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)
12/1999
12/02/1999DE19824421A1 Gehäuseausbildung an einer Gasturbine Housing education at a gas turbine
12/02/1999DE19815914A1 Distributor for supply of gas, air and coolant to gas turbine burners
12/02/1999CA2332819A1 Recuperator for gas turbine engine
12/01/1999EP0961017A2 High temperature resistant coating
12/01/1999EP0960308A1 Gas turbine installation with a ceramic-covered combustion chamber housing
12/01/1999EP0783651B1 Tangential air entry fuel nozzle
12/01/1999EP0769093B1 Turbine vane assembly with integrally cast cooling fluid nozzle
11/1999
11/30/1999US5993980 Protective coating for protecting a component from corrosion, oxidation and excessive thermal stress, process for producing the coating and gas turbine component
11/30/1999US5993149 Variable area compensation valve
11/30/1999US5992139 Turbine engine with turbocompressor for supplying atomizing fluid to turbine engine fuel system
11/24/1999EP0959298A2 Premixing fuel injector and method of operation
11/24/1999EP0959235A2 Gas turbine power plant
11/24/1999EP0959230A2 Shroud cooling assembly for gas turbine engine
11/24/1999EP0958452A1 Ramjet engine for power generation
11/23/1999US5988890 Rotor shaft
11/23/1999US5987879 Spring seal device for combustor
11/23/1999US5987878 Fuel reforming apparatus and electric power generating system having the same
11/23/1999US5987877 Turboprop engine with an air-oil cooler
11/23/1999CA2159040C Ammonia absorption refrigeration cycle for combined cycle power plant
11/23/1999CA2127772C Indirect contact chiller air-precooler method and apparatus
11/18/1999WO1999058233A1 Liquid spray nozzle and use of same
11/18/1999DE19821365A1 Kühlung einer Wabendichtung im mit Heißgas beaufschlagten Teil einer Gasturbine Cooling of a honeycomb seal loaded with hot gas part of a gas turbine
11/18/1999CA2272112A1 Premixing fuel injector and method of operation
11/18/1999CA2269348A1 Turbogenerator/motor control system
11/17/1999EP0957237A2 Cooling of a honeycomb seal in a gas turbine
11/17/1999EP0865570A4 Noise suppression system for a jet engine
11/16/1999US5984637 Cooling medium path structure for gas turbine blade
11/16/1999US5984636 Cooling arrangement for turbine rotor
11/16/1999US5984630 Reduced windage high pressure turbine forward outer seal
11/16/1999US5983642 Combustor with two stage primary fuel tube with concentric members and flow regulating
11/16/1999US5983623 System for cooling gas turbine blades
11/16/1999US5983621 Method for controlling the flow rate of fuel within a gas turbine
11/11/1999WO1999057421A1 Gas and steam turbine installation
11/11/1999DE19819769A1 Gasturbinenanlage Gas turbine plant
11/10/1999EP0955457A2 Gas turbine fuel system
11/10/1999EP0955456A2 Air inlet conduit for a gas turbine
11/10/1999EP0955455A1 Power generation method and power generating apparatus
11/10/1999EP0954719A1 Atomizing dual fuel nozzle for a combustion turbine
11/10/1999EP0954688A1 Torch assembly
11/10/1999EP0954687A1 Combustion turbine with fuel heating system
11/09/1999US5979593 Hybrid mode-scattering/sound-absorbing segmented liner system and method
11/09/1999US5979156 Cooling steam system for steam cooled gas turbine
11/04/1999WO1999056005A1 Cooling scheme for turbine hot parts
11/04/1999WO1999033701A9 Self-adjusting air intake
11/04/1999DE19819267A1 Radial compressor with radially external vaned impeller
11/04/1999DE19817705A1 Kühlluftentnahme auf der Saugseite einer Diffusorschaufel einer radialen Kompressorstufe von Gasturbinen Cooling air extraction on the suction side of a diffuser vane radial compressor stage of gas turbines
11/03/1999EP0953749A2 Pressure compensated fuel delivery system for the combustors of gas turbines
11/03/1999EP0953728A1 Booster compressor with tandem blading
11/03/1999EP0839262B1 Gas turbine engine case coated with thermal barrier coating to control axial airfoil clearance
11/03/1999EP0784845A4 Active control of aircraft engine inlet noise using compact sound sources and distributed error sensors
11/03/1999EP0619856B1 Aluminide-silicide coatings, coating compositions, process for coating and improved coated products
11/02/1999US5976332 This invention relates to gas or steam turbines, and specifically to high performance power systems employing such devices.
