Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants › F02K 1 - Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
Patents for F02K 1 - Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (6,699)
12/2014
12/25/2014US20140373506 Reverse scissor thrist reverser for a turbine engine
12/24/2014CN104246196A 连接燃气涡轮发动机环形部件 Connecting a gas turbine engine annular member
12/24/2014CN104234869A 气流隔热保温航天冲压发动机 Airflow insulation aerospace ramjet
12/23/2014US8915060 Method of varying a fan duct throat area
12/18/2014US20140366554 Cross reference to related applications
12/17/2014CN204024855U 一种新型喷管隔热屏悬挂结构 A new nozzle heat shield suspension structure
12/17/2014CN204024854U 一种球面收敛二元矢量喷管冷却结构 A Spherical convergence of two yuan vectoring nozzle cooling structure
12/17/2014CN104214008A 一种新型尾锥 A new tail cone
12/17/2014CN104214007A 速度型做功机构发动机 Engine speed-type acting agency
12/17/2014CN101772634B 可移动反推整流罩以及设置有这种整流罩的推力反向器 Movable thrust reverser cowl and provided with such a thrust reverser cowl
12/16/2014US8910482 Aircraft engine nozzle
12/16/2014US8910464 Lift fan spherical thrust vectoring nozzle
12/11/2014US20140360158 Twin-door thrust reverser
12/10/2014CN204003152U 一种收敛喷管外罩 An astringent nozzle housing
12/10/2014CN204003151U 一种具有良好气动性能的中心体结构 A structure having a central body good aerodynamic performance
12/10/2014CN104204490A 用于飞行器涡轮喷气发动机的气体喷射锥体 Turbojet engines for aircraft gas jet cone
12/10/2014CN104204421A 可变截面喷嘴以及装配有该喷嘴的飞机涡轮喷气发动机机舱 Variable nozzle and nozzle fitted with the turbojet aircraft cabin
12/10/2014CN104196649A 一种新型二元遮挡旋流中心体结构 A new two yuan cyclone center block structure
12/10/2014CN104196648A 一种新型轴对称收敛喷管 A new axisymmetric convergent nozzle
12/10/2014CN102428263B 包括具有声音消除器的排放气体引导锥体的涡轮发动机 Canceller includes a sound guiding cone of the exhaust gas turbine engine
12/09/2014US8907595 Aircraft engine nacelle comprising a mobile cowl moved by electric motors
12/09/2014US8904801 Device and method for controlling vortex structures in a turbulent air jet
12/09/2014US8904795 Noise reducing device and jet propulsion system
12/09/2014US8904751 Thrust reverser assembly and method of operation
12/09/2014US8904750 Gas turbine engine variable area exhaust nozzle
12/04/2014US20140353399 Thrust reverser system with translating-rotating blocker doors and method of operation
12/02/2014US8899512 Acoustic attenuation panel for aircraft for engine nacelle
12/02/2014US8899013 Thrust reverser having locking/unlocking cascade vanes
11/2014
11/27/2014US20140345254 Secondary nozzle for jet engine
11/27/2014US20140345252 System, apparatus, and method for a virtual blocker
11/25/2014US8893503 Deployable divergent nozzle for a propulsive unit
11/20/2014US20140341744 Cellular acoustic structure for a turbojet engine and turbojet engine incorporating at least one such structure
11/18/2014US8892295 Control and monitoring system and method
11/18/2014US8887489 Noise control chevron for a nozzle, and nozzle and turboshaft engine provided with such a chevron
11/18/2014US8887484 Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine
11/13/2014US20140332627 Control and safety system for an airplane
11/13/2014US20140332604 Device for Fastening a Hollow Part
11/13/2014US20140332311 Noise suppressor
11/11/2014US8881502 Mixer that performs reciprocating rotary motion for a confluent-flow nozzle of a turbine engine, and a method of controlling it
11/06/2014US20140325957 System and apparatus for a split cascade
11/06/2014US20140325956 System, apparatus, and method for thrust vectoring
11/04/2014US8876043 Aircraft engine exhaust nozzle system for jet noise reduction
11/04/2014US8876018 Arrangement of thrust reverser flap link rods on the internal fixed structure of a turbojet engine nacelle
11/04/2014US8875520 Gas turbine engine device
11/04/2014US8875518 Nacelle with an adaptable outlet section
11/04/2014US8875486 Guide system for nacelle assembly
10/2014
10/30/2014US20140319243 Reverser having movable cascades, and translatably variable nozzle
10/30/2014US20140319242 Nozzle, structure element and method of producing a nozzle
10/28/2014US8870530 Gas turbine engine
