浮动的减震器构件的翼片 With a broken shock absorber fins free-floating members
12/24/2014CN104246132A 用于齿轮传动涡扇发动机的低噪声压缩机转子 Low noise compressor rotor for Geared Turbofan engine
12/24/2014CN103161608B 采用轴流斜流串列复合压缩系统单转子微小型涡扇发动机 Axial flow tandem compound using oblique compression system single rotor micro turbofan engine
12/23/2014US8915090 Gas turbine engine mid turbine frame with flow turning features
12/23/2014US8915085 Bleed assembly for a gas turbine engine
12/23/2014US8915061 Aircraft, propulsion system, and inlet with supersonic compression
12/23/2014US8915060 Method of varying a fan duct throat area
12/18/2014US20140366554 Cross reference to related applications
12/17/2014CN104220738A 具有单独的核心和推进单元的燃气涡轮机发动机 Having a core and a separate gas turbine propulsion engine unit
12/16/2014US8911203 Fan rotor support
12/16/2014US8910482 Aircraft engine nozzle
12/16/2014US8910465 Gas turbine engine and heat exchange system
12/11/2014US20140363276 Ultra high bypass ratio turbofan engine
12/10/2014CN104204491A 航空器用喷气引擎的风扇动叶片 For aircraft jet engine fan rotor blades
12/10/2014CN104204469A 具有气体监测器的气轮机控制系统 Gas turbine with a gas monitor control system
12/10/2014CN104204468A 用于涡轮喷气引擎的点火单元 For turbojet engine ignition unit
12/10/2014CN104204460A 具有径向保持力的空气阻滞环组件 Air having a radial blocking ring assembly holding force
12/10/2014CN104204459A 燃气涡轮发动机风扇驱动齿轮系统的扭矩框架衬套布置 Torque frame gas turbine engine fan drive gear system bushing arrangement
12/09/2014US8904795 Noise reducing device and jet propulsion system
12/09/2014US8904753 Thermal management system for gas turbine engine
12/09/2014US8904750 Gas turbine engine variable area exhaust nozzle
12/04/2014US20140356159 Low hub-to-tip ratio fan for a turbofan gas turbine engine
12/04/2014US20140352321 Gas turbine engine system and an associated method thereof
12/02/2014US8900083 Fan drive gear system integrated carrier and torque frame
12/02/2014US8899916 Torque frame and asymmetric journal bearing for fan drive gear system
12/02/2014US8899915 Geared architecture for high speed and small volume fan drive turbine
11/2014
11/27/2014US20140345254 Secondary nozzle for jet engine
11/27/2014US20140345253 Multi-nozzle flow diverter for jet engine
11/25/2014US8895134 Apparatus and method for coating a compressor housing
11/25/2014US8894351 Retaining ring
11/25/2014US8893502 Augmentor spray bar with tip support bushing
11/18/2014US8888439 Turbomachine casing assembly
11/18/2014US8887488 Power plant for UAV
11/18/2014US8887487 Geared turbofan gas turbine engine architecture
11/18/2014US8887486 Ram air fan inlet housing
11/18/2014US8887485 Three spool gas turbine engine having a clutch and compressor bypass
11/18/2014US8887484 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine
11/04/2014US8876467 Inner wall for a turbomachine nacelle
11/04/2014US8876465 Gas turbine engine
11/04/2014US8876462 System of contra-rotating propellers driven by a planetary gear train providing a balanced distribution of torque between the two propellers
11/04/2014US8876018 Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle
10/2014
10/28/2014US8870530 Gas turbine engine
10/28/2014US8869509 Accessory flow recovery system and method for thermal efficient pump and control system
10/28/2014US8869508 Gas turbine engine variable area fan nozzle control
10/28/2014US8869507 Translatable cascade thrust reverser
10/28/2014US8869505 Variable area fan nozzle and thrust reverser
10/28/2014US8869504 Geared turbofan engine gearbox arrangement
10/23/2014US20140314548 Turbine engine and vane system
10/21/2014US8863491 Gas turbine engine shaft bearing configuration
10/14/2014US8862362 Scheduling of variable area fan nozzle to optimize engine performance
10/14/2014US8858182 Fan blade with sheath
10/14/2014US8858164 Air discharge system for an aeronautical turbine engine compressor
10/14/2014US8858163 Ventilation inlet
10/14/2014US8857151 Corrugated core cowl for a gas turbine engine
10/09/2014WO2014163709A2 Platform for ceramic matrix composite turbine blades
10/09/2014US20140298772 Mischvorrichtung und turbofantriebwerk mit einer derartigen mischvorrichtung
10/09/2014DE102013205911A1 Mischvorrichtung und Turbofantriebwerk mit einer derartigen Mischvorrichtung Mixer and turbofan engine with such a mixing device
10/07/2014US8850824 Aircraft gas turbine with variable bypass nozzle by deforming element
10/07/2014US8850793 Turbine section of high bypass turbofan
10/02/2014WO2014160509A1 Gas turbine engine with three stream, variable area, vectorable nozzle
10/02/2014WO2014158244A2 Intercooled gas turbine with closed combined power cycle
10/02/2014US20140290213 Duct blocker seal assembly for a gas turbine engine
10/02/2014US20140290211 Turbine engine including balanced low pressure stage count
09/2014
09/30/2014US8845292 Blade-retaining device for turbomachine propeller
09/30/2014US8845291 Engine arrangement
09/30/2014US8845277 Geared turbofan engine with integral gear and bearing supports
09/30/2014US8844553 Passive boundary layer bleed system for nacelle inlet airflow control
09/30/2014US8844266 Variable bypass ratio augmented gas turbine engine
09/30/2014US8844265 Turbine section of high bypass turbofan
09/30/2014US8844264 Gas turbine engine with ejector
09/30/2014US8844263 Aircraft turbine engine and use of such a turbine engine
09/30/2014US8844262 Exhaust for a gas turbine engine
09/30/2014CA2637647C External wall of a fan conduit in a turbine engine
09/25/2014WO2014152875A1 Gas turbine engine architecture with nested concentric combustor
09/25/2014WO2014152101A1 Turbofan engine bearing and gearbox arrangement
09/25/2014WO2014151356A1 Geared architecture turbofan engine thermal management system and method
09/25/2014WO2014150500A1 Nacelle internal and external flow control
09/25/2014WO2014150377A1 Electrically coupled counter-rotation for gas turbine compressors
09/25/2014WO2014149100A1 Heat exchanger integrated with a gas turbine engine and adaptive flow control
09/25/2014US20140283501 Elongated geared turbofan with high bypass ratio
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