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)
09/2014
09/16/2014US8833055 Locking/unlocking device for a thrust reverser with a sliding cover and adaptive nozzle for aircraft engine nacelle
09/14/2014CA2846520A1 Aerodynamically active stiffening feature for gas turbine recuperator
09/12/2014WO2014138416A1 Fixturing for thermal spray coating of gas turbine components
09/12/2014WO2014137553A1 Exhaust system having a flow path liner supported by structural duct segments
09/12/2014WO2014135786A1 Nozzle having a variable neck section for a spacecraft thruster provided with a mobile needle
09/12/2014CA2845455A1 Gas turbine engine exhaust mixer with aerodynamic struts
09/11/2014US20140252167 Reverse core engine thrust reverser for under wing
09/11/2014US20140250895 Modulated ejector cooling
09/11/2014US20140250863 Rear mounted reverse core engine thrust reverser
09/10/2014EP2773861A1 Cascade-type thrust reverser with one-piece mobile cowl
09/09/2014US8831900 System for controlling at least one actuator for thrust reverser cowlings on a turbojet engine and method for testing said system
09/09/2014US8827199 Turboshaft engine supporting pylon covered with a porous material and turboshaft engine/pylon assembly
09/09/2014US8826669 Gas turbine exhaust case
09/09/2014US8826637 Arrangement for the discharge of oil-venting air on a gas-turbine engine
09/04/2014WO2014134262A1 Repair of surface damage at edges of cellular panels
09/04/2014WO2014099077A3 Gas turbine engine asymmetric nozzle guide vanes
09/04/2014US20140246514 Turbomachine thrust reverser
09/04/2014US20140245716 Twin-door thrust reverser
09/04/2014US20140245715 Primary cowl of a turbofan comprising a rotating ring having micro-jets
09/03/2014EP2771560A1 Telescoping fluid porting tube
09/03/2014EP2771559A1 Device for attaching a hollow part
09/02/2014US8821115 Seal assembly
09/02/2014US8820088 Variable area fan nozzle with acoustic system for a gas turbine engine
09/02/2014US8820084 Apparatus for controlling a boundary layer in a diffusing flow path of a power generating machine
08/2014
08/28/2014WO2014130361A1 Turbofan engine including third flowpath exhaust nozzle
08/28/2014US20140239084 Tandem thrust reverser with sliding rails
08/28/2014US20140239083 Pivot thrust reverser surrounding inner surface of bypass duct
08/28/2014US20140237990 Variable area fan nozzle with wall thickness distribution
08/27/2014EP2770190A2 Exhaust section for bypass gas turbine engines
08/26/2014US8813907 Noise reduction system with chamber
08/26/2014US8813503 Gas turbine control systems and methods
08/22/2014CA2843075A1 Exhaust section for bypass gas turbine engines
08/21/2014US20140234089 Actuating assembly for a thrust reverser of an aircraft engine
08/21/2014US20140234074 Method of mixing between a primary flow and a secondary flow in a turbine engine, corresponding device and turbine engine
08/21/2014US20140230404 Gas turbine engine exhaust mixer
08/20/2014EP2766259A1 Rear nacelle assembly for a turbojet engine
08/19/2014CA2599095C Turbine exhaust strut airfoil and gas path profile
08/19/2014CA2585879C Exhaust assembly for propulsion gases in an aircraft with twist elbow
08/14/2014WO2014123595A2 Thrust reverser system with translating rotating cascade and method of operation
08/14/2014DE102014101508A1 Verfahren zur Vorhersage von Fehlern in einem Flugzeug-Schubumkehrsystem A method for predicting errors in an airplane thrust reverser system
08/13/2014EP2765295A2 A panel mounting arrangement
08/13/2014CN103987949A 一种涡轮发动机的缩放喷嘴 A turbine engine nozzle scaling
08/13/2014CN103987948A 喷管装置及其制造方法 Nozzle device and manufacturing method thereof
08/13/2014CN103979114A 用于预测飞机反推力装置系统中的故障的方法 Prediction of the aircraft thrust reverser system for a fault
08/13/2014CN101835969B 格栅式推力反向器 Grill-type thrust reverser
08/12/2014US8800294 Integrated aero-engine flowpath structure
08/12/2014US8800262 Thrust reverser for a turbofan engine nacelle
08/12/2014US8800261 Gas turbine engine with noise attenuating variable area fan nozzle
08/12/2014US8800260 Fan variable area nozzle with cable actuator system
08/12/2014US8800259 Thrust vector system
08/12/2014CA2842327A1 Method for predicting faults in an aircraft thrust reverser system
