| 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) |
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| 09/25/2013 | CN103321749A Isothermal compression type heat engine |
| 09/25/2013 | CN103321748A Vertical combustion gas turbine |
| 09/25/2013 | CN102953825B Pneumatic supersonic velocity/hypersonic velocity adjustable air inlet passage for self-circulation of forebody |
| 09/25/2013 | CN102505990B Power generation method of condensing double-working medium gas turbine circulation system |
| 09/25/2013 | CN102282276B Ni-based single crystal superalloy |
| 09/25/2013 | CN102272427B 发动机 Engine |
| 09/24/2013 | US8540492 Intake cone in a fiber compound material for a gas-turbine engine |
| 09/24/2013 | US8539749 Systems and apparatus relating to reheat combustion turbine engines with exhaust gas recirculation |
| 09/24/2013 | CA2714871C Method and apparatus for production of a cast component |
| 09/24/2013 | CA2692745C Compressor wash nozzle integrated in an inlet case strut |
| 09/24/2013 | CA2675400C Gas turbine engine fan bleed heat exchanger system |
| 09/24/2013 | CA2603410C Fuel conveying member with heat pipe |
| 09/23/2013 | CA2810028A1 Combustor heat shield |
| 09/23/2013 | CA2809801A1 Fabricated heat shield |
| 09/23/2013 | CA2809420A1 Seal arrangements for gas turbine engines |
| 09/19/2013 | WO2013138217A1 Constant-speed pump system for engine thermal management system aoc reduction and environmental control system loss elimination |
| 09/19/2013 | WO2013138215A1 Pump system for tms aoc reduction |
| 09/19/2013 | WO2013138212A1 Gas turbine engine variable stator vane assembly |
| 09/19/2013 | WO2013138129A1 Gas turbine engine airfoil cooling circuit |
| 09/19/2013 | WO2013138050A1 Fuel air premixer for gas turbine engine |
| 09/19/2013 | WO2013138040A1 Compressor inlet manifold for a gas turbine engine |
| 09/19/2013 | WO2013138023A1 Turbomachine rotor balancing system |
| 09/19/2013 | WO2013138009A1 Improved cooling pedestal array |
| 09/19/2013 | WO2013137723A1 Screen panel for covering at least partly an air intake opening of an air inlet house of a combustion engine or a compressor |
| 09/19/2013 | US20130243589 Turbojet engine nacelle reinforcing structure |
| 09/19/2013 | US20130240002 System for washing an aero gas turbine engine |
| 09/19/2013 | US20130239588 Pump system for tms aoc reduction |
| 09/19/2013 | US20130239587 Gas turbine engine compressor arrangement |
| 09/19/2013 | US20130239585 Tangential flow duct with full annular exit component |
| 09/19/2013 | US20130239584 Constant-speed pump system for engine thermal management system aoc reduction and environmental control system loss elimination |
| 09/19/2013 | US20130239581 Systems and Methods for Preventing Flashback in a Combustor Assembly |
| 09/19/2013 | US20130239580 High altitude start of a gas turbine engine using fuel pulsing and starter toggling |
| 09/19/2013 | US20130239578 Internal thermal management for motor driven machinery |
| 09/19/2013 | US20130239542 Structures and methods for intercooling aircraft gas turbine engines |
| 09/19/2013 | US20130239541 Turbine nozzle segment and corresponding gas turbine engine |
| 09/19/2013 | DE112011104492T5 Verfahren zum Auswuchten einer rotierenden Anordnung eines Gasturbinenmotors Method for balancing a rotating assembly of a gas turbine engine |
| 09/19/2013 | DE10352252B4 Kompressor für eine Turbogruppe Compressor for a turbo set |
| 09/19/2013 | DE102012204162A1 Ringbrennkammer-Bypass Annular combustor bypass |
| 09/19/2013 | DE102012204078A1 Druckluftspeicher-Turbinen-Kraftwerk sowie Verfahren zum Trocknen von feuchter Druckluft bei einem Druckluftspeicher-Turbinen-Kraftwerk Compressed air energy storage power plant turbine, as well as method for drying of moist compressed air in a compressed air energy storage power plant turbine |
| 09/18/2013 | EP2639509A2 Combustor and method of reducing thermal stresses in a combustor |
| 09/18/2013 | EP2639429A1 Aircraft engine |
| 09/18/2013 | EP2639428A2 Pre-filter or coalescer |
| 09/18/2013 | CN203201665U Air inlet temperature adjusting device of combustion gas turbine |
| 09/18/2013 | CN103314206A Nacelle for an aircraft bypass turbojet engine |
| 09/18/2013 | CN103306821A Apparatus for extracting input power from the low pressure spool of a turbine engine |
| 09/18/2013 | CN103306820A Supersonic air feeding channel and three-dimensional determining method for wall surface of supersonic air feeding channel |
