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)
11/2001
11/08/2001US20010037728 Rotating regenerative absorber, desorber
11/08/2001US20010037646 Cooling structure of combustor tail tube
11/08/2001US20010037570 Repair of coated turbine components
11/07/2001EP1152191A2 Combustor having a ceramic matrix composite liner
11/07/2001EP1152125A1 Method and apparatus for the cooling of the inlet part of the axis of a steam turbine
11/07/2001EP0796986B1 Gas-turbine engine
11/06/2001US6313544 Self-contained energy center for producing mechanical, electrical, and heat energy
11/06/2001US6312832 Low thermal conductivity heat barrier coating, a metal article having such a coating, and a process for depositing the coating
11/06/2001US6312220 Air turbine motor
11/06/2001US6312218 Sealing arrangement
11/06/2001US6312215 Turbine engine windmilling brake
11/06/2001US6311475 Device for igniting a combustion in a combustion chamber of a gas turbine
11/06/2001US6311474 Combined cycle electric power plant
11/06/2001US6311472 Method and means of fluid supply for combustion systems
11/06/2001CA2215276C Method and apparatus for detecting burner blowout
11/01/2001US20010035003 Passive mounted lining system
10/2001
10/31/2001EP1149998A2 Water injection for reducing gas turbine engine emissions
10/31/2001EP1149986A2 Turbine frame assembly
10/31/2001EP1149985A2 Metallic shroud structure
10/31/2001EP1149984A2 Hook support for a closed circuit fluid cooled gas turbine nozzle stage segment
10/31/2001EP1149982A2 A method of joining a vane cavity insert to a nozzle segment of a gas turbine
10/31/2001EP0898646B1 Closed loop air cooling system for combustion turbines
10/31/2001DE10020673A1 Metal housing structure for running blade area of axially through-flowed compressor and turbine stages, particularly in gas turbine drive units, has circular ring-shaped, closed, mechanically stable outer wall and inner wall
10/31/2001CN1074085C Exhaust recirculation type combined plant
10/30/2001US6310022 Hydroxylated wetting agent selected from polypropylene glycol, polyethylene glycol, glycerine, ethylene glycol, propylene glycol, chelating agent, emulsifier, crown ether
10/30/2001US6309177 Concentricity ring
10/30/2001US6308740 Method and system of pulsed or unsteady ejector
10/30/2001US6308513 Turbine and gas turbine
10/30/2001US6308512 Supercharging system for gas turbines
10/30/2001US6308511 Method and device for cooling guide vanes in a gas turbine plant
10/30/2001US6308409 Recuperator cell assembly system
10/30/2001CA2262722C Gas turbine combined plant, method of operating the same, and steam-cooling system for gas turbine hot section
10/28/2001CA2344109A1 Methods and apparatus for reducing gas turbine engine emissions
10/25/2001WO2001021847A3 Superalloys with improved weldability for high temperature applications
10/25/2001US20010034582 Thermal efficiency diagnostic method and apparatus of a combined power generation plant
10/25/2001US20010032477 Heat exchanger for cooling and for a pre-cooler for turbine intake air conditioning
10/25/2001US20010032450 Adaptable, modular efficient gas turbine power plant and associated method
10/24/2001EP1148299A1 Method and apparatus for increasing heat transfer from combustors
10/24/2001EP1148221A2 Method and device to cool the casings of turbojet engines
10/24/2001EP1148220A2 Combustion turbine cooling media supply system and related method
10/24/2001EP1148210A2 Steam cooling apparatus for turbine
10/24/2001EP1147849A1 Method for repositioning or repairing holes
10/24/2001EP1146989A1 Laser drilling holes in a cylindrical workpiece
10/23/2001US6307278 Microturbine power generating system
10/23/2001US6307275 Method and apparatus for controlling a high-speed AC permanent magnet synchronous motor coupled to an industrial turbo engine
10/23/2001US6306515 Thermal barrier and overlay coating systems comprising composite metal/metal oxide bond coating layers
10/23/2001US6305172 Scroll for a combustion system
10/23/2001US6305158 Combustion turbine power plant operable at full power using supplemental compressed air
10/23/2001US6305157 Gas turbine engine
10/23/2001US6305156 Integrated bleed air and engine starting system
10/23/2001US6305155 System for compensating for a pressure loss in the cooling-air ducting in a gas turbine plant
10/23/2001US6305077 Repair of coated turbine components
