| 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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| 01/17/2002 | WO2002004796A1 Method and system for power production and assemblies for retroactive mounting in a system for power production |
| 01/17/2002 | US20020006078 Sound-absorbing and reinforcing structure for engine nacelle acoustic panel |
| 01/17/2002 | US20020005643 Automatic turbogenerator restarting method and system |
| 01/17/2002 | US20020005233 Fine particle sizes; turbine blades |
| 01/17/2002 | US20020005038 Method and apparatus for the cooling of jet-engine turbine casings |
| 01/17/2002 | DE10002581C2 Turbolader Turbocharger |
| 01/16/2002 | EP1172610A1 Fuel nozzle for premix turbine combustor |
| 01/16/2002 | EP1172544A1 Combined turbo and rocket engine with air liquefier and air separator |
| 01/16/2002 | EP1172524A2 Method for deploying shroud segments of different thickness in a turbine engine |
| 01/16/2002 | EP1172523A2 Method and apparatus for supplying cooling air to turbine rotors |
| 01/16/2002 | EP1172460A2 A method for applying a high-temperature bond coat on a metal substrate |
| 01/16/2002 | EP1171699A2 Control of the inlet of an auxiliary power unit |
| 01/16/2002 | EP1171691A1 Frangible cover for turbofan engine blade removal and access |
| 01/15/2002 | US6339208 Method of forming cooling holes |
| 01/15/2002 | US6338578 Retaining arrangement for a bearing, in particular for a high pressure compressor shaft |
| 01/15/2002 | US6338241 Combined cycle power generation plant and operating method thereof |
| 01/15/2002 | US6338239 Turbine system having a reformer and method thereof |
| 01/15/2002 | CA2230334C Combined cycle power plant |
| 01/15/2002 | CA2065679C Shroud cooling assembly for gas turbine engine |
| 01/13/2002 | CA2352811A1 A fuel discharge member, a burner, a premixing nozzle of a combustor, a combustor, a gas turbine, and a jet engine |
| 01/10/2002 | WO2002003024A1 Play measuring sensor by multiple depth abrasion |
| 01/10/2002 | WO2002002920A1 System and method for gaseous fuel control for a turbogenerator/motor |
| 01/10/2002 | WO2002002913A1 Drainage system for gas turbine supporting bearings |
| 01/10/2002 | WO2002002912A1 Draining and cooling system for gas turbine cushions |
| 01/10/2002 | WO2002002911A1 Connecting system for a transition duct in a gas turbine |
| 01/10/2002 | WO2000066887A9 Thermodynamic process and system for generating work |
| 01/10/2002 | US20020002828 Thermal energy reusing system |
| 01/10/2002 | US20020002820 Gas turbine apparatus with heat exchanger |
| 01/10/2002 | US20020002819 Apparatus and methods for supplying auxiliary steam in a combined cycle system |
| 01/10/2002 | US20020002818 Apparatus for fuel nozzle staging for gas turbine engines |
| 01/09/2002 | EP1170571A1 Sensor to measure play by multi-stage abrasion |
| 01/09/2002 | EP1170207A2 Link component for aircraft engine mounting systems |
| 01/09/2002 | EP1169585A1 Self-centering brush seal |
| 01/09/2002 | EP1169557A1 Biomass combustion chamber for gas turbine |
| 01/09/2002 | EP1169495A1 Electrochemical stripping of turbine blades |
| 01/09/2002 | CN1330134A Nickel compound used as vanadium corrosion inhibitor and burning method using it |
| 01/08/2002 | US6336317 Quasi-isothermal Brayton cycle engine |
| 01/08/2002 | US6336316 Heat engine |
| 01/08/2002 | CA2252274C Gas turbine spindle bolt seal device |
| 01/08/2002 | CA2230325C Steam cooled gas turbine system |
| 01/03/2002 | WO2002001055A1 Method and apparatus for providing shutoff, overspeed protection, and directional control of a bypass flow in a fuel delivery system |
| 01/03/2002 | WO2002001047A1 Combined cycle power generation plant and method of operating such a plant |
| 01/03/2002 | US20020000343 Apparatus for damping acoustic vibrations in a combustor |
| 01/02/2002 | EP1167722A2 Methods and apparatus for delivering cooling air within gas turbines |
| 01/02/2002 | EP1167721A2 Method and system for cooling a gas turbine plant |
| 01/02/2002 | EP1167697A1 Turbine engine |
| 01/02/2002 | EP1167185A2 Sound-absorbing and reinforcing structure for engine nacelle acoustic panel |
| 01/02/2002 | EP1165964A2 Load sharing valve and system for operating centrifugal pumps in parallel |
| 01/02/2002 | EP1165942A1 Turbo-engine with an array of wall elements that can be cooled and method for cooling an array of wall elements |