| 09/18/2013 | CN103306819A Aerospace adjustable air inlet device |
| 09/18/2013 | CN103306818A Gas turbine frame stiffening rails |
| 09/18/2013 | CN102297025B Micro gas turbine generator employing mixed oxygen-enriched combustion |
| 09/18/2013 | CN102297024B Miniature pure oxygen combustion gas turbine generator |
| 09/18/2013 | CN102287266B Micro fully-wind-driven oxygen enriched combustion type gas turbine generator |
| 09/18/2013 | CN101945808B Aircraft engine assembly comprising downwardly offset engine mounts on the fan casing |
| 09/17/2013 | US8538657 Systems and methods for controlling fuel flow to a turbine component |
| 09/17/2013 | US8534077 Turbine engine with a power turbine equipped with an electric power generator |
| 09/17/2013 | US8534076 Combustor-turbine seal interface for gas turbine engine |
| 09/17/2013 | US8534041 Apparatus and assembly for a spark igniter having tangential embedded pins |
| 09/17/2013 | US8534040 Apparatus and method for igniting a combustor |
| 09/17/2013 | CA2610787C System for deicing the leading edge of a nose inlet cowl for a turbine engine |
| 09/17/2013 | CA2604636C Internal fuel manifold with airblast nozzles |
| 09/17/2013 | CA2509863C Double impingement vane platform cooling |
| 09/13/2013 | CA2805836A1 High altitude start of a gas turbine engine using fuel pulsing and starter toggling |
| 09/12/2013 | WO2013134020A1 Gas turbine engine configured to shape power output |
| 09/12/2013 | WO2013133997A1 Erosion resistant and hydrophobic article |
| 09/12/2013 | WO2013133945A1 Airfoil with improved internal cooling channel pedestals |
| 09/12/2013 | WO2013133935A1 Gas turbine engine fuel heating system |
| 09/12/2013 | WO2013132936A1 Shaft seal device |
| 09/12/2013 | WO2013132692A1 Sealing device and gas turbine provided with sealing device |
| 09/12/2013 | WO2013132433A1 Preparation of exhaust gas from a gas turbine for exhaust gas recirculation |
| 09/12/2013 | WO2013131970A1 Gas turbine with primary and secondary lubricating oil cooler |
| 09/12/2013 | WO2013131968A1 Device and method for gas turbine unlocking after shut down |
| 09/12/2013 | US20130238215 Monitoring of a filter of the fuel-supply system of an aircraft engine |
| 09/12/2013 | US20130236315 Compressor/turbine rotor-torque transmission through hybrid drive |
| 09/12/2013 | US20130236301 Apparatus And System For Directing Hot Gas |
| 09/12/2013 | US20130236289 Turbine interstage seal system |
| 09/12/2013 | US20130234396 Transition Piece Aft-Frame Seals |
| 09/12/2013 | US20130232991 Airfoil with improved internal cooling channel pedestals |
| 09/12/2013 | US20130232989 Gas turbine engine fuel heating system |
| 09/12/2013 | US20130232986 Combustor and method for reducing thermal stresses in a combustor |
| 09/12/2013 | US20130232979 System for enhancing mixing in a multi-tube fuel nozzle |
| 09/12/2013 | US20130232977 Fuel nozzle and a combustor for a gas turbine |
| 09/12/2013 | US20130232976 Gas turbine fuel flow measurement using inert gas |
| 09/12/2013 | US20130232939 Gradual oxidation with adiabatic temperature above flameout temperature |
| 09/12/2013 | DE102013203777A1 Kanalsystemeinrichtung Channel system setup |
| 09/11/2013 | EP2636982A2 Tubular heat exchange systems |
| 09/11/2013 | EP2636873A2 Apparatus for extracting input power from the low pressure spool of a turbine engine |
| 09/11/2013 | EP2636872A2 Turbomachine drive arrangement |
| 09/11/2013 | EP2636871A2 Methods and systems for inlet airflow measurement using inert gas |
| 09/11/2013 | EP2636870A1 Preparation of exhaust gas from a gas turbine for exhaust gas recirculation |
| 09/11/2013 | EP2636592A2 Sandwich structure with shear stiffness between skins and compliance in the thickness direction |
| 09/11/2013 | CN103299084A Turbofan engine |
| 09/11/2013 | CN103299048A 燃气轮机 Gas turbine |
| 09/11/2013 | CN103299047A Method for starting a turbomachine |
| 09/11/2013 | CN103291507A Fuel enrichment engine utilizing exhaust heat |
| 09/11/2013 | CN103291462A Oil drainage method of split type fuel pump |
| 09/11/2013 | CN103291461A Engine inlet fuel temperature regulating system |
| 09/11/2013 | CN103291460A Fuel purging system for a turbine assembly |
| 09/11/2013 | CN103291459A Gas film hole used for cooling gas turbine engine |
| 09/11/2013 | CN103291458A Counter-rotating low pressure turbine with gear system mounted to mid turbine frame |
| 09/11/2013 | CN103291457A Transition piece aft frame assembly having a heat shield |
| 09/11/2013 | CN103291456A Electrical harness |