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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07/08/1997 | US5645397 For a gas turbine engine |
07/08/1997 | US5645127 Coolant supply arrangement for jet engine turbine walls |
07/03/1997 | WO1997023715A2 Process for operating a gas turbine and gas turbine operating in this way |
07/03/1997 | DE19549141A1 Method of operating gas turbine group with low-calorie fuel |
07/02/1997 | EP0781909A2 Gas turbine with water injection |
07/02/1997 | EP0781897A2 Method and device for the wet cleaning of the nozzle ring of a turbocharger |
07/02/1997 | EP0596062B1 Anti-icing system |
07/01/1997 | US5644394 System for repairing damaged gas turbine engine airfoils |
06/26/1997 | DE19548739A1 Process for fuel distribution in axially symmetric burner chamber |
06/25/1997 | EP0780639A2 Combustion chamber |
06/25/1997 | EP0780557A1 System to support the restart of a windmilling turbofan engine |
06/25/1997 | CN1152924A Proteins from mammaliam liver and their use in oncology |
06/24/1997 | US5640841 Plasma torch ignition for low NOx combustion turbine combustor with monitoring means and plasma generation control means |
06/24/1997 | US5640840 Recuperative steam cooled gas turbine method and apparatus |
06/21/1997 | CA2193167A1 System for engine restart following complete inflight engine shutdown |
06/19/1997 | WO1997021912A1 A power plant |
06/19/1997 | WO1997012125A3 Sealing element for sealing a gap and gas turbine facility |
06/19/1997 | DE19601507C1 Flame blow back tester for engine component groups |
06/19/1997 | DE19546726A1 Quench cooler for cooling hot flowing gas |
06/19/1997 | DE19546725A1 Cooler for hot flowing gas |
06/18/1997 | EP0779487A2 Quench cooler |
06/18/1997 | EP0779423A2 Quench cooler |
06/18/1997 | EP0778921A1 Pumping device |
06/12/1997 | WO1997021044A1 A coupling device |
06/12/1997 | WO1997021024A1 Reactive acoustic silencer |
06/11/1997 | EP0778443A1 Fuel injector arrangement; a method of operating a fuel injector arrangement |
06/11/1997 | EP0778407A2 Nozzle sealing apparatus |
06/11/1997 | EP0778396A2 Exhaust gas system for gas turbine |
06/11/1997 | CN1151474A Work method of power station equipment |
06/11/1997 | CN1151473A Method of operating gas-turbine group |
06/10/1997 | US5636659 Variable area compensation valve |
06/10/1997 | US5636511 For ignition of fuel in admixture with air within a gas combustor |
06/10/1997 | US5636507 Coordinated fuel-air controller for gas turbine without load feedback |
06/05/1997 | WO1997019869A1 Jet aircraft engine transport apparatus |
06/05/1997 | CA2164370A1 Reactive acoustic silencer |
06/04/1997 | EP0776529A1 Ultra-high efficiency turbine and fuel cell combination |
06/04/1997 | CN1150995A Liquefied natural gas gasification device for gas turbine compound circulating power plant |
06/03/1997 | US5634766 Turbine stator vane segments having combined air and steam cooling circuits |
06/03/1997 | US5634339 Non-polluting, open brayton cycle automotive power unit |
05/29/1997 | WO1997019257A1 Vane for gas turbine |
05/29/1997 | WO1997019256A1 Heat-recovery gas turbine rotor |
05/27/1997 | US5632148 Power augmentation of a gas turbine by inlet air chilling |
05/22/1997 | WO1997018396A1 Optimization of turbomachinery harmonics |
05/22/1997 | CA2237611A1 Optimization of turbomachinery harmonics |
05/21/1997 | EP0774572A1 Compact closed cycle gas turbine for the propulsion of a vehicle |
05/20/1997 | US5630702 Arrangement for influencing the radial clearance of the blading in axial-flow compressors including hollow spaces filled with insulating material |
05/18/1997 | CA2164648A1 Closed combined cycle with high-temperature exhaust gas |
05/17/1997 | CA2190524A1 Compact, solid brayton cycle motor; propulsion system using said motor; the vehicule using said propulsion system |
05/14/1997 | EP0773410A2 Fuel and air mixing tubes |
05/14/1997 | EP0773403A1 Power plant |