08/12/2014CA2592483C Exhaust cone for channeling a gas stream downstream from a turbine
08/07/2014US20140217195 Nacelle
08/07/2014US20140216005 Gas Turbine Engine Assembly Including A Thrust Reverser
08/07/2014US20140216002 Gas turbine engine having slim-line nacelle
08/06/2014EP2762714A2 Exhaust cone
08/06/2014EP2762408A1 Bi-directional ventilation systems for use with aircraft and related methods
08/06/2014EP2761158A1 Thrust reverser gates having side openings
08/05/2014US8794007 Rocket propulsion device and method for assembling rocket propulsion device
08/05/2014US8793973 Thrust reverser for a dual-flow turbine engine nacelle
08/05/2014CA2674927C Translatable thrust inverter for jet engine
08/01/2014DE202012013035U1 Turbo-Rotor-Triebwerk Turbo-rotor engine
07/2014
07/30/2014CN203740127U 变体无人战斗机 Variants of unmanned aircraft
07/29/2014US8789355 Support structure and mounting componet for a thrust inverter
07/29/2014CA2619561C Variable section flow mixer for dual flow turbojet for supersonic aircraft
07/24/2014WO2014111709A1 Rocket motors and their use
07/23/2014EP2757241A2 Gas turbine exhaust noise reduction
07/23/2014CN103939235A 一种用于短距垂直起降发动机的旋转式推力矢量喷管 Rotary thrust vectoring nozzle for a short-range VTOL engine
07/23/2014CN103939234A 一种变循环发动机可调机构中的共同驱动式后涵道引射器 A variable cycle engine Adjustable bodies after co-driven ducted ejector
07/23/2014CN102748160B 用于固体火箭发动机柔性喷管的柔性接头总成及其制备方法 Flexible joint assembly and preparation method for solid rocket motor nozzle flexible
07/23/2014CN102308401B 燃气涡轮的热电生成 Thermoelectric generation gas turbine
07/22/2014US8783621 Method and system for controlling a set of at least two satellites, designed to provide a service on a geostationary orbit, rendering said service on a non-geostationary orbit
07/22/2014US8783412 Sound absorber for a gas turbine exhaust cone, and method for the production thereof
07/22/2014US8783010 Cascade type thrust reverser having a pivoting door
07/22/2014US8782896 Method for the manufacture of an ejector nozzle tube
07/17/2014WO2014109785A1 Below wing reverse core gas turbine engine with thrust reverser
07/17/2014WO2014066508A3 Unducted thrust producing system architecture
07/17/2014WO2014058502A3 Ceramic centerbody for an aircraft gas turbine engine and method of making
07/17/2014US20140196436 Operation stabilization method and operation stabilization apparatus for supersonic intake
07/16/2014EP2753813A1 Turbofan engine with convergent - divergent exhaust nozzle
07/16/2014CN203717160U 一种喷气式发动机 A jet engine
07/16/2014CN103925115A 一种变循环发动机可调机构中的拉杆轴承平动式前涵道引射器 A variable cycle engine Adjustable institutions rod bearing translational front ducted ejector
07/16/2014CN103925114A 一种变循环发动机可调机构中的滚轮滑块平动式前涵道引射器 A variable cycle engine Adjustable institutions translational front wheel slide ducted ejector
07/15/2014US8776946 Gas turbine exhaust cone
07/15/2014US8776527 Techniques to reduce infrared detection of a gas turbine engine
07/15/2014CA2588950C Central body for a turbojet engine exhaust channel
07/15/2014CA2573521C Core exhaust mixer, having a variable area, for turbo-fan jet engines of supersonic aircraft
07/10/2014US20140191080 Aircraft propulsion system comprising an aft pylon fairing with lateral walls that are profiled for injecting cool air along a thermal protection floor
07/09/2014CN203702369U 喷气发动机尾部横截面为矩形的矢量喷管 Jet engine tail rectangular cross section of vectoring nozzle
07/09/2014CN103917766A 推力反向装置 Thrust reverser system
07/09/2014CN103917765A 具有双门的推力反向器 Thrust reverser with double doors
07/08/2014US8770339 Silencer for an auxiliary power unit of an aircraft
07/08/2014US8769959 Nozzle with an adjustable throat
07/08/2014US8769926 Thrust reverser having an aerodynamic coupling for a front frame
07/08/2014CA2585920C Exhaust assembly forming a horizontal elbow for propulsion gases in an aircraft
07/08/2014CA2585878C Exhaust assembly for propulsion gases in an aircraft forming an elbow
07/03/2014WO2014105529A1 Flow diverter to redirect secondary flow
07/03/2014US20140182265 Rocket Propulsion Systems, and Related Methods
07/02/2014CN103899434A 一种多轴固定几何气动矢量喷管结构 One kind of multi-axis fixed geometry vectoring nozzle structure
07/02/2014CN103899433A 一种新型激波控制推力矢量喷管结构 A new shock thrust vector control nozzle structure
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