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)
10/2009
10/28/2009	CN101566104A Method and device for zero emission of carbon dioxide by utilizing liquid hydrogen condensation
10/28/2009	CN101566102A Power generator of rotary-catalytic regenerative-type gas turbine
10/28/2009	CN101566101A Power generation method of rotary-catalytic regenerative-type low-calorific-value gas turbine
10/28/2009	CN100554664C Two-spool turbomachine, driving module for the turbomachine and turbomachine assembly method
10/28/2009	CN100554647C Method and apparatus for reducing flow across compressor airfoil tips
10/28/2009	CN100554086C Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine
10/27/2009	CA2342670C Method for removing carbon dioxide from the exhaust gas from a gas turbine plant, and device for carrying out the method
10/22/2009	WO2009101267A3 Monitoring of a high‑pressure pump in a turbine engine fuel supply circuit
10/22/2009	US20090260660 Method and apparatus for cleaning a turbofan gas turbine engine
10/22/2009	US20090260368 Method for operating a gas turbine
10/22/2009	US20090260367 Multi-Compressor String With Multiple Variable Speed Fluid Drives
10/22/2009	US20090260344 Rear fan case for a gas turbine engine
10/22/2009	US20090260342 Gas turbine
10/22/2009	US20090260341 Distributed zoning for engine inlet ice protection
10/22/2009	DE19882241B4 Gas- und Dampfturbinen-Kraftwerk zum Erzeugen elektrischer Energie Gas and steam turbine power plant for generating electrical energy
10/22/2009	DE102008031274B3 Impulse-loaded characteristic diagram determining method for exhaust-gas turbo-charger of motor vehicle, involves predetermining operating point of turbo-charger to be examined, and positioning operating point on test bed device
10/22/2009	DE102008019891A1 Erosionsschutzbeschichtung Erosion protection coating
10/22/2009	DE102008019890A1 Dichtungsanordnung Seal assembly
10/22/2009	DE102008019331A1 Inlet seal for compressor of gas-turbine engine, has open-porous metallic sponge with filling material made of heat resistant duroplastic synthetic resin infiltrated in open-porous cavities of metallic sponge
10/22/2009	DE102008018863A1 Vorrichtung zur Luftversorgung Apparatus for supplying air to
10/22/2009	DE102004050182B4 Verfahren zur Luftkonditionierung A method of air conditioning
10/21/2009	EP2110518A1 Method for cleaning a high-temperature component and a device therefore
10/21/2009	EP2110516A2 Gas turbine engine rotor lock prevention system and corresponding method
10/21/2009	EP2110449A1 Heat resistant member
10/21/2009	EP2110314A2 De-icing system for engine inlet and method of preventing ice formation
10/21/2009	EP1373593B1 Method and device for gas phase diffusion coating of metal components
10/21/2009	CN100552300C Concentric fixed dilution and variable bypass air injection for a combustor
10/21/2009	CN100552200C Rotary injector
10/20/2009	US7603862 Combustion device
10/20/2009	US7603839 Scavenge pump system and method
10/20/2009	CA2464563C Rabbet mounted combustor
10/18/2009	CA2662500A1 Gas turbine engine rotor lock prevention system and method
10/15/2009	WO2009126847A1 Gas turbine engine cooling system and method
10/15/2009	WO2009125120A2 Device and method for balancing pressure in a turbojet bearing housing
10/15/2009	US20090256003 Method of manufacturing a fuel distributor
10/15/2009	US20090255652 Heat exchange device and method
10/15/2009	US20090255589 Turbine engine for aircraft
10/15/2009	US20090255271 Structural nacelle
10/15/2009	US20090255267 Comubstor seal having multiple cooling fluid pathways
10/15/2009	US20090255266 Surface treatments for preventing hydrocarbon thermal degradation deposits on articles
10/15/2009	US20090255264 Fuel nozzle
10/15/2009	US20090255263 Gas-turbine burner for a gas turbine with purging mechanism for a fuel nozzle
10/15/2009	US20090255261 Method of manufacturing a unitary venturi
10/15/2009	US20090255258 Pre-filming air-blast fuel injector having a reduced hydraulic spray angle
10/15/2009	US20090255256 Method of manufacturing combustor components
10/15/2009	US20090255242 Low Pressure Drop Mixer for Radial Mixing of Internal Combustion Engine Exhaust Flows, Combustor Incorporating Same, and Methods of Mixing
10/15/2009	DE102009003769A1 Oberflächenbehandlungen zum Verhindern von Abscheidungen aus thermischen Kohlenwasserstoff-Abbauprodukten auf Gegenständen Surface treatments to prevent deposits from thermal hydrocarbon degradation products on objects
10/15/2009	DE102009003761A1 Kühlvorrichtung für Brennkammerübergangsstück Cooling device for combustion transition piece
10/15/2009	DE102008018101A1 Strahltriebwerk mit mindestens einem Notantrieb Jet engine with at least one emergency drive