10/28/2014US8869508 Gas turbine engine variable area fan nozzle control
10/28/2014US8869507 Translatable cascade thrust reverser
10/28/2014US8869506 Turbojet engine nacelle including a device for absorbing circumferential stresses
10/28/2014US8869505 Variable area fan nozzle and thrust reverser
10/28/2014US8869504 Geared turbofan engine gearbox arrangement
10/21/2014US8863893 Engine inlet varying impedance acoustic liner section
10/16/2014US20140305097 Fan variable area nozzle with cable actuator system
10/09/2014US20140301837 Door for a thrust reverser with doors
10/09/2014DE102013205911A1 Mischvorrichtung und Turbofantriebwerk mit einer derartigen Mischvorrichtung Mixer and turbofan engine with such a mixing device
10/09/2014DE102013006109A1 Antriebsvorrichtung einer variablen Ausströmdüse eines Fluggasturbinentriebwerks Drive means a variable exhaust nozzle of an aircraft gas turbine engine
10/08/2014EP2787210A1 Mixing device and turbofan engine with such a mixing device
10/07/2014US8850824 Aircraft gas turbine with variable bypass nozzle by deforming element
10/07/2014US8850823 Integrated aero-engine flowpath structure
10/02/2014WO2014160509A1 Gas turbine engine with three stream, variable area, vectorable nozzle
10/02/2014WO2014160486A1 Compact actuation system for a gas turbine engine exhaust nozzle
10/02/2014WO2014160449A2 Three stream, variable area fixed aperture nozzle with pneumatic actuation
10/02/2014WO2014159311A1 Ventilation system using thrust reverser linkages
10/02/2014WO2014158852A1 Engine thrust reverser lock
10/02/2014WO2014158237A2 Gas turbine engine configuration interface
09/2014
09/30/2014US8844863 Device for mechanically decoupled fastening of an aircraft component perfused by hot gas
09/30/2014US8844294 Gas turbine engine having slim-line nacelle
09/30/2014US8844264 Gas turbine engine with ejector
09/30/2014US8844262 Exhaust for a gas turbine engine
09/30/2014US8844261 Variable area fan nozzle thrust reverser
09/25/2014WO2014150500A1 Nacelle internal and external flow control
09/25/2014WO2014150426A1 Variable area fan nozzle with wall thickness distribution
09/25/2014WO2014149604A1 Apu exhaust system
09/25/2014WO2014149325A1 Internal/external single expansion ramp nozzle with integrated third stream
09/25/2014WO2014149292A1 Titanium aluminide turbine exhaust structure
09/25/2014WO2014147247A1 Actuation device for moving a movable cover of a thrust reverser
09/25/2014US20140284395 Gas turbine exhaust noise reduction
09/24/2014EP2781728A2 Thrust reverser inner fixed structure with corner fitting
09/24/2014EP2780574A1 Thrust reverser having twin doors
09/23/2014US8840064 Stub frame for a cascade thrust reverser structure
09/23/2014US8839601 Door for thrust reverser of an aircraft nacelle
09/23/2014CA2627521C Control method for actuating a thrust reverser
09/23/2014CA2527645C Bullnose step turbine nozzle
09/18/2014WO2014143281A1 Asymmetric fan nozzle in high-bpr separate-flow nacelle
09/18/2014WO2014143267A1 Gas turbine engine with low fan noise
09/18/2014WO2014140491A1 Mechanical inhibiting device integrated into a defence line of a thrust reverser
09/18/2014US20140270935 Engine Thrust Reverser Lock
09/18/2014US20140263737 Three stream, variable area fixed aperture nozzle with pneumatic actuation
09/18/2014US20140263712 Exhaust nozzle apparatus and method for multi stream aircraft engine
09/18/2014US20140260283 Gas turbine engine exhaust mixer with aerodynamic struts
09/18/2014US20140259661 Variable area fan nozzle with wall thickness distribution
09/18/2014US20140259631 Internal/external single expansion ramp nozzle with integrated third stream
09/17/2014EP2779367A2 Gas turbine engine actuation systems including high temperature actuators and methods for the manufacture thereof
09/17/2014EP2778380A2 Gas turbine engine exhaust mixer with aerodynamic struts
09/17/2014EP2776699A1 Thrust reverser device
09/16/2014US8834056 Bipod flexure ring
09/16/2014US8833515 Method for the production of a sound absorber, especially for a gas turbine exhaust cone
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