11/02/1999US5975844 Sealing element for sealing a gap and gas turbine plant
11/02/1999US5975237 Reinforcing structure for engine nacelle acoustic panel
11/02/1999US5974782 Method for enabling operation of an aircraft turbo-engine with rotor unbalance
11/02/1999US5974780 Method for reducing the production of NOX in a gas turbine
10/1999
10/28/1999WO1999054610A1 Anti-coking fuel injector purging device
10/28/1999WO1999054609A1 Turbine engine with cooled p3 air to impeller rear cavity
10/28/1999WO1999054598A1 Containment system for containing blade burst
10/28/1999DE19918900A1 High temperature component, especially metallic gas turbine component
10/27/1999EP0952317A2 Purging system for a gas turbine fuel supply
10/27/1999EP0952316A2 Gas turbine inlet air cooling method for combined cycle power plants
10/27/1999EP0952310A2 Penetration resistant fan casing for a turbine engine
10/27/1999EP0951614A1 Cooling system for gas turbine vane
10/26/1999US5971710 Turbomachinery blade or vane with a permanent machining datum
10/26/1999US5971400 Seal assembly and rotary machine containing such seal assembly
10/26/1999US5971000 Internal compression supersonic engine inlet
10/26/1999US5970715 Fuel/air mixing device for jet engines
10/20/1999EP0950859A1 Separator for combustion chamber with two burner heads
10/20/1999EP0950811A2 Starting device for model turbine engine
10/20/1999EP0950808A2 Turbofan engine including fans with reduced speed
10/20/1999CN1232524A Gas turbine airfoil cooling system and method
10/19/1999US5967746 Gas turbine interstage portion seal device
10/19/1999US5967745 Gas turbine shroud and platform seal system
10/19/1999US5967169 Air intake for engines
10/19/1999US5966926 Liquid fuel injector purge system
10/19/1999US5966925 Gas turbine power plant control for starting and stopping
10/14/1999DE19815473A1 Heißgasführendes Gassammelrohr einer Gasturbine Hot Gas-conducting gas collecting tube of a gas turbine
10/14/1999DE19814627A1 Kühlluftentnahme auf der Gehäuseseite eines Diffusors einer Kompressorstufe von Gasturbinen Cooling air tapping on the housing side of a diffuser of a compressor stage of gas turbine
10/13/1999EP0949454A2 Liquid fuel and water injection purge systems for a gas turbine
10/13/1999EP0949410A2 Coated transition duct for a gas turbine
10/13/1999CN1231384A Discharge header for guiding hot gas in gas turbine
10/12/1999US5966525 Acoustically improved gas turbine blade array
10/12/1999US5966452 Sound reduction method and system for jet engines
10/12/1999US5965048 Heated chamber including an open wall with a gas curtain
10/12/1999US5964574 Exhaust-gas turbine of a turbocharger
10/12/1999CA2012176C Infrared suppressor for a gas turbine engine
10/07/1999WO1999050943A1 Protective sheath
10/07/1999WO1999050534A1 Deflector for controlling entry of cooling air leakage into the gaspath of a gas turbine engine
10/07/1999WO1999032768A9 Microturbine power generating system including auxiliary compressor
10/07/1999DE19814588A1 Thermal protection layer for an oxidic fiber composite material used especially as a gas turbine combustion chamber coating
10/06/1999EP0947707A2 Cooling air withdrawal from the outside of a diffuser of a gas turbine compressor stage
10/06/1999EP0947044A2 Electrical system for turbine/alternator on common shaft
10/06/1999CN1230977A Dimethyl ether fuel and method of generating power in dry low NOx combustion system
10/06/1999CN1230630A Ignition method for combustion-chamber burner for gas-turbine installation
10/05/1999CA2172291C Pressurized ball bearing assemblies
09/1999
09/30/1999WO1999048837A1 Use of high temperature insulation for ceramic matrix composites in gas turbines
09/30/1999WO1999033701A3 Self-adjusting air intake
09/30/1999DE19812834A1 Procedure for igniting burner of combustion chambers in gas turbine plants by using gas-operated pilot flame
09/29/1999EP0945607A2 Intake-air cooling for a gas turbine of a combined power plant