10/15/2009	DE102008014684A1 Turbolader mit einer Lageranordnung zur Lagerung einer Welle des Turboladers Turbocharger with a bearing assembly for supporting a shaft of the turbocharger
10/15/2009	CA2719472A1 Device and method for balancing pressure in a turbojet bearing housing
10/14/2009	EP2108799A1 Jet engine with at least one emergency drive
10/14/2009	EP2108078A2 A gas turbine
10/14/2009	EP2038534B1 Turbine engine for aircraft
10/14/2009	CN101558224A Device for improving the effectiveness of acoustic treatments in an aircraft drive duct
10/14/2009	CN101556045A Cooling apparatus for combustor transition piece
10/14/2009	CN101555834A Combustion engine island technique
10/14/2009	CN101555833A Transition piece impingement sleeve and method of assembly
10/14/2009	CN101554924A Device for feeding combustion air to an air craft engines
10/14/2009	CN100549530C Burner of gas turbine
10/14/2009	CN100549529C Method for converting wire wrap of outer and inner cowl into one-piece type cowl
10/14/2009	CN100549528C Gas turbine control apparatus, gas turbine system and gas turbine control method
10/14/2009	CN100549391C Gas calorie variation suppressing device, fuel gas supply facility, gas turbine facility, and boiler facility
10/14/2009	CN100549390C Internal combustion turbine exhaustion diffuser
10/13/2009	US7600972 Methods and apparatus for cooling gas turbine engine rotor assemblies
10/13/2009	US7600605 Aircraft ground run-up enclosure
10/13/2009	US7600382 Turbine engine with interstage heat transfer
10/13/2009	CA2558201C A three gear type gear pump of a fuel supply system
10/13/2009	CA2413635C Fuel injection device for a single combustion chamber gas turbine
10/08/2009	WO2009122474A1 Cooling structure for gas turbine combustor
10/08/2009	WO2009122066A2 Air intake lip for turbojet nacelle
10/08/2009	WO2009122057A1 Centrifugal oil separator having variable channel section
10/08/2009	WO2009121750A1 Aircraft power plant comprising engagable pumps and method of operation
10/08/2009	WO2009098402A3 Locking system for air intake structure for turbojet engine nacelle
10/08/2009	US20090252593 Cooling apparatus for combustor transition piece
10/08/2009	US20090249793 Apparatus for Modifying the Content of a Gaseous Fuel
10/08/2009	DE10331268B4 Anordnung für die thermische und/oder akustische Isolierung einer Anlage Arrangement for the thermal and / or acoustic insulation of a plant
10/08/2009	DE102009003701A1 Temperaturabsenkung am Einlass von Gasturbinen während Unterfrequenzereignissen und zugehöriges Verfahren Lowering the temperature at the inlet of gas turbines during underfrequency events and associated method
10/08/2009	CA2718318A1 Air intake lip for turbojet nacelle
10/08/2009	CA2715190A1 Centrifugal oil separator having variable channel section
10/07/2009	EP2107228A1 Aircraft power plant comprising engagable pumps and method of operation
10/07/2009	EP2107227A1 Operation of a gas turbine
10/07/2009	EP2107216A2 Method for determining the total pressure distribution across a fan entry plane
10/07/2009	EP2038532B1 Air intake for an aircraft turbine engine
10/07/2009	CN101550874A Gas turbine inlet temperature suppression during under frequency events and related method
10/07/2009	CN101550873A A kind of internal combustion engine using biofuel
10/07/2009	CN101550872A Re-heat combustor for a gas turbine engine
10/06/2009	US7597743 first metal (e.g., nickel) is plated onto graphite in the first section, and a second metal (e.g., iron) is plated onto graphite in the second section
10/06/2009	US7596953 Method for detecting compressor stall precursors
10/06/2009	US7596949 Method and apparatus for heat shielding gas turbine engines
10/06/2009	US7596947 Gas turbine plant
10/06/2009	US7596939 Gas turbine apparatus
10/01/2009	WO2009120778A2 Subsonic and stationary ramjet engines
10/01/2009	WO2009119345A1 Alloy material having high-temperature corrosion resistance, heat-shielding coating material, turbine member, and gas turbine
10/01/2009	WO2009119149A1 Combustor tail tube guide jig, method for removing combustor of gas turbine and method for fixing the same
10/01/2009	WO2009119133A1 Cover for cooling passage, method of manufacturing the cover, and gas turbine
10/01/2009	WO2009119127A1 Gas turbine, intermediate shaft for gas turbine, and method of cooling gas turbine compressor
10/01/2009	WO2009119126A1 Gas turbine
10/01/2009	WO2009118956A1 Gas turbine and method of forming insertion hole for combustor of gas turbine
10/01/2009	WO2009118298A1 Turbine engine including a reversible electric machine

1 ... 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 128 129 130 131 132 ... 309