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)
12/2013
12/04/2013CN103423024A Control and suspension mechanism for binary spray pipe contraction section
12/04/2013CN103423023A Binary convergent-divergent nozzle of pulse detonation engine
12/04/2013CN103419935A Vertical take-off and landing aircraft in saucer-shaped arrangement and based on novel high-lift device
12/04/2013CN103419923A Thrust gain device with high-speed wall attached air flow
12/04/2013CN102588080B Dynamic fluid gas working medium compression system
12/04/2013CN102301123B Soundproof exhaust pipe for a turbine engine
11/2013
11/28/2013US20130313333 System of support thrust from wasted exhaust
11/28/2013DE102012208673A1 Device for discharging oil ventilation air from lubrication oil venting system of dual flow jet engine, has air outlet formed at suction side and at pressure side such that oil ventilation air is exhausted over air outlet into flow channel
11/27/2013EP2667005A2 Thrust reverser system
11/27/2013EP2665911A1 Aircraft turbojet engine thrust reverser with a reduced number of latches
11/27/2013EP2665910A1 Aviation gas turbine thrust reversing device
11/27/2013EP2665909A2 Nacelle for an aircraft bypass turbojet engine
11/27/2013EP2665908A2 Nacelle for an aircraft bypass turbojet engine
11/27/2013EP2665904A1 Sound absorber for a gas turbine exhaust cone, and method for the production thereof
11/27/2013EP2665899A2 Method for the production of a sound absorber, especially for a gas turbine exhaust cone
11/27/2013EP2665898A2 Gas turbine exhaust cone
11/26/2013US8590316 CMC mixer with structural outer cowling
11/26/2013US8590287 Device for opening and closing a thrust reverser door of a jet engine
11/24/2013CA2807905A1 Thrust reverser system
11/21/2013US20130306755 Linked Ring Petal Actuation for Variable Area Fan Nozzle
11/21/2013US20130306400 Method of Designing and Making an Acoustic Liner for Jet Aircraft Engines
11/21/2013US20130305727 Built-up composite structures with a graded coefficient of thermal expansion for extreme environment applications
11/20/2013EP2664773A2 Linked ring petal assembly for variable area fan nozzle
11/20/2013EP2663762A1 Door for thrust reverser of an aircraft nacelle
11/20/2013EP2663741A1 Device for linking a front frame to a fan casing
11/20/2013EP2179194B1 Spring for a cascade-type thrust reverser shutter for an aircraft jet engine
11/20/2013EP2074309B1 Nacelle assembly for a high-bypass gas turbine engine and corresponding method of varying a fan nozzle exit area
11/20/2013EP2069630B1 Nacelle assembly and corresponding method
11/20/2013EP2064433B1 Gas turbine engine system and corresponding method for controlling a bypass airflow
11/19/2013US8584356 Method of manufacturing a CMC flow mixer lobed structure for a gas turbine aeroengine
11/16/2013CA2807989A1 Linked ring petal actuation for variable area fan nozzle
11/14/2013WO2013167825A1 Thrust reverser with controlled-deployment blocking flap
11/14/2013US20130298524 Device for linking a front frame to a fan casing
11/14/2013US20130298523 Constant pressure aerospike thruster
11/12/2013US8583294 Actuation control system
11/12/2013US8578716 Valve system for a gas turbine engine
11/12/2013US8578699 Control system for turbojet engine nacelle
11/12/2013US8578698 Cascade-type thrust reverser for jet engine
11/12/2013CA2637901C Air inlet shroud structure
11/07/2013WO2013137951A3 Flexible leaf spring seal for sealing an air gap between moving turbine engine exhaust nozzle parts
11/07/2013US20130292490 Door for thrust reverser of an aircraft nacelle
11/07/2013US20130292489 Thrust reverser having a lockable variable nozzle section
11/07/2013DE102012009228A1 Jet propulsion system for vehicle e.g. watercraft e.g. ship, has velocity component that is directed forward in travel direction based on vector sum of pulsed currents entering pulse balance space to which pulsed currents are flowed
11/06/2013EP2660454A2 Thrust reverser assembly and method of operation
11/06/2013EP2660442A2 Integrated thermal protection and leakage reduction in a supersonic air intake system
11/06/2013EP2660148A1 Overpressure door for aircraft
11/06/2013EP2659118A1 Flight vehicle, propulsion system and thrust vectoring system
