| 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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| 10/31/2007 | CN200968223Y Sealing apparatus between combustion engine turbine stages |
| 10/31/2007 | CN101063422A Methods and system for reducing pressure losses in gas turbine engines |
| 10/31/2007 | CN100346066C System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber |
| 10/31/2007 | CN100346059C 涡轮叶片和燃气轮机 Turbine blades and turbine |
| 10/30/2007 | US7287961 Retaining arrangement |
| 10/30/2007 | US7287955 Gas turbine clearance control devices |
| 10/30/2007 | US7287384 Bearing chamber pressurization system |
| 10/30/2007 | US7287382 Gas turbine combustor end cover |
| 10/30/2007 | US7287368 Fluid system |
| 10/30/2007 | CA2335019C A method for starting a combustion device |
| 10/25/2007 | WO2007120185A2 Gas turbine engine mixing duct and method to start the engine |
| 10/25/2007 | WO2007119404A1 Ni-BASE SUPERALLOY, METHOD FOR PRODUCING SAME, AND TURBINE BLADE OR TURBINE VANE COMPONENT |
| 10/25/2007 | WO2003071117A8 Ejector based engines |
| 10/25/2007 | US20070246302 Pre-heating an aircraft oil reservoir |
| 10/25/2007 | US20070246293 Method and device for reducing engine noise |
| 10/25/2007 | US20070246183 Refractory metal core wall thickness control |
| 10/25/2007 | US20070245746 Methods and systems for detecting rotor assembly speed oscillation in turbine engines |
| 10/25/2007 | US20070245745 Method and device for optimizing a light-up procedure of a gas turbine engine |
| 10/25/2007 | US20070245706 Pre-heating of a liquid in an aircraft reservoir |
| 10/25/2007 | US20070245697 Single/multiple guard(s)/cap(s) and/or screen(s) with engine attached apparatus and/or pole with rotational system(s)-centrifuge chamber/manifold particle collector |
| 10/25/2007 | DE102007018374A1 Verfahren und Gerät für den Betrieb eines Gasturbinentriebwerks Method and apparatus for operating a gas turbine engine |
| 10/25/2007 | DE102007015125A1 Kegelstumpfturbinenmotor mit diagonaler Strömungsrichtung, bei dem zB Explosionsgase oder Dampf bei der Expansion in vorgegebene diagonale Richtung die Turboantriebsschaufeln durchströmen und durch Hebelkraft die Antriebswelle in kraftvolle Drehbewegungen versetzen Truncated cone turbine engine with a diagonal flow direction in which eg explosion gases or vapor flow through the turbo drive blades in the expansion given in diagonal direction and move through leverage the drive shaft into powerful rotary movements |
| 10/25/2007 | CA2626259A1 Gas turbine engine mixing duct and method to start the engine |
| 10/24/2007 | EP1847737A2 Variable clearance positive pressure packing ring and carrier arrangement with leaf springs |
| 10/24/2007 | EP1847699A2 Relighting a turbofan engine |
| 10/24/2007 | EP1847698A1 Pre-heating of a liquid in an aircraft reservoir |
| 10/24/2007 | EP1846641A1 Method for activating a pressure storage system, and a pressure storage system |
| 10/24/2007 | CN200965136Y Heavy type combustion turbine case system |
| 10/24/2007 | CN101059102A Variable power nozzle ejector for turbine system |
| 10/24/2007 | CN101059101A Gas turbine inlet conditioning system and method |
| 10/24/2007 | CN100344396C Process and apparatus for manufacturing a turbine component, turbine components and use of apparatus |
| 10/23/2007 | US7286966 Rotation planning apparatus and rotation planning system |
| 10/23/2007 | US7284957 Composite integrally bladed rotor |
| 10/23/2007 | US7284378 Methods and apparatus for low emission gas turbine energy generation |
| 10/23/2007 | US7284377 Method and apparatus for operating an intercooler for a gas turbine engine |
| 10/23/2007 | US7284364 Passive exhaust suppressor and method |
| 10/23/2007 | US7284363 Method of power generation for airborne vehicles |
| 10/23/2007 | CA2399710C Method for producing local aluminide coating |
| 10/23/2007 | CA2244528C Leaktight fitting for a shaft end |
| 10/18/2007 | US20070240427 Compact compound engine package |
| 10/18/2007 | US20070240416 Integral cooling system for rotary engine |
| 10/17/2007 | EP1845236A2 Flap gasket for a turbo engine |
| 10/17/2007 | EP1844223A1 Ventilating air intake arrangement with mobile closing device |
| 10/17/2007 | EP1204532B1 One-step noble metal-aluminide coatings |
| 10/17/2007 | CN101057104A Burner starting method |
| 10/17/2007 | CN100343647C Estimating method for fatigue life of turbine blade, turbine blade creep elongation strain measurement device and turbine blade |
| 10/17/2007 | CN100343556C Method of manufacturing axis seals, axis seals, axis seals members and rotary machine using axis seals |
| 10/16/2007 | US7281382 Method and apparatus for detecting the presence of flame in the exhaust path of a gas turbine engine |
| 10/16/2007 | CA2343189C Laser drilling holes in a cylindrical workpiece |
| 10/11/2007 | WO2007112726A1 Jet engine with detachably arranged generator unit |
| 10/11/2007 | WO2006096796A3 Torque drive mechanism for gas compressor |
| 10/11/2007 | US20070237971 Comprising zirconia; low thermal conductivity and high thermomechanical strength |
| 10/11/2007 | US20070237639 Turbine element |
