Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02K - Jet-propulsion plants
More topics under "F02K - Jet-propulsion plants" (18,201)
F02K 1 - Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (6,699)
F02K 3 - Plants including a gas turbine driving a compressor or a ducted fan (4,580)
F02K 5 - Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan (170)
F02K 7 - Plants in which the working-fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof (1,599)
F02K 9 - Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (4,689)
F02K 99 - Subject matter not provided for in other groups of this subclass (464)
Patents for F02K - Jet-propulsion plants (76)
03/2013
03/26/2013US8403629 Stator for a jet engine, a jet engine comprising such a stator, and an aircraft comprising the jet engine
12/2012
12/11/2012US8327617 Outlet nozzle for a jet engine, an aircraft comprising the outlet nozzle and a method for controlling a gas flow from the jet engine
07/2012
07/10/2012US8215096 Outlet device for a jet engine and a craft comprising such an outlet device
07/10/2012CA2536759C Induction coupled variable nozzle
03/2011
03/08/2011US7900460 Outlet device for a jet engine and a jet engine comprising such an outlet device
07/2010
07/13/2010US7753311 Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine
04/2010
04/01/2010WO2006049552A9 Outlet device for a jet engine and a craft comprising such an outlet device
10/2009
10/21/2009CN100552200C Rotary injector
08/2009
08/27/2009US20090211224 Outlet device for a jet engine and a craft comprising such an outlet device
07/2009
07/16/2009US20090180872 Gas turbine casing for enclosing a gas turbine component
09/2008
09/04/2008US20080213088 Stator for a Jet Engine, a Jet Engine Comprising Such a Stator, and an Aircraft Comprising the Jet Engine
06/2008
06/25/2008CN101208509A Turbo rocket with real Carnot cycle
06/18/2008CN101201015A 旋转喷射器 Rotary injector
05/2008
05/08/2008US20080104940 Device for Controlling a Gas Flow, a Jet Engine Comprising the Device and an Aircraft Comprising the Device
02/2008
02/26/2008US7334998 Low-noise fan exit guide vanes
01/2008
01/24/2008US20080016873 Outlet Device for a Jet Engine and a Jet Engine Comprising Such an Outlet Device
12/2007
12/27/2007US20070295860 Propulsion System, Aircraft Comprising the Propulsion System and an Outlet Device for a Jet Engine
11/2007
11/29/2007US20070271901 An outlet nozzle for a jet engine, an aircraft comprising the outlet nozzle and a method for controlling a gas flow from the jet engine
10/2007
10/24/2007EP1846649A1 Outlet device for a jet engine and a craft comprising such an outlet device
07/2007
07/25/2007EP1809893A1 Stator for a jet engine, a jet engine comprising such a stator, and an aircraft comprising the jet engine
07/25/2007EP1809892A1 An outlet device for a jet engine and a jet engine comprising such an outlet device
07/25/2007EP1809891A1 Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine
07/25/2007EP1809888A1 An outlet nozzle for a jet engine, an aircraft comprising the outlet nozzle and a method for controlling a gas flow from the jet engine
07/25/2007EP1809887A1 A device for controlling a gas flow, a jet engine comprising the device and an aircraft somprising the device
07/19/2007WO2005012714A3 Turbo rocket with real carnot cycle
06/2007
06/27/2007EP1799970A1 Gas turbine casing for enclosing a gas turbine component
10/2006
10/31/2006US7127880 Induction coupled variable nozzle
09/2006
09/21/2006WO2005026518A3 Induction coupled variable nozzle
07/2006
07/05/2006EP1676024A2 Induction coupled variable nozzle
06/2006
06/28/2006CN1795323A Rotary injector
05/2006
05/18/2006US20060104819 Low-noise fan exit guide vanes