10/23/2001CA2076117C Gas turbine engine polygonal structural frame with axially curved panels
10/18/2001WO2001076348A2 Improved brush-seal designs for turbines and similar rotary apparatus
10/18/2001WO2001019675A3 Supersonic external-compression diffuser and method for designing same
10/18/2001US20010031199 Steam control apparatus for turbine
10/18/2001US20010031198 Frangible cover for turbofan engine blade removal and access
10/18/2001US20010030425 Combustion control method and system
10/18/2001US20010029680 Method and treatment device for the cooling of highly heated metal components
10/18/2001DE10017429A1 Verbundkeramiksubstrat mit gradierter thermochemischer Schutzschicht Composite ceramic substrate with graded thermochemical protective layer
10/18/2001DE10016259A1 Kompaktes millimeterwellentechnisches System zum Enteisen und/oder Vorbeugen einer Vereisung der äußeren Oberfläche von meteorologischen Einflüssen ausgesetzten Hohlraum- oder Schalenstrukturen Compact millimeter wave technology system for de-icing and / or preventing icing of the outer surface exposed on meteorological conditions cavity or shell structures
10/18/2001DE10005246C1 Exhaust gas turbocharger for IC engine has force acting on compressor shaft supported by magnetic bearing detected for controlling variable turbine geometry
10/17/2001EP1146289A1 Cooling structure of combustor tail tube
10/17/2001EP1146203A2 Impingement cooling of an undercut region of a turbine nozzle segment
10/17/2001EP1146202A2 Side wall cooling of a turbine nozzle segment
10/17/2001EP1146201A2 A method of controlling the side wall thickness of a turbine nozzle segment for improved cooling
10/17/2001EP1144826A1 Apparatus and method to increase turbine power
10/17/2001EP1144808A1 Method of cooling a combustion turbine
10/17/2001EP1144710A2 Electron beam physical vapor deposition apparatus and control panel therefor
10/17/2001EP1144141A1 Multipiece core assembly
10/17/2001EP0785837B1 Interactive laser welding at elevated temperatures of superalloy articles
10/17/2001CN1318138A Sealing system, esp for rotary machine
10/17/2001CN1317633A Method and appts. for reducing heat stress in gas turbine
10/16/2001US6302649 Superalloy weld composition and repaired turbine engine component
10/16/2001US6302647 Turbine inlet scroll
10/16/2001US6301928 Method for improving the performance of a cryogenic heat exchanger under frosting conditions
10/16/2001US6301897 Gas turbine suction air-cooling system
10/16/2001US6301874 Combined cycle power plant with steam-cooled gas turbine
10/16/2001CA2297610C Ultra-high efficiency turbine and fuel cell combination
10/16/2001CA2244048C Gas turbine interstage portion seal device
10/16/2001CA2242073C Combined cycle power generation plant
10/11/2001WO2001075383A1 A heat exchanger
10/11/2001WO2001075286A1 Regenerative fuel heating system
10/11/2001WO2001075272A2 Turbine engine foreign object damage detection system
10/11/2001WO2001074662A1 Compact millimeter wave technical system for de-icing and/or preventing the formation of ice on the outer surface of hollow or shell structures exposed to meteorological influences
10/11/2001US20010028845 Air turbine starter with seal assembly
10/11/2001US20010027653 Cooling system for gas turbine combustor
10/11/2001US20010027642 Intake-air cooling type gas turbine power equipment and combined power plant using same
10/11/2001US20010027641 Fluid apparatus and method of using the same
10/11/2001US20010027640 Fuel divider and ecology system for a gas turbine engine
10/11/2001US20010027637 Gas-turbine engine combustion system
10/11/2001DE10014810A1 Exhaust gas turbocharger radial turbine for internal combustion engine; has turbine wheel and flow channel for working medium and has separating wall between turbine and bearing casings
10/11/2001CA2403783A1 A heat exchanger
10/10/2001EP1143319A1 Device and method of flow and pressure regulation of the fuel actuating a servovalve unit
10/10/2001EP1143201A2 Cooling system for gas turbine combustor
10/10/2001EP1143196A1 Methods and apparatus for reducing thermal stresses within turbine engines
10/10/2001EP1143128A2 Fuel supply system
10/10/2001EP1143110A2 Side wall cooling for nozzle segments of a gas turbine
10/10/2001EP1143109A2 Impingement cooling of an undercut region of a turbine nozzle segment
10/10/2001EP1143107A2 Gas turbine transition duct end frame cooling