Patents
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)
07/2013
07/04/2013US20130167542 Flowsleeve of a turbomachine component
07/04/2013US20130167541 Air-Fuel Premixer for Gas Turbine Combustor with Variable Swirler
07/04/2013US20130167540 Combustor of a turbomachine
07/04/2013US20130167538 Apparatus for mixing fuel and air in a combustion system
07/04/2013US20130167374 Process of producing ceramic matrix composites and ceramic matrix composites formed thereby
07/04/2013DE102012113167A1 Verfahren und Vorrichtung zum Gewinnen diskreter Axialspieldaten unter Verwendung von Radialspielsensoren Method and apparatus for obtaining discrete Axialspieldaten using radial clearance sensors
07/04/2013CA2853399A1 Turbine engine comprising an electrically activated fuel supply pump, and turbine engine fuel supply method
07/04/2013CA2825849A1 Hot gas expander inlet casing assembly and method
07/03/2013EP2611026A1 Generator excitation during load fault conditions
07/03/2013EP2610465A1 Solar gas turbine system
07/03/2013EP2610460A2 Gas turbine engine compressor arrangement
07/03/2013EP2610441A2 Compact high-pressure exhaust muffling devices
07/03/2013EP2610440A2 Mounting device and method of assembling the same
07/03/2013EP2610360A1 Co-based alloy
07/03/2013EP2609313A1 Method for optimizing the control of a free turbine power package for an aircraft, and control for implementing same
07/03/2013EP2609312A2 Integral plus proportional dual pump switching system
07/03/2013EP2609296A2 Method for mounting shielding on a turbine casing, and mounting assembly for implementing same
07/03/2013EP2609012A2 Method for optimizing the overall energy efficiency of an aircraft, and main power package for implementing same
07/03/2013CN203035353U Ground air source starting device of aircraft engine
07/03/2013CN203035352U Two-stage compression large aircraft ground air source starting air feeding system
07/03/2013CN203035351U Thermal insulation structure
07/03/2013CN103189619A Gas turbine combustor with mounting for helmholtz resonators
07/03/2013CN103184936A Engine and aircraft
07/03/2013CN103184935A Hot-air anti-icer for engine inlet
07/03/2013CN103184934A Working fluid sensor system for power generation system
07/03/2013CN102140964B Structure for improving cooling efficiency of gas film of discrete hole
07/02/2013US8478625 Method for operating a gas storage power plant
07/02/2013US8475160 Low emissions combustion apparatus and method
07/02/2013US8474267 Radial turbine engine floating ring seal
07/02/2013US8474266 System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle
07/02/2013US8474265 Fuel nozzle for a turbine combustor, and methods of forming same
07/02/2013US8474241 Engine with intake air temperature control system
07/02/2013US8474240 Regenerative gas generator
07/02/2013CA2766010C Passive cooling system for auxiliary power unit installation
07/02/2013CA2713479C Staged compressor water wash system
07/02/2013CA2684510C Diffuser with improved erosion resistance
07/02/2013CA2586891C Ventilating air intake arrangement with mobile closing device
07/02/2013CA2498259C Absorber made of elastomer material for support links or other link units
06/2013
06/30/2013CA2800464A1 Gas turbine engine with low stage count low pressure turbine
06/30/2013CA2800001A1 Gas turbine engine compressor arrangement
06/30/2013CA2799810A1 Connector assembly and method of fabricating the same
06/30/2013CA2799349A1 Mounting device and method of assembling the same
06/29/2013CA2800049A1 Seal for a variable area fan nozzle
06/27/2013WO2013095951A2 System and method for flame stabilization
06/27/2013WO2013095212A1 Gas turbine engine component
06/27/2013WO2013095209A1 Gas turbine engine component
06/27/2013WO2013095202A1 Method for manufacturing of a gas turbine engine component
06/27/2013WO2013094433A1 Gas turbine engine and method for starting same
06/27/2013WO2013094432A1 Gas turbine engine provided with heat exchanger, and method for starting gas turbine engine