05/11/2006WO2006049568A1 An outlet nozzle for a jet engine, an aircraft comprising the outlet nozzle and a method for controlling a gas flow from the jet engine
05/11/2006WO2006049556A1 A device for controlling a gas flow, a jet engine comprising the device and an aircraft somprising the device
05/11/2006WO2006049555A1 Propulsion system, aircraft comprising the propulsion system and an outlet device for a jet engine
05/11/2006WO2006049553A1 An outlet device for a jet engine and a jet engine comprising such an outlet device
05/11/2006WO2006049552A1 Outlet device for a jet engine and a craft comprising such an outlet device
05/11/2006WO2006049551A1 Stator for a jet engine, a jet engine comprising such a stator, and an aircraft comprising the jet engine
04/2006
04/13/2006WO2006038859A1 Gas turbine casing for enclosing a gas turbine component
04/13/2006CA2582691A1 Gas turbine casing for enclosing a gas turbine component
04/06/2006WO2005057001A3 Low-noise fan exit guide vanes
03/2006
03/15/2006EP1635054A2 Solid-propellant engine casing, and solid-propellant engine featuring such a casing
02/2006
02/22/2006EP1627145A2 Turbo rocket with real carnot cycle
02/22/2006EP1627139A2 Rotary injector
02/01/2006EP1620643A2 Self-aligning thrust reverser system lock assembly
11/2005
11/17/2005WO2005035963A3 Method and apparatus using jets to initiate detonations
11/15/2005US6964171 Method and apparatus using jets to initiate detonations
10/2005
10/12/2005EP1583899A2 Controlled autoignition propellant systems
09/2005
09/21/2005EP1576334A2 Multi-nozzle grid missile propulsion system
08/2005
08/09/2005US6925812 Rotary injector
06/2005
06/30/2005US20050138914 Turbo rocket with real carnot cycle
06/23/2005WO2005057001A2 Low-noise fan exit guide vanes
05/2005
05/26/2005WO2004099602A3 Self-aligning thrust reverser system lock assembly
05/12/2005WO2005028843A3 Rotary injector
04/2005
04/28/2005US20050086927 Induction coupled variable nozzle
04/21/2005WO2005035963A2 Method and apparatus using jets to initiate detonations
03/2005
03/31/2005WO2005028843A2 Rotary injector
03/31/2005WO2005028842A2 Controlled autoignition propellant systems
03/31/2005CA2526029A1 Rotary injector
03/24/2005WO2005026518A2 Induction coupled variable nozzle
03/17/2005US20050058957 Method and apparatus using jets to initiate detonations
02/2005
02/24/2005US20050039463 Rotary injector
02/10/2005WO2005012714A2 Turbo rocket with real carnot cycle
02/10/2005WO2004099601A3 Multi-nozzle grid missile propulsion system
02/10/2005CA2526591A1 Turbo rocket with real carnot cycle
01/2005
01/06/2005US20050001095 Self-aligning thrust reverser system lock assembly
11/2004
11/18/2004WO2004099602A2 Self-aligning thrust reverser system lock assembly
11/18/2004WO2004099601A2 Multi-nozzle grid missile propulsion system
04/2003
04/23/2003EP0932755B1 An axisymmetric vectoring nozzle actuating system having multiple power control circuits
08/1999
08/04/1999EP0932755A1 An axisymmetric vectoring nozzle actuating system having multiple power control circuits
04/1998
04/23/1998WO1998016732A1 An axisymmetric vectoring nozzle actuating system having multiple power control circuits
04/21/1998US5740988 Axisymmetric vectoring nozzle actuating system having multiple power control circuits
06/1982
06/29/1982CA1126519A1 Method and apparatus for reducing nitrous oxide emissions from combustors
03/1981
03/24/1981CA1097983A1 Steering arrangement for projectiles of the missile kind, and projectiles fitted with this arrangement
10/1980
10/07/1980US4226083 Method and apparatus for reducing nitrous oxide emissions from combustors
09/1980
09/16/1980US4222232 Method and apparatus for reducing nitrous oxide emissions from combustors
07/1980
07/08/1980US4211378 Steering arrangement for projectiles of the missile kind, and projectiles fitted with this arrangement