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)
11/2005
11/23/2005EP1598566A1 A fastener assembly for attaching a non-metal component to a metal component
11/23/2005EP1598562A1 A fastener assembly for attaching a non-metal component to a metal component
11/23/2005EP1597472A2 Confluent exhaust nozzle
11/22/2005US6966189 System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber
11/22/2005US6966175 Rotary adjustable exhaust nozzle
11/22/2005CA2225608C A thrust reverser system for a dual flow bypass turbojet with upstream clamshells
11/20/2005CA2500677A1 A fastener assembly for attaching a non-metal component to a metal component
11/20/2005CA2500439A1 A fastener assembly for attaching a non-metal component to a metal component
11/20/2005CA2500430A1 Divergent flap for a gas turbine engine
11/17/2005WO2005107382A2 Method and device for reducing engine noise
11/17/2005US20050256682 Method of evaluation of space systems for safety assurance and residual risk to flightcrew
11/17/2005US20050252716 Electronically controlled dual chamber variable resonator
11/17/2005US20050252193 System and method for controlling the temperature and infrared signature of an engine
11/17/2005CA2547846A1 Method and device for reducing engine noise
11/16/2005EP1595069A2 Self stowing thrust reverser
11/16/2005EP1595068A2 Ventilated confluent exhaust nozzle
11/16/2005EP1595067A2 Recessed engine nacelle
11/15/2005US6964169 Hollow tapered body flattened in the transverse direction, wall being divided transversely into four adjacent parts, trapezoidal wall, made of refractory fibers embedded in another refractory matrics; vapor deposit refractory matrics; durability
11/15/2005CA2234436C Device for closing and locking the blockers of a thrust reverser
11/10/2005US20050247046 Jet nozzle mixer
11/10/2005DE102004018725A1 Dämpfung von Schwingungen einer Brennkammer durch Resonatoren Damping of oscillations of a combustion chamber through resonators
11/09/2005CN1693691A Air compression aeroengine
11/08/2005US6962044 Method and apparatus of asymmetric injection into subsonic flow of a high aspect ratio/complex geometry nozzle
11/03/2005US20050242557 Anti-roll thrust system for hydrogen powered vehicles
11/03/2005DE102004022358B3 Method for coating substrates with hard materials, useful in producing radiation guides, comprises spraying them with induction plasma
10/2005
10/27/2005WO2005100858A1 Damping of vibration of a combustion chamber by resonators
10/27/2005US20050235630 High temperature dynamic seal for scramjet variable geometry
10/27/2005US20050235629 Cooling scheme for scramjet variable geometry hardware
10/27/2005US20050235628 Ejector cooled nozzle
10/26/2005EP1588102A2 Heat shield element, combustion chamber and gas turbine
10/26/2005CN1224779C Stopper type jet pipe
10/20/2005US20050230176 Anti-roll thrust system for vehicles
10/20/2005US20050229586 Variable area nozzle
10/20/2005US20050229585 Gas turbine engine exhaust nozzle
10/20/2005US20050229584 Aircraft structure that includes a duct for guiding fluid flow therethrough
10/20/2005US20050229583 Hybrid propulsion system
10/19/2005EP1585896A1 Apparatus and method for controlling primary fluid flow using secondary fluid flow injection
10/19/2005EP1470329B1 Nozzle throat area control apparatus and method
10/19/2005EP1409866B1 Thrust reverser position determination system and method
10/13/2005WO2005094227A2 Spider actuated thrust reverser
10/13/2005WO2005081864A9 Jet nozzle mixer
10/13/2005US20050223695 Thrust vector control system for a plug nozzle rocket engine
10/13/2005US20050223694 Ducted air power plant
10/13/2005US20050223692 Apparatus and method for reduction of jet noise from turbofan engines having separate bypass and core flows
10/13/2005US20050223691 Apparatus and method for reduction jet noise from single jets
10/13/2005CA2536739A1 Spider actuated thrust reverser
10/12/2005EP1583899A2 Controlled autoignition propellant systems
10/06/2005US20050217271 Turbine engine nozzle
10/06/2005US20050217239 Methods and apparatus for exhausting gases from gas turbine engines