06/27/2013WO2013094381A1 Method for operating lean-fuel suction gas turbine engine, and gas turbine electricity generation device
06/27/2013WO2013094379A1 Control method and control device for lean-fuel suction gas turbine
06/27/2013WO2013093023A1 Bearing system for a turbocompressor and turbocompressor having the bearing system
06/27/2013WO2013092684A1 A powerplant comprising a condensed water recovery device
06/27/2013WO2013092563A1 Vent for a gaseous fuel supply circuit of a gas turbine, and associated method
06/27/2013WO2013092279A1 Sound insulation device and engine provided therewith and provision method
06/27/2013US20130164488 Airfoils for wake desensitization and method for fabricating same
06/27/2013US20130164115 Bleed air and hot section component cooling air system and method
06/27/2013US20130161446 Hinging cradle for fan cowls supported by said cowls in closed position
06/27/2013US20130160466 Nickel Based Forged Alloy, Gas Turbine Member Using Said Alloy and Gas Turbine Using Said Member
06/27/2013US20130160465 Gas turbine engine systems
06/27/2013US20130160464 Anti-vibration mount
06/27/2013US20130160463 Raft assembly
06/27/2013US20130160462 Gas turbine engine part
06/27/2013US20130160461 Electronic unit mounting
06/27/2013US20130160460 Rigid raft
06/27/2013US20130160459 Accessory mounting for a gas turbine
06/27/2013US20130160458 Electrical raft assembly
06/27/2013US20130160457 System and method for improved combustor temperature uniformity
06/27/2013US20130160456 System and method for controlling oxygen emissions from a gas turbine
06/27/2013US20130160455 System and method of expanding a fluid in a hermetically-sealed casing
06/27/2013US20130160454 Gas turbine engine with supersonic compressor
06/27/2013US20130160452 Aerodynamic shroud for the back of a combustion chamber of a turbomachine
06/27/2013US20130160424 Method for Operating a Combined Cycle Power Plant
06/27/2013DE102012223015A1 Turbolader mit verstellbarem Kern Turbocharger with adjustable core
06/27/2013DE102011056826A1 Schallschutzvorrichtung und damit versehenes Triebwerk und Verfahren zur Bereitstellung The sound insulation device and thus provided the engine and method for providing
06/26/2013EP2607669A1 System for supplying fuel to gas turbine combustor and method for supplying fuel to gas turbine combustor
06/26/2013EP2607667A2 Electrical Raft with Map
06/26/2013EP2607666A2 Rigid raft
06/26/2013EP2607665A2 Gas Turbine Engine Part
06/26/2013EP2607664A2 Electrical wiring assembly for gas turbine engines
06/26/2013EP2607663A2 Raft Assembly
06/26/2013EP2607662A2 Electrical Connectors
06/26/2013EP2607661A2 Electrical Connectors
06/26/2013EP2607660A2 Electrical Harness
06/26/2013EP2607659A2 Method of Servicing a Gas Turbine Engine
06/26/2013EP2607658A2 Accessory mounting for a gas turbine
06/26/2013EP2607657A2 Active flow control intake for a gas turbine engine
06/26/2013EP2607656A2 Gas turbine engine particle separator
06/26/2013EP2607655A2 Intake liner for a gas turbine engine
06/26/2013EP2607654A2 Anti-vibration mount for gas turbine wiring assembly
06/26/2013EP2607653A2 Electrical assembly with ground plane for gas turbine engines
06/26/2013EP2607652A2 Gas turbine engine subsystems
06/26/2013EP2607651A2 Electronic unit mounting
06/26/2013CN103175218A System and method for improved combustor temperature uniformity
06/26/2013CN103174522A Power plant comprising condensed water recovery device
06/26/2013CN103174521A 燃气涡轮发动机微粒分离器 The gas turbine engine particulate separator
06/26/2013CN103174520A Subsonic outflowing high external pressure internal waverider type air inlet and designing method thereof
06/26/2013CN102330605B Heavy combustion engine assembling method for assembling rotor and front and rear supports in combining manner
06/25/2013US8469309 Monolithic structure for mounting aircraft engine
06/25/2013US8468997 Internal combustion engine with variable effective length connecting rod
1 ... 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 ... 309