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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08/18/1998 | US5794338 Method for repairing a turbine engine member damaged tip |
08/13/1998 | DE19729433C1 Support device for exhaust gas channel of gas turbine |
08/12/1998 | EP0797747B1 Bulkhead cooling fairing |
08/12/1998 | EP0757750B1 Brush seal support and vane assembly windage cover |
08/12/1998 | CN1190449A Liquefied natural gas (LNG) fueled combined cycle power plant and LNG fueled gas turbine plant |
08/11/1998 | US5792744 Proteins from mammalian liver |
08/11/1998 | US5791789 Rotor support for a turbine engine |
08/11/1998 | US5791148 Liner of a gas turbine engine combustor having trapped vortex cavity |
08/11/1998 | US5791138 Turbofan engine with reduced noise |
08/11/1998 | US5791137 Radial inflow dual fuel injector |
08/11/1998 | US5791136 Combined-cycle power generation plant, including a gas turbine, an annual exhaust gas channel having swirl suppression vanes, and a heat recovery boiler |
08/06/1998 | WO1998034068A1 Gas turbine installation with a ceramic-covered combustion chamber housing |
08/06/1998 | WO1998034013A1 Gas turbine cooling stationary vane |
08/06/1998 | DE19705215C1 Gas-turbine compressor set with heat recirculation |
08/05/1998 | EP0856651A2 Starting method for a turbine engine |
08/05/1998 | EP0856640A1 Sealing consisting of stacked strip sliding freely in a slot |
08/05/1998 | EP0856639A2 Nozzle ring for a radial turbine |
08/05/1998 | EP0856095A1 Variable area compensation valve |
08/04/1998 | US5790972 Method and apparatus for cooling the inlet air of gas turbine and internal combustion engine prime movers |
08/04/1998 | US5787703 Combined ramjet and rocket engine having rectilinear duct |
07/30/1998 | WO1998033012A1 Atomizing dual fuel nozzle for a combustion turbine |
07/30/1998 | WO1998032960A1 Combustion turbine with fuel heating system |
07/30/1998 | WO1998032954A1 Combined gas and steam turbine installation and method to operate the same |
07/30/1998 | WO1998032953A1 Gas turbine rotor for steam cooling |
07/30/1998 | DE19704976A1 Gasturbinenanlage mit einem mit Keramiksteinen ausgekleideten Brennkammergehäuse Gas turbine plant with a ceramic lined combustor casing stones |
07/30/1998 | CA2278481A1 Atomizing dual fuel nozzle for a combustion turbine |
07/30/1998 | CA2276696A1 Combustion turbine with fuel heating system |
07/29/1998 | EP0855022A1 Methods for the design, quality control, and management of fatigue-limited metal components |
07/29/1998 | EP0854976A1 Combined pressurizing, flow measuring and flow splitting valve |
07/28/1998 | US5785492 Method and apparatus for sealing a gas turbine stator vane assembly |
07/28/1998 | US5784877 Rocket-ramjet engine casing port closure |
07/28/1998 | US5784876 Combuster and operating method for gas-or liquid-fuelled turbine arrangement |
07/23/1998 | DE19716696C1 Gas-turbine air intake system design |
07/22/1998 | EP0854278A2 Recovery of heat from the combustion products of a gas turbine engine |
07/22/1998 | EP0854269A1 Control device for the flux of cooling air for high temperature combustion chamber |
07/22/1998 | CN1188210A Combusion chamber having integrated guide blades |
07/22/1998 | CN1188181A Method for tracing leaks in closed or hal-open cooling system of gas turbine |
07/22/1998 | CN1188179A Compressor-wheel arrangement for turbochargers |
07/21/1998 | US5783932 Power generation plant and control apparatus therefor |
07/21/1998 | US5782093 Gas turbine intake air cooling apparatus |
07/21/1998 | US5782082 Aircraft engine acoustic liner |
07/21/1998 | US5782080 Quench cooler for gas turbine system |
07/21/1998 | US5782077 Device for bleeding off and cooling hot air in an aircraft engine |
07/21/1998 | US5782076 Closed loop air cooling system for combustion turbines |
07/16/1998 | WO1998030793A1 Torch assembly |
07/16/1998 | WO1998030338A1 Modular coating fixture |
07/16/1998 | CA2277078A1 Torch assembly |
