| 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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| 05/18/2004 | US6735953 Turbomachine-driven environmental control system |
| 05/18/2004 | US6735952 Single pump lubrication and starter system |
| 05/18/2004 | US6735949 Gas turbine engine combustor can with trapped vortex cavity |
| 05/13/2004 | WO2004015257A3 Particle separator for a turbine engine |
| 05/13/2004 | WO2004003357A3 Orbiting combustion nozzle engine |
| 05/13/2004 | US20040091361 Methods and apparatus for reducing flow across compressor airfoil tips |
| 05/13/2004 | US20040091350 Fluidic actuation for improved diffuser performance |
| 05/13/2004 | US20040090211 Method and apparatus for compensating output voltage fluctuations of turbine/alternator on common shaft |
| 05/13/2004 | US20040088998 Turbine |
| 05/13/2004 | US20040088995 Method for cooling a gas turbine and gas turbine installation |
| 05/13/2004 | US20040088991 Fault management system for gas turbine engines |
| 05/13/2004 | US20040088987 Integrated gas compressor |
| 05/13/2004 | US20040088980 Method for converting thermal energy into mechanical work |
| 05/13/2004 | US20040088966 1-Axis type combined cycle plant |
| 05/12/2004 | EP1418478A1 Apparatus for reading identification connectors |
| 05/12/2004 | EP1418320A1 Gas turbine |
| 05/12/2004 | EP1418319A1 Gas turbine |
| 05/12/2004 | EP1418312A2 Turbine blade oxidation monitoring and life prediction using neural network based diagnostic techniques in conjunction with pyrometer signals |
| 05/12/2004 | EP1418255A1 Electrochemical Process for the Simultaneous Stripping of Diverse Coatings From a Metal Substrate |
| 05/12/2004 | EP1418252A2 Multiphase thermal barrier coatings for very high temperature applications |
| 05/12/2004 | EP0993543B1 Cooling scheme for turbine hot parts |
| 05/12/2004 | CN1495351A System for controlling and regulating rlame temp. of single shaft gas turbine |
| 05/12/2004 | CN1495341A Easy-to-assemble heat-screening device for connecting cooling tube and through hole |
| 05/12/2004 | CN1495339A Simplified nozzle supporting device for gas turbine |
| 05/12/2004 | CN1495235A Thermal-insulating coating with low thermal conductivity |
| 05/12/2004 | CA2447460A1 System and method for displaying real-time turbine corrected output and heat rate |
| 05/11/2004 | US6733238 Axial-flow turbine having stepped portion formed in axial-flow turbine passage |
| 05/11/2004 | US6733235 Shroud segment and assembly for a turbine engine |
| 05/11/2004 | US6733229 Insert metering plates for gas turbine nozzles |
| 05/11/2004 | US6733014 Brush seal |
| 05/11/2004 | US6732532 Resilient mount for a CMC combustion chamber of a turbomachine in a metal casing |
| 05/11/2004 | US6732531 Combustion system for a gas turbine engine with variable airflow pressure actuated premix injector |
| 05/11/2004 | US6732530 Gas turbine compressor and clearance controlling method therefor |
| 05/11/2004 | US6732529 Off loading clutch for gas turbine engine starting |
| 05/11/2004 | US6732528 Gas turbine combustor |
| 05/11/2004 | CA2263036C Gas turbine combined cycle |
| 05/06/2004 | WO2004038229A1 Method for operating a compressor in the region of the compressor pumping point, and compressor |
| 05/06/2004 | WO2004038199A1 Method and system for controlling gas turbine engine |
| 05/06/2004 | WO2004038196A2 Gas turbine engine starting system and method |
| 05/06/2004 | WO2004038180A1 Apparatus and method for reducing the heat load of an airfoil |
| 05/06/2004 | US20040086635 Method of repairing a stationary shroud of a gas turbine engine using laser cladding |
| 05/06/2004 | US20040086387 Continual radial loading device for steam turbine reaction type buckets and related method |
| 05/06/2004 | US20040086382 Gas turbine engine axial stator compressor |
| 05/06/2004 | US20040086379 Flowpath sealing and streamlining configuration for a turbine |
| 05/06/2004 | US20040086024 Turbine blade (bucket) health monitoring and prognosis using neural network based diagnostic techniques in conjunction with pyrometer signals |
| 05/06/2004 | US20040083801 Apparatus and method for inspecting dovetail slot width for gas turbine engine disk |
| 05/06/2004 | US20040083736 Turbine arrangement and a method of operating a turbine arrangement |
| 05/06/2004 | US20040083712 Heat transfer apparatus |
| 05/06/2004 | US20040083711 Fuel metering unit with a compensated regulator valve in a turbomachine |
| 05/06/2004 | EP1416206A2 Valve having pressure balancing piston and method involving same |
