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)
06/2012
06/26/2012US8205434 Joint for a shape memory material
06/26/2012CA2472935C Device for reducing jet noise from a turbine engine
06/21/2012WO2012080604A1 Nacelle for a bypass turbojet engine
06/21/2012US20120151899 Morphing structure and method
06/21/2012CA2820774A1 Nacelle for a bypass turbojet engine
06/20/2012EP2466101A2 System and method for operating a thrust reverser for a turbofan propulsion system
06/20/2012EP2466100A2 Method and apparatus for variable exhaust nozzle exit area
06/20/2012EP2464850A2 Thrust reversal device
06/19/2012US8201390 Partial cascade thrust reverser
06/14/2012WO2012075844A1 Silencer
06/14/2012US20120145808 Method and apparatus for variable exhaust nozzle exit area
06/14/2012CA2754855A1 Method and apparatus for variable exhaust nozzle exit area
06/13/2012EP2462331A1 Nested fairing thrust reverser
06/13/2012EP2462330A2 High stiffness shape memory alloy actuated aerostructure
06/13/2012CN102493894A Nozzle exhaust mixing method and device based on pneumatic tab technique
06/13/2012CN101809849B Double-acting telescopic linear actuator with single-motor drive system
06/12/2012US8196410 Stress reduction feature to improve fuel nozzle sheath durability
06/12/2012CA2660001C Thrust reverser nozzle for a turbofan gas turbine engine
06/07/2012WO2012074648A2 Thrust reverser and variable area fan nozzle actuation system and method
06/07/2012WO2012010774A3 Turbojet engine nacelle
06/07/2012US20120138707 Thrust reversal device
06/07/2012US20120137656 Actuation system
06/07/2012US20120137654 Thrust Reverser and Variable Area Fan Nozzle Actuation System and Method
06/07/2012CA2810410A1 Thrust reverser and variable area fan nozzle actuation system and method
06/06/2012EP2461010A1 Active fan flutter control
06/06/2012EP2459862A2 Integrated thrust reverser assembly
06/06/2012EP2459445A2 Engine assembly for an aircraft of which the attachment strut comprises a structural case forming an internal radial delimitation of the secondary flow
06/05/2012CA2470926C Aircraft engine in which there is a small clearance separating the fan cowls and the thrust inverter cowls
05/2012
05/30/2012EP2458028A2 Coating a perforated surface
05/30/2012CN102483012A Structuring assembly for an exhaust nozzle
05/30/2012CN102483011A 推力反向装置 Thrust reversing device
05/30/2012CN102482945A A mounting apparatus
05/30/2012CN101782026B Divergent dual-throat nozzle with gas-injection divergent section
05/30/2012CN101573524B Nacelle for aircraft jet engine and aircraft including such nacelle
05/29/2012US8186145 Rocket nozzles for unconventional vehicles
05/29/2012US8186143 Morphing structure and method
05/24/2012WO2012067743A1 Thermal integration of thermoelectric device
05/24/2012WO2012066211A1 Turbojet engine nacelle reinforcing structure
05/24/2012WO2012066210A2 Nacelle for an aircraft bypass turbojet engine
05/24/2012US20120124962 Method of varying a fan duct throat area
05/24/2012CA2816455A1 Turbojet engine nacelle reinforcing structure
05/24/2012CA2816255A1 Nacelle for an aircraft bypass turbojet engine
05/23/2012CN202228210U An aircraft engine outer adjusting sheet
05/23/2012CN102472201A High stiffness shape memory alloy actuated aerostructure
05/23/2012CN102472112A 用于例如推力反向器罩的可移动飞行器发动机舱元件的驱动系统 Aircraft nacelle movable element, for example, the driving system of the thrust reverser cover
05/23/2012CN101537397B Fuel prefilming air atomizer spray nozzle
05/23/2012CN101384485B Turbojet engine nacelle with lateral opening of covers
05/22/2012CA2484262C A rocket engine nozzle that is steerable by means of a moving diverging portion on a cardan mount
05/17/2012US20120117940 Gas turbine engine with pylon mounted accessory drive
05/17/2012US20120117939 Turboshaft engine with reduced noise emission for aircraft
05/16/2012EP2452049A1 Actuating system for a movable aircraft engine nacelle element, such as a thrust reverser cover