10/06/2005US20050217237 Thrust, with or without the ejection of propellant
10/05/2005EP1582730A1 Apparatus for exhausting gases from gas turbine engines
10/05/2005EP1448883B8 Noise attenuator arrangement
09/2005
09/30/2005CA2502374A1 Methods and apparatus for exhausting gases from gas turbine engines
09/29/2005WO2005091272A1 Assembly for reducing noise in turbofan engines
09/29/2005WO2005090156A1 Annular acoustic panel
09/29/2005US20050214107 Methods and apparatus for operating gas turbine engines
09/29/2005US20050211822 Variable cycle propulsion system with gas tapping for a supersonic airplane, and a method of operation
09/29/2005US20050210864 Device for supplying cooling air to exhaust nozzle flaps
09/29/2005US20050210861 Axial divergent section slot nozzle
09/29/2005US20050210860 Methods and apparatus for operating gas turbine engines
09/28/2005EP1580420A1 Axial divergent section slot nozzle
09/28/2005EP1580419A1 Primary nozzle with chevrons for bypass turboreactor engine of an aircraft and aircraft with such a nozzle
09/28/2005EP1580418A2 Gas turbine engine comprising a noise suppression system
09/28/2005EP1580417A2 Noise suppression system for a gas turbine
09/28/2005EP1579112A1 Thrust reverser comprising optimised deflector gratings
09/28/2005CN2729342Y Fuel-oil atomzation nozzle
09/27/2005US6948317 Methods and apparatus for flade engine nozzle
09/27/2005US6948307 Rocket engine nozzle that is steerable by means of a moving diverging portion on a cardan mount
09/22/2005WO2005001247A3 Confluent exhaust nozzle
09/22/2005US20050205354 Dual chamber variable geometry resonator
09/22/2005US20050205351 Noise reduction tubes
09/22/2005US20050204742 Confluent exhaust nozzle
09/21/2005EP1577530A1 Device and method for providing ignition to a post-combustor for bypass gas turbine
09/21/2005EP1577505A2 Support bracket for turboprop engine nozzle
09/21/2005EP1576273A1 Thurst reverser system power drive unit with dual sequential torque decoupler
09/21/2005CN1670349A Gas turbine engine component having bypass circuit
09/20/2005CA2243099C Turbofan thrust reverser with axially guided blockers attached to the primary cowling
09/15/2005WO2005085620A1 Variable cycle engine for propelling subsonic aircraft
09/15/2005US20050198940 Ablative afterburner
09/14/2005EP1574699A1 Afterburner with ablative nozzle
09/13/2005US6942181 Passive cooling system for auxiliary power unit installation
09/13/2005CA2224534C Divergent petal arrangement for a convergent-divergent aircraft engine nozzle
09/09/2005WO2005081864A2 Jet nozzle mixer
09/08/2005US20050193716 Jet exhaust noise reduction system and method
09/08/2005DE10242393A1 Abgasabschirmung für ein Flugzeugtriebwerk Exhaust shield for an aircraft engine
09/06/2005US6938408 Thrust vectoring and variable exhaust area for jet engine nozzle
09/01/2005US20050188678 Component for being subjected to high thermal load during operation and a method for manufacturing such a component
09/01/2005US20050188676 Ventilated confluent exhaust nozzle
08/2005
08/31/2005EP1568868A2 High by-pass ratio turbofan
08/31/2005CN1662419A Ducted air power plant
08/30/2005US6935834 Noise reduction conduit for static components in aircraft engines
08/30/2005US6935118 Exhaust nozzle segmented basesheet and production method thereof
08/30/2005US6935098 Turbomachine nozzle with noise reduction
08/30/2005US6935097 Lock assembly that inhibits thrust reverser movement at or near the stowed position
08/24/2005CA2498242A1 Process for improving the ignition performance of a post-combustion device for a turbofan and post-combustion device with improved ignition performance
08/18/2005DE102004004076A1 Turbo blade drive unit has compressor combustion unit turbine and mixer nozzle with chevron shape giving subsonic exhaust gas outflow speeds
08/17/2005EP1448883B1 Noise attenuator arrangement
08/11/2005WO2005021934A3 Ventilated confluent exhaust nozzle
08/11/2005US20050172611 Sinuous chevron exhaust nozzle
08/11/2005US20050172609 Turbojet having a large bypass ratio
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