| 05/06/2004 | EP1416136A1 Fuel metering apparatus with a compensated regulating valve in a turbomachine |
| 05/06/2004 | EP1416135A1 Plate-like body joining method, joined body, gas turbine burner tail pipe, and gas turbine burner |
| 05/06/2004 | EP1416123A2 Vortex inlet vanes |
| 05/06/2004 | EP1416122A2 Apparatus and method for inspecting dovetail slot width for gas turbine engine rotor disk |
| 05/06/2004 | EP1415112A1 Pre-mix burner and method for operation thereof |
| 05/06/2004 | DE10249471A1 Verfahren zum Betreiben eines Verdichters im Bereich der Verdichter-Pumpgrenze und Verdichter A method of operating a compressor in the compressor surge margin and compressor |
| 05/06/2004 | DE10247905A1 Verfahren zum Hochfahren eines Wellenstranges sowie Vorrichtung zur Durchführung des Verfahrens A method for powering up a shaft assembly as well as apparatus for carrying out the method |
| 05/06/2004 | CA2446323A1 Turbine blade (bucket) health monitoring and prognosis using neural network based diagnostic techniques in conjunction with pyrometer signals |
| 05/05/2004 | CN1494633A Method for closing used hole on top of gas turbine blade |
| 05/04/2004 | US6730422 Thermal barrier coatings with low thermal conductivity |
| 05/04/2004 | US6730413 Thermal barrier coating |
| 05/04/2004 | US6730179 Method for producing local aluminide coating |
| 05/04/2004 | US6729142 Thermal turbomachine and process for igniting the thermal turbomachine |
| 05/04/2004 | US6729140 Electrical machine |
| 04/30/2004 | CA2446343A1 Method of repairing a stationary shroud of a gas turbine engine using laser cladding |
| 04/29/2004 | WO2004036731A1 Method for running-up a shaft assembly and device for carrying out the method |
| 04/29/2004 | WO2003098006A8 Turbine no-load speed limiter |
| 04/29/2004 | WO2003074210A3 Method and device for producing precision investment-cast ne metal alloy members and ne metal alloys for carrying out said method |
| 04/29/2004 | US20040081548 Flow directing device |
| 04/29/2004 | US20040080300 Gas turbine engine starter-generator exciter starting system and method |
| 04/29/2004 | US20040080164 Turbine generator starting method and turbine generation system |
| 04/29/2004 | US20040079834 Active system for wide area suppression of engine vortex |
| 04/29/2004 | US20040079082 Combustor liner with inverted turbulators |
| 04/29/2004 | US20040079081 Fuel system |
| 04/28/2004 | EP1413831A1 Annular combustor for a gas turbine and gas turbine |
| 04/28/2004 | EP1413829A2 Combustor liner with inverted turbulators |
| 04/28/2004 | EP1413822A1 Uncoupling arrangement of a turbojet engine fan using an explosive charge |
| 04/28/2004 | EP1413771A1 Casing, compressor, turbine and gas turbine engine having such casing |
| 04/28/2004 | EP1413721A2 Air inlet for an aircraft jet engine with an active system for the suppression of a ground vortex |
| 04/28/2004 | EP1413715A1 Impingement cooling of a gas turbine rotor blade platform |
| 04/28/2004 | EP1413711A1 Process and device for cooling of gas turbine rotor blades |
| 04/28/2004 | EP1412618A1 Seal element for sealing a gap and combustion turbine having a seal element |
| 04/28/2004 | EP1198619B1 Bond coats for turbine components and method of applying the same |
| 04/28/2004 | EP0944767B1 Process for preparing an abradable seal, abradable seal, and gas turbine engine component comprising such an abradable seal |
| 04/28/2004 | CN2613604Y Technological diffuser for engine |
| 04/28/2004 | CN1492187A Double circular burning chamber prefabricated machine cover of gas turbine engine and its producing method |
| 04/28/2004 | CN1492184A Premixing burner, gas turbine and fuel burning method with distributive mass flow |
| 04/28/2004 | CN1492129A Method and device for supporting variable bypass valve system |
| 04/28/2004 | CN1492065A Nickel base alloy |
| 04/27/2004 | US6726444 Hybrid high temperature articles and method of making |
| 04/27/2004 | US6725876 Control valve with integrated electro-hydraulic actuator |
| 04/27/2004 | US6725666 Combustion-chamber arrangement |
| 04/27/2004 | US6725665 Method of operation of gas turbine having multiple burners |
| 04/27/2004 | US6725663 Power plant and associated starting method |
| 04/27/2004 | US6725645 Turbofan engine internal anti-ice device |
| 04/27/2004 | US6725540 Method for repairing turbine engine components |
| 04/23/2004 | CA2446035A1 Flow directing device |
| 04/22/2004 | WO2004033966A1 A fuel injector |
| 04/22/2004 | WO2004033874A1 Combustor controller |
| 04/22/2004 | WO2004033873A1 Air intake housing, in particular for the air intake of gas turbines |