Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
Patents for F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants (30,889)
10/2012
10/26/2012WO2012087420A3 Method for balancing rotating assembly of gas turbine engine
10/25/2012US20120271527 Distributed aircraft engine fuel system
10/25/2012US20120266606 Air turbine start system with monopole starter air valve position
10/25/2012US20120266604 Fuel nozzle and method for operating a combustor
10/25/2012US20120266603 Multi-layer ceramic composite porous structure
10/25/2012US20120266601 System and method for removing heat from a turbomachine
10/25/2012US20120266600 Fuel feed circuit for an aeroengine
10/24/2012EP2514949A2 Air turbine start system with monopole speed sensor
10/24/2012EP2514948A2 Distributed aircraft engine fuel system
10/24/2012EP2514947A1 Gas turbine engine including a nacelle assembly which comprises a cavity and a fan containment case
10/24/2012EP2514927A2 Independently-controlled gas turbine inlet guide vanes and variable stator vanes
10/24/2012EP2514926A1 Hybrid control system
10/24/2012EP2513561A2 Guiding of a spark plug into a turbine engine combustion chamber
10/24/2012EP2513487A2 Turbo compressor and compressor system comprising said turbo compressor
10/24/2012EP2513431A1 Arrangement and method for closed flow cooling of a gas turbine engine component
10/24/2012EP2513429A2 A gas turbine generator
10/24/2012EP2512927A2 Aircraft nacelle air intake incorporating optimized ice-treatment hot air injection means
10/24/2012EP2512619A1 Air intake for a plant
10/24/2012CN202500908U Transmission device and combustion gas turbine with same
10/24/2012CN202500659U 密封装置 Sealing device
10/24/2012CN202500658U Oil injection atomizing device for engine
10/24/2012CN202500616U Sealing device for tooth structure
10/24/2012CN102753807A Device for ejecting gas from a gas turbine engine and gas turbine engine
10/24/2012CN102753801A Link between the exhaust casing and a structural ring of the fan duct of a jet engine
10/24/2012CN102748136A Apparatus to seal with a turbine blade stage in a gas turbine
10/24/2012CN102748135A Method for designing fixed-geometry two-dimensional mixed-compression type supersonic velocity air inlet channel
10/24/2012CN101067381B Gas turbine has cooling air transfer system
10/23/2012US8292978 Radial air intake device with integrated bypass for an air inlet
10/23/2012US8291716 Hybrid propulsive engine including at least one independently rotatable turbine stator
10/23/2012US8291715 Bi-modal turbine assembly and starter / drive turbine system employing the same
10/23/2012US8291707 Multi-stage check valve
10/23/2012CA2504171C Fixed ring assembly for a gas turbine
10/23/2012CA2500942C Ceramic-based bushing for a variable setting system for turbine engine blades
10/23/2012CA2487800C Engine mounting structure under an aircraft wing
10/20/2012CA2769809A1 Distributed aircraft engine fuel system
10/18/2012WO2012140373A1 Fuel circuit comprising means for controlling a pump
10/18/2012WO2012094362A3 APPLYING OZONE NOx CONTROL TO AN HRSG FOR A FOSSIL FUEL TURBINE APPLICATION
10/18/2012US20120260670 Apparatus to seal with a turbine blade stage in a gas turbine
10/18/2012US20120260669 Front centerbody support for a gas turbine engine
10/18/2012US20120260667 Power Plant
10/18/2012US20120260665 Reheat combustor for a gas turbine engine
10/18/2012US20120260663 Fuel supply arrangement
10/18/2012US20120260662 Radiation shield for a gas turbine combustor
10/18/2012US20120260661 Compression ramp boundary layer removal
10/18/2012US20120260659 Interface between a combustor basket and a transition of a gas turbine engine
10/18/2012US20120260658 Fuel feed circuit for an aeroengine
10/18/2012US20120260622 Reheat burner injection system
10/18/2012DE102011007250A1 Turboladerkartusche mit gleitlager gestütztem Wälzlager Turbocharger cartridge with plain bearings aided
10/18/2012CA2832098A1 Fuel circuit comprising means for controlling a pump
10/17/2012EP2511612A1 Structure for connecting a combustor to a turbine unit, and gas turbine
10/17/2012EP2511500A2 Coupling shaft for gas turbine fan drive gear system
10/17/2012EP2511499A2 Fuel flow divider and ecology system for a gas turbine engine fuel flow control system