| 10/11/2007 | US20070235157 Method of forming concavities in the surface of a metal component, and related processes and articles |
| 10/11/2007 | US20070234734 System and method for turbine engine startup profile characterization |
| 10/11/2007 | US20070234733 Small gas turbine engine with multiple burn zones |
| 10/11/2007 | US20070234732 Gas turbine engine fuel control system having a transfer valve and a shutoff valve and a common controller therefor |
| 10/11/2007 | US20070234731 System and method for providing air to a compressor of an aircraft auxiliary gas turbine engine |
| 10/11/2007 | US20070234729 Methods and apparatus for cooling gas turbine engine components |
| 10/11/2007 | US20070234725 Counterbalanced fuel slinger in a gas turbine engine |
| 10/11/2007 | US20070234724 Redundant fuel manifold sealing arrangement |
| 10/11/2007 | US20070234703 Sealing structure of spindle bolt, and gas turbine |
| 10/11/2007 | DE102006016147A1 Verfahren zum Herstellen einer Wabendichtung A method for manufacturing a honeycomb seal |
| 10/11/2007 | DE102006015639A1 Strahltriebwerk mit Generatoreinheit Jet engine with generator unit |
| 10/11/2007 | DE102006012977A1 Thermal-insulating layer system for use in e.g. gas turbine, has active thermal-insulating layer counteracting heat flow, which is defined by intrinsic thermal conductivity of passive poor heat conducting thermal-insulating layer |
| 10/11/2007 | CA2647468A1 Jet engine with detachably arranged generator unit |
| 10/10/2007 | EP1843045A1 Turbofan engine |
| 10/10/2007 | EP1843022A2 System and method for providing air to a compresssor of an aircraft auxiliary gas turbine engine |
| 10/10/2007 | EP1841967A1 Intercooled turbo-compressor |
| 10/10/2007 | EP1841960A1 Starter generator system for a tip turbine engine |
| 10/10/2007 | EP1699697B1 Air guiding flap of an aircraft comprising control of the pressure forces impinging thereon, process for adjusting the position of an air guiding flap and ram air system including such an air guiding flap |
| 10/10/2007 | EP1388131B1 Improved fluid metering device |
| 10/10/2007 | CN101052784A Air inlet for turbine supercharger of internal-combustion engine |
| 10/10/2007 | CN101050727A Medium cooling isobaric backheating gas turbine |
| 10/10/2007 | CN101050726A System and method for providing air to a compresssor of an aircraft auxiliary gas turbine engine |
| 10/10/2007 | CN101050713A Closed loop, steam cooled turbine shroud |
| 10/09/2007 | US7278827 Cooling air evacuation slots of turbine blades |
| 10/09/2007 | US7278475 Control arrangement for cooling power electronic components |
| 10/09/2007 | US7278472 Internally mounted radial flow intercooler for a combustion air changer |
| 10/09/2007 | US7278255 Gas turbine installation |
| 10/09/2007 | CA2333030C A rotor machine device |
| 10/05/2007 | CA2582806A1 System and method for providing air to a compressor of an aircraft auxiliary gas turbine engine |
| 10/04/2007 | WO2007110494A1 Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone |
| 10/04/2007 | WO2007110491A1 Air inlet shroud structure |
| 10/04/2007 | US20070232327 Wireless terminal location using apparatus and methods employing carrier diversity |
| 10/04/2007 | US20070231122 Turbine Nozzle Segment, Turbine Nozzle, Turbine, and Gas Turbine Engine |
| 10/04/2007 | DE3601957B3 Wärmeschutzauskleidung für Brennkammern von Strahltriebwerken Heat resistant lining for combustion chambers of jet engines |
| 10/04/2007 | DE102007015311A1 Method for operating a gas turbine wherein during conversion of combustion process based on liquid fuel operation to gaseous operation, the first fuel which is kept back by combustion is purged by means of water |
| 10/04/2007 | DE102006019722A1 Secondary burner attachment device for sequential operating gas turbine system, has fuel mixture burned in primary burner during formation of hot gases, supplied to burner for secondary successive combustion, formed as flow channel |
| 10/04/2007 | DE102006015530A1 Turbo-machine e.g. turbine, for use in power plant, has axial sealant designed in circular recess of stator, and attached to rotor blade row, and completely circular opened groove for recess designed in upstream wall of recess |
| 10/04/2007 | CA2644592A1 Structure for an air inlet lip of an electric de-icing pod comprising an acoustic attenuation zone |
| 10/04/2007 | CA2637901A1 Air inlet shroud structure |
| 10/04/2007 | CA2580670A1 Integrated strut design for mid-turbine frames with u-base |
| 10/03/2007 | EP1840465A2 Burner system with staged fuel injection |
| 10/03/2007 | EP1839800A1 Method for local application of diffusion aluminide coating |
| 10/03/2007 | EP1263997B1 Casting systems and methods with auxiliary cooling onto a liquidus portion of a casting |
| 09/30/2007 | CA2582629A1 Apparatus to inject a mixture of air and fuel, combustion chamber and turbine engine equipped with such an apparatus |
| 09/29/2007 | CA2580164A1 Inverted stiffened shell panel torque transmission for loaded struts and mid-turbine frames |
| 09/27/2007 | WO2007106983A1 Calibration of optical patternator spray parameter measurements |
| 09/27/2007 | WO2007106982A1 Method of computing spray parameters from optical patternation |