05/16/2012EP2181262B1 Variable area fan nozzle with bypass flow
05/16/2012CN102459856A Thrust reversing device
05/10/2012WO2012059677A2 Aircraft turbojet engine thrust reverser with a lower number of actuators
05/10/2012WO2012059662A1 Thrust reverser device without a control rod in the stream
05/10/2012US20120111662 Engine exhaust
05/10/2012US20120110980 Variable area fan nozzle fan flutter management system
05/10/2012US20120110979 Flutter sensing system for a gas turbine engine
05/10/2012CA2815613A1 Thrust reverser device without a control rod in the stream
05/10/2012CA2814384A1 Aircraft turbojet engine thrust reverser with a lower number of actuators
05/09/2012CN102449294A Thrust reverser for a dual-flow turbine engine nacelle
05/09/2012CN102448822A Aircraft engine nacelle comprising a mobile cowl moved by electric motors
05/09/2012CN102444499A Exhaust mixing method of refiling pneumatic ribbed jet pipe and device thereof
05/09/2012CN101292083B Turbojet engine with attenuated jet noise
05/09/2012CN101263295B Method for attenuating the noise of a turbofan
05/08/2012US8172175 Pivoting door thrust reverser for a turbofan gas turbine engine
05/03/2012DE102010049885A1 Turbo jet engine for aircraft, has static support tube concentrically supported within low pressure shaft, where front end of tube is guided into front area of engine and motor-generator-unit is arranged at front end of tube
05/02/2012EP2447520A2 Compliant sealing joint for an aircraft exhaust system
05/02/2012EP2447519A2 Gas turbine engine with variable area fan nozzle
05/02/2012CN102439282A Cowling for a turbine engine nozzle provided with side fins for reducing the noise of the jet
05/02/2012CN102434315A Bypass type double-throat passive vectoring sprayer nozzle
05/02/2012CN101528543B Side-opening jet engine nacelle
05/01/2012US8170771 Fluid-powered thrust reverser actuation system speed control
05/01/2012US8166763 Gas turbine fuel injector with a removable pilot assembly
04/2012
04/26/2012WO2012052552A1 Actuation system for a propulsive unit of an airplane
04/26/2012US20120097761 Twelve-hour structure for thrust reverser, in particular with grids
04/26/2012US20120096830 Turbine and method thereof
04/26/2012CA2814159A1 Actuation system for a propulsive unit of an airplane
04/25/2012EP2444645A2 Gas turbine engine with variable area fan nozzle
04/25/2012EP2192289B1 Intake silencer for gas turbine
04/25/2012CN202203066U Hot-punching engine
04/25/2012CN202202986U 引射喷气发动机 Ejector jet engine
04/25/2012CN102428263A Turbine Engine Comprising An Exhaust-Gas Guide Cone With A Sound Suppressor
04/24/2012US8162257 Nacelle for double flow engine
04/24/2012US8162101 Ram intake unit having a sound absorbing structure
04/24/2012US8161754 Continuously variable flow nozzle assembly
04/24/2012CA2673001C Jet flow discharge nozzle and jet engine
04/24/2012CA2466759C Fuel nozzle sheath retention ring
04/19/2012WO2012049386A1 Device for connecting a thrust reverser front frame to a fan casing and nacelle incorporating such a device
04/19/2012WO2012025690A3 Method for mounting shielding on a turbine casing, and mounting assembly for implementing same
04/19/2012US20120091270 Aircraft configuration
04/19/2012CA2811147A1 Device for connecting a thrust reverser front frame to a fan casing and nacelle incorporating such a device
04/18/2012EP2440768A1 Thrust reversing device
04/18/2012EP2118476B1 Method for controlling electric motors of a thrust reverser
04/18/2012EP1878903B1 Air compression engine
04/18/2012CN202194736U 一种大范围可调节离心式喷嘴 One kind of large-scale centrifugal adjustable nozzle
04/18/2012CN102417030A Air-discharge device for an airplane turbofan engine
04/17/2012US8157207 Jet engine nozzle exit configurations, including projections oriented relative to pylons, and associated systems and methods
04/17/2012US8156745 Exhaust nozzle seal with segmented basesheet
04/17/2012US8156727 Fan nozzle of adjustable section
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