10/17/2012EP2511498A2 Fuel supply arrangement
10/17/2012EP2511484A2 Front centerbody support for a gas turbine engine
10/17/2012EP2510380A1 Monitoring system for an inner chamber of a machine
10/17/2012CN102741614A Combustor and gas turbine
10/17/2012CN102741524A Thermal energy storage apparatus for an adiabatic compressed air energy storage system and corresponding method of forming this system
10/17/2012CN102741506A Rotor blade for gas turbine, method for manufacturing same, and gas turbine using rotor blade
10/17/2012CN102733957A Gaseous flow separator with device for thermal-bridge defrosting
10/16/2012US8286654 Gas turbine engine inlet with noise reduction features
10/16/2012US8286434 Isentropic compression inlet for supersonic aircraft
10/16/2012US8286414 Pressure control method and system to reduce gas turbine fuel supply pressure requirements
10/16/2012CA2542707C Connector arrangement between an inner ring bearing and a joint, the ring and joint adapted to such an arrangement and the turbomachine equipped therewith
10/16/2012CA2459892C Redundant prime mover system
10/11/2012WO2012137898A1 Turbine vane
10/11/2012WO2012137844A1 Aircraft engine
10/11/2012WO2012137843A1 Generator apparatus for aircraft
10/11/2012WO2012136787A1 Gas turbine assembly and corresponding operating method
10/11/2012WO2012136493A1 Gas turbine comprising a heat shield and method of operation
10/11/2012WO2012136437A1 Process for cooling the turbine stage and gas turbine having a cooled turbine stage
10/11/2012US20120259502 System and method for use in evaluating an operation of a combustion machine
10/11/2012US20120255311 Cooling structure, gas turbine combustor and manufacturing method of cooling structure
10/11/2012US20120255310 Combustor nozzle and method for supplying fuel to a combustor
10/11/2012US20120255275 Guiding a sparkplug in a turbine engine combustion chamber
10/11/2012DE102011007059A1 Combustion chamber arrangement for partial load operation of gas turbine, has pipes whose walls are formed with apertures, where apertures are arranged such that air flow into chamber is adjusted by rotation of one pipe against another pipe
10/11/2012CA2832493A1 Gas turbine assembly and corresponding operating method
10/11/2012CA2832155A1 Aircraft engine
10/11/2012CA2832153A1 Generator device for aircraft
10/11/2012CA2831382A1 Turbine vane
10/10/2012EP2508734A2 Combustor with integrated control valve system
10/10/2012EP2508733A1 Gas turbine with a cooled turbine stage and method for cooling the turbine stage
10/10/2012EP2508721A2 Integrated gasification combined cycle system with vapor absorption chilling
10/10/2012EP2508713A1 Gas turbine comprising a heat shield and method of operation
10/10/2012EP2507493A1 Thermal energy storage apparatus for an adiabatic compressed air energy storage system and corresponding method of forming this system
10/10/2012EP2507481A2 Method for operating a steam turbine, steam turbine and atomizer
10/10/2012CN202483721U Back-flushing system of inlet filtering net of gas turbine
10/10/2012CN102725497A Micro-turbine combustor
10/10/2012CN102725130A Cylindrical structure and method for manufacturing the same
10/10/2012CN102720589A Plasma body igniter and gas turbine
10/10/2012CN102720588A Anti-ice device and anti-ice method of aero piston engine
10/10/2012CN102720587A Variable cross-section high supersonic speed inward rotation type air inlet with consistency of local contraction ratio
10/10/2012CN101675225B Gas turbine plant
10/09/2012US8281604 Divergent turbine nozzle
10/09/2012US8281603 Fastener assembly for connecting rocket engine nozzles
10/09/2012US8281602 Circumferentially self expanding combustor support for a turbine engine
10/09/2012US8281598 Gas-turbine combustion chamber with ceramic flame tube
10/09/2012US8281563 Gas-turbine bearing oil system with improved oil return arrangement
10/09/2012CA2512377C Turbojet with a guard plate to protect burner ring fuel rail, the burner ring and the guard plate
10/06/2012CA2773964A1 Flow device and method and system using the flow device
10/04/2012WO2012133630A1 Combustor for gas turbine engine and gas turbine
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