05/14/1997 | EP0773349A1 Cooling-air cooling unit for power plants |
05/14/1997 | EP0772756A1 Microcomponent sheet architecture |
05/13/1997 | US5628184 Apparatus for reducing the production of NOx in a gas turbine |
05/13/1997 | US5628179 Steam attemperation circuit for a combined cycle steam cooled gas turbine |
05/06/1997 | US5626019 Gas turbine intake air cooling apparatus |
05/06/1997 | US5626018 Gas turbine engine |
05/02/1997 | EP0770771A1 Compressor with intercooling |
05/02/1997 | EP0770770A1 Method of operating a gas turbo group |
05/02/1997 | EP0770093A1 Proteins from mammalian liver and their use in oncology |
05/01/1997 | WO1997009578A3 Method and apparatus for cooling the inlet air of gas turbine and internal combustion engine prime movers |
04/30/1997 | CN1148662A Running method of gas turbine generating set |
04/29/1997 | US5625664 Methods for the design, quality control, and management of fatigue-limited metal components |
04/29/1997 | US5624513 Filling component with uncured adhesive, curing, applying force to remove insert bonded to adhesive from airfoil |
04/29/1997 | US5624231 Cooled turbine blade for a gas turbine |
04/29/1997 | US5623821 Turbojet equipped with a deicing system on the intake case |
04/24/1997 | WO1997014881A1 Combustor cooling for gas turbine engines |
04/24/1997 | WO1997014875A1 Gas turbine regenerative cooled combustor |
04/24/1997 | WO1997014871A1 Variable area compensation valve |
04/24/1997 | WO1997014497A1 Microcomponent chemical process sheet architecture |
04/24/1997 | DE19634296A1 Aircraft fan jet propulsion unit |
04/24/1997 | CA2235377A1 Combustor cooling for gas turbine engines |
04/23/1997 | EP0769093A1 Turbine vane assembly with integrally cast cooling fluid nozzle |
04/22/1997 | US5622474 Blade tip seal insert |
04/22/1997 | US5622472 Protective shield for a turbo-engine |
04/22/1997 | US5622438 Fire resistant bearing compartment cover |
04/22/1997 | US5622044 Apparatus for augmenting power produced from gas turbines |
04/17/1997 | WO1997014032A1 Methods for the design, quality control, and management of fatigue-limited metal components |
04/17/1997 | WO1997013972A1 Combined pressurizing, flow measuring and flow splitting valve |
04/17/1997 | WO1997013552A1 Radiotherapy apparatus for treating a patient |
04/17/1997 | DE19544927A1 Gas turbine for driving generator or machinery |
04/17/1997 | DE19537636A1 Power generation method for power station |
04/16/1997 | EP0768449A1 Process for operating a power plant |
04/16/1997 | EP0768448A1 Cooled turbine vane assembly |
04/16/1997 | EP0767868A1 Pressure vessel fuel nozzle support for an industrial gas turbine engine |
04/15/1997 | US5620154 Three link failsafe engine mount |
04/10/1997 | WO1997013100A1 Improved method and apparatus for the destruction of volatile organic compounds |
04/09/1997 | EP0767345A2 Process for operating a power plant |
04/09/1997 | EP0603334B1 Temperature control of the air supply in pfbc plants |
04/08/1997 | US5618222 Method and a machine for working a blade sector |
04/08/1997 | US5617718 Gas-turbine group with temperature controlled fuel auto-ignition |
04/08/1997 | US5617717 Flame stabilization system for aircraft jet engine augmentor using plasma plume ignitors |
04/08/1997 | US5617716 Method for supplying vaporized fuel oil to a gas turbine combustor and system for same |
04/03/1997 | WO1997012165A1 Fluid line with integrated unpressurized return flow |
04/03/1997 | WO1997012134A1 Mounting for sound-absorbing members |
04/03/1997 | WO1997012125A2 Sealing element for sealing a gap and gas turbine facility |
04/03/1997 | DE19536181A1 Jet engine for hypersonic aircraft |
04/02/1997 | EP0765951A2 Abradable ceramic coating |
04/02/1997 | EP0765453A1 Pilot injector for gas turbine engines |
04/02/1997 | EP0714477B1 Control of position of supersonic inlet shock |
04/02/1997 | EP0623189B1 Coolable outer air seal assembly for a turbine |