| 01/02/2002 | EP1117588A4 Aircraft engine air intake system |
| 01/02/2002 | CN2469193Y Means for cooling feeding air for gas turbine |
| 01/01/2002 | US6335105 For forming part for a gas turbine engine, heat resistance |
| 01/01/2002 | US6334756 Turbine rotor, cooling method of turbine blades of the rotor and gas turbine with the rotor |
| 01/01/2002 | US6334755 Turbomachine including a device for supplying pressurized gas |
| 01/01/2002 | US6334746 Transport system for a power generation unit |
| 01/01/2002 | US6334299 Ramjet engine for power generation |
| 01/01/2002 | US6334296 Fuel divider and ecology system for a gas turbine engine |
| 01/01/2002 | US6334295 Rotating diffuser for pressure recovery in a steam cooling circuit of a gas turbine |
| 01/01/2002 | CA2251198C Gas turbine stationary blade |
| 01/01/2002 | CA2251192C Gas turbine stationary blade double cross type seal device |
| 01/01/2002 | CA2230317C Low temperature hydrogen combustion turbine |
| 12/28/2001 | CA2350970A1 Sound-absorbing and reinforcing structure for engine nacelle acoustic panel |
| 12/27/2001 | WO2001098437A1 Use of nickel compounds as vanadium corrosion inhibitors |
| 12/27/2001 | WO2001098232A1 Protective coating including porouos silicon nitride matrix and noble metal |
| 12/27/2001 | WO2001097951A1 Direct turbine air chiller/scrubber system |
| 12/27/2001 | US20010055653 Process for cleaning an article, process for coating an article, and device therefor |
| 12/27/2001 | US20010054354 Includes at least one spray scrubbing area, where the water is collected, recirculated, and filtered. |
| 12/26/2001 | CN1328617A Turbomachine |
| 12/26/2001 | CN1076782C Vane for gas turbine |
| 12/25/2001 | US6333488 Method for setting up and controlling confinement media flow in laser shock peening |
| 12/25/2001 | US6333484 Welding superalloy articles |
| 12/25/2001 | US6332321 Apparatus for augmenting power produced from gas turbines |
| 12/25/2001 | US6332272 Method of repairing a turbine blade |
| 12/25/2001 | CA2245639C Recovery type steam-cooled gas turbine |
| 12/20/2001 | WO2001096723A1 Method and apparatus for cooling the inlet air of combustion turbines |
| 12/20/2001 | WO2001048887A3 Brush seal |
| 12/20/2001 | US20010052231 Recuperator for use with turbine/turbo-alternator |
| 12/20/2001 | US20010052230 Fuel preheating in a gas turbine |
| 12/20/2001 | DE10027842A1 Gas turbine layout cooling system bleeds portion of film cooling air through turbine blade via inlet or outlet edge borings for direct blade wall service. |
| 12/20/2001 | DE10019437A1 Verfahren und Vorrichtung zum Kühlen der Gehäuse von Turbinen von Strahltriebwerken Method and apparatus for cooling the housing of turbines of jet engines |
| 12/19/2001 | EP1164273A2 Turbo jet engine with heat exchanger |
| 12/19/2001 | EP1164252A2 Support pedestals for a wall cover in a gas turbine nozzle segment |
| 12/19/2001 | EP1163430A1 Covering element and arrangement with a covering element and a support structure |
| 12/19/2001 | EP1163425A1 Turbine blade |
| 12/19/2001 | EP1163151A1 Modular air intake duct for aircraft |
| 12/19/2001 | EP0988441B1 Combustion turbine cooling panel |
| 12/19/2001 | CN1076430C Heat recovery gas turbine rotor |
| 12/18/2001 | US6331097 Method and apparatus for purging turbine wheel cavities |
| 12/18/2001 | US6331096 Apparatus and methods for impingement cooling of an undercut region adjacent a side wall of a turbine nozzle segment |
| 12/18/2001 | US6331078 Turbine engine bearing |
| 12/18/2001 | US6330985 Link component for aircraft engine mounting systems |
| 12/18/2001 | US6330789 Methods of operation a dual-fuel injector for a gas turbine with simultaneous liquid and gaseous fuels injection during transients |
| 12/18/2001 | CA2119246C Closed loop fuel control system and method |
| 12/18/2001 | CA2076100C Low noise fan assembly |
| 12/18/2001 | CA2076083C Flow activated flowpath liner seal |
| 12/18/2001 | CA2048829C High pressure compressor flowpath bleed valve extraction slot |
| 12/13/2001 | US20010051095 Turbine nozzle stage having thermocouple guide tube |
| 12/13/2001 | US20010049934 Method and apparatus for fuel gas moisturization and heating |
| 12/13/2001 | DE10027833A1 Verfahren zum Kühlen einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens A method for cooling a gas turbine plant and gas turbine system for implementing the method |
| 12/12/2001 | EP1162355A2 Cooling method for a gas turbine |