07/15/1998 | EP0852681A1 Fluid line with integrated unpressurized return flow |
07/15/1998 | EP0852665A1 Mounting for sound-absorbing members |
07/15/1998 | EP0852659A2 Sealing element for sealing a gap and gas turbine facility |
07/15/1998 | CN1187600A Method of disgorging flames from two stream tangential entry nozzle |
07/15/1998 | CN1187581A Two Stream tangential entry nozzle |
07/14/1998 | US5780729 For a test cell |
07/14/1998 | US5780171 Gas turbine engine component |
07/14/1998 | US5780116 Method for producing an abradable seal |
07/14/1998 | US5779442 Removable inner turbine shell with bucket tip clearance control |
07/14/1998 | US5779438 Arrangement for and method of cooling a wall surrounded on one side by hot gas |
07/14/1998 | US5779436 Turbine blade clearance control system |
07/14/1998 | US5778675 Method of power generation and load management with hybrid mode of operation of a combustion turbine derivative power plant |
07/14/1998 | US5778657 Combined cycle power plant |
07/09/1998 | WO1998029653A1 Power generation method and power generating apparatus |
07/09/1998 | WO1998029640A1 Cooling system for gas turbine vane |
07/09/1998 | CA2274519A1 Cooling system for gas turbine vane |
07/08/1998 | EP0852286A2 Bearing lubrication configuration in a turbine engine |
07/08/1998 | EP0852285A1 Turbulator configuration for cooling passages of rotor blade in a gas turbine engine |
07/08/1998 | EP0852284A1 Turbulator configuration for cooling passages of an airfoil in a gas turbine engine |
07/08/1998 | CN1186926A Flame disgorging two stream tangential entry nozzle |
07/07/1998 | US5775878 Turbine of thermostructural composite material, in particular of small diameter, and a method of manufacturing it |
07/07/1998 | US5775638 Mounting arrangement for a gas turbine engine |
07/07/1998 | US5775108 For a turbomachine |
07/07/1998 | US5775098 Bypass air valve for a gas turbine |
07/01/1998 | EP0851105A2 Turbocooler air assist fuel atomization in a gas turbine engine |
07/01/1998 | EP0851104A1 Gas turbine with heat recovery steam generator for cooling the combustion chamber, then injecting downstream of the combustion zone |
07/01/1998 | EP0851099A2 Gas turbine generator |
07/01/1998 | EP0851098A2 A method for improving the cooling effectiveness of film cooling holes |
07/01/1998 | EP0850831A2 Inlet nose cone assembly and method for repairing the assembly |
07/01/1998 | CN1186194A Method and apparatus for electric power generation |
07/01/1998 | CN1186150A Coolable blade |
06/30/1998 | US5772398 Cooled turbine guide vane |
06/30/1998 | US5772182 Fuel flow control valve |
06/30/1998 | US5771693 Gas compressor |
06/30/1998 | US5771577 Method for making a fluid cooled article with protective coating |
06/30/1998 | CA2225947A1 Low nox combustor having dual fuel injection system |
06/25/1998 | WO1998027330A1 Ramjet engine for power generation |
06/25/1998 | WO1998009868A3 Noise suppression system for a jet engine |
06/25/1998 | CA2274709A1 Ramjet engine for power generation |
06/24/1998 | EP0849533A2 Burner arrangement for a gas turbine |
06/24/1998 | EP0849531A2 Method of combustion with low acoustics |
06/24/1998 | EP0849527A2 Method of combustion with a two stream tangential entry nozzle |
06/24/1998 | EP0849451A2 Method to stabilize combustion in a gas turbine power station |
06/24/1998 | EP0763164B1 Turbofan containment structure |
06/24/1998 | EP0763163B1 Aircraft fan containment structure |
06/24/1998 | EP0760052B1 Variable thickness isogrid case |
06/24/1998 | EP0758932B1 Cooled gas turbine blade |
06/24/1998 | EP0757752B1 Aircraft fan containment structure restraint |
06/24/1998 | EP0756667B1 Gas turbine airfoil clocking |
06/24/1998 | CN1185565A Burner for gas turbine |
06/23/1998 | US5768893 Turbine with internal heating passages |
06/23/1998 | US5768884 Gas turbine engine having flat rated horsepower |
06/23/1998 | US5768778 One-piece engine inlet acoustic barrel |