11/06/2013CN101675238B Exhaust system for gas turbine
11/05/2013US8572986 Retainer for suspended thermal protection elements in a gas turbine engine
10/2013
10/31/2013WO2013163510A1 Connecting gas turbine engine annular members
10/31/2013WO2013160627A1 Turbofan engine nacelle with downstream section
10/31/2013WO2013160308A1 Actuating device for moving a mobile cap of a thrust reverser
10/31/2013WO2013160298A1 Actuating device for moving a thrust reverser
10/31/2013WO2013119314A3 Channeled spring seal for sealing an air gap between moving plates
10/31/2013US20130283799 Resonance damper for damping acoustic oscillations from combustor
10/30/2013EP2655191A1 Inner structure for an aircraft nacelle
10/30/2013CN103375302A Turboprop engine and usage method thereof
10/30/2013CN101981300B Device for reducing noise generated by aircraft jet engine with fluid jets of same orientation
10/30/2013CN101922380B Actuation system for translating variable area fan nozzle
10/30/2013CA2813241A1 Thrust reverser assembly and method of operation
10/29/2013CA2796895C Turbine exhaust case and method of making
10/24/2013WO2013158180A2 Variable area fan nozzle fan flutter management system
10/24/2013WO2013158169A1 Method of using an afterburner to reduce high velocity jet engine noise
10/24/2013US20130277454 Aircraft propulsion assembly
10/23/2013EP2653701A1 Control apparatus for a variable section nozzle of an aircraft
10/23/2013EP2653700A2 High bleed flow muffling system
10/23/2013EP2651764A1 Nacelle for a bypass turbojet engine
10/23/2013CN103370522A Cowl assembly
10/23/2013CN103362688A Thrust reverser actuator with primary lock
10/22/2013US8566000 System and method for controlling a single-spool turboshaft engine
10/22/2013US8561385 Flying object
10/22/2013US8561384 Fan exhaust nozzle for turbofan engine
10/22/2013CA2606525C Air compression type engine for aviation
10/22/2013CA2592794C Cowling for turbine engine nozzle with triangular inflection point patterns to reduce jet noise
10/22/2013CA2592484C Cowling for turbine engine nozzle with triangular double top patterns to reduce jet noise
10/22/2013CA2542717C Aircraft engine exhaust nozzle
10/17/2013WO2013152793A1 Reflection silencer
10/16/2013EP2650519A2 Thrust reverser actuator with primary lock
10/16/2013CN102251879B Differential adjustable unilateral expansion nozzle
10/16/2013CN101849094B A device and method for controlling vortex structures in a turbulent air jet
10/15/2013US8556027 Eductor exhaust silencer assembly with bypass gasflow
10/15/2013CA2545761C Methods and apparatus for assembling gas turbine engines
10/10/2013WO2013151304A1 Power transmission apparatus for jet engine
10/10/2013US20130263600 Assembly including a reverse thrust device and system for actuating said device
10/09/2013EP2646673A2 Thrust reverser and variable area fan nozzle actuation system and method
10/08/2013CA2592272C Rotary movement mixer for a confluent flow nozzle of a turbine engine
10/03/2013WO2013144512A1 Integration of parts of an afterbody of an aircraft engine
10/03/2013WO2013103427A3 Linear detonation wave diverter
10/03/2013US20130255225 Gas turbine engine thrust reverser system
10/02/2013EP2644924A1 Jam tolerant actuator decoupler
10/02/2013CN103334850A Connecting rod type two-dimensional jet pipe contraction section control mechanism
10/02/2013CN103334849A Double-sliding beam type two-dimensional convergent-divergent nozzle control mechanism for single actuator systems
10/02/2013CN102105666B Method and device for implementing the thrust reversers of an aircraft
10/02/2013CN101680395B Multiple-acting linear actuator
10/01/2013US8548714 Method for making uniform the thrust command of the engines of an aircraft
10/01/2013US8544278 Turboshaft engine with reduced noise emission for aircraft
09/2013
09/26/2013WO2013141939A2 Method of manufacturing a turbomachine component, an airfoil and a gas turbine engine
09/26/2013WO2013141932A1 Gas turbine engine with fan variable area nozzle for low fan pressure ratio
09/26/2013WO2013141930A1 Gas turbine engine with low fan pressure ratio
09/26/2013WO2013140088A1 Variable-section jet pipe and aircraft turbojet engine nacelle equipped with such a jet pipe
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