| 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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| 03/29/2011 | CA2559963C Gas turbine engine provided with a foreign matter removal passage |
| 03/29/2011 | CA2473335C Improved device for attaching a motor shaft to a bearing support |
| 03/29/2011 | CA2425409C Process of formation of a ceramic coating on a substrate by electron-beam physical vapor deposition |
| 03/28/2011 | CA2714861A1 Gas turbine engine breather exhaust oil collector |
| 03/25/2011 | CA2715209A1 Ventilation for a turbine wheel in a turbomachine |
| 03/25/2011 | CA2715169A1 Cooling system for a gas turbine and corresponding operation method |
| 03/24/2011 | WO2011034469A1 A noise attenuation panel and a gas turbine component comprising a noise attenuation panel |
| 03/24/2011 | WO2011033697A1 Mounting/dismounting jig for combustor tail pipe and tail pipe installation method |
| 03/24/2011 | WO2011033204A1 Turbine engine with contra-rotating non-ducted propellers |
| 03/24/2011 | WO2011007303A4 System and method for enhancing engine performance |
| 03/24/2011 | WO2010087984A3 Combined heat and power with a peak temperature heat load |
| 03/24/2011 | US20110070079 Annular seal |
| 03/24/2011 | US20110070075 Fastback turbulator structure and turbine nozzle incorporating same |
| 03/24/2011 | US20110068541 Oil seal assembly |
| 03/24/2011 | US20110068222 Propulsion unit for an aircraft and air intake structure for such a unit |
| 03/24/2011 | US20110067412 Gas turbine aircraft engines and operation thereof |
| 03/24/2011 | US20110067409 Air Cooled Turbine Component Having an Internal Filtration System |
| 03/24/2011 | US20110067404 Universal Multi-Nozzle Combustion System and Method |
| 03/24/2011 | US20110067403 Lean burn injectors having multiple pilot circuits |
| 03/24/2011 | US20110067402 Fuel Nozzle Assembly for Use in a Combustor of a Gas Turbine Engine |
| 03/24/2011 | US20110067379 Dual fuel combustor nozzle for a turbomachine |
| 03/24/2011 | DE102010037409A1 Universelles Mehrfachdüsen-Verbrennungssystem und Verfahren Universal multi-nozzle combustion system and method |
| 03/24/2011 | DE102010037353A1 Brennstoffdüsenrollmembrandichtung Fuel nozzle rolling diaphragm seal |
| 03/24/2011 | DE102009029647A1 Axial-Radial-Strömungsmaschine Axial-radial flow machine |
| 03/24/2011 | DE102009029540A1 Device for protection of turbo engines from impact of external bodies, e.g. bird strike, is provided at air inlet of turbo engine and has aerodynamic protection elements |
| 03/24/2011 | DE102005025823B4 Verfahren und Vorrichtung zum Kühlen einer Brennkammerauskleidung und eines Übergangsteils einer Gasturbine Method and apparatus for cooling a combustor liner and a transition piece of a gas turbine |
| 03/23/2011 | EP2299092A2 Air Particle Separator for a Gas Turbine Engine |
| 03/23/2011 | EP2299091A1 Method for Switching over a Gas Turbine Burner Operation from Liquid to Gas Fuel and Vice-Versa |
| 03/23/2011 | EP2299067A2 Turbomachine core coupling assembly |
| 03/23/2011 | EP2296963A1 Shape-changing structure with superelastic foam material |
| 03/23/2011 | CN101988431A System and method for supplying fuel to a gas turbine |
| 03/23/2011 | CN101988430A Combustion gas turbine |
| 03/22/2011 | US7908840 Turbine engine with integrated generator having shared lubrication system |
| 03/22/2011 | CA2619081C Seal structure of gas turbine combustor |
| 03/22/2011 | CA2413126C Structure for separating the high and low pressure turboexpanders of a gas turbine |
| 03/17/2011 | WO2011031340A2 Self-contained oil feed heat shield for a gas turbine engine |
| 03/17/2011 | US20110061397 Circumferentially self expanding combustor support for a turbine engine |
| 03/17/2011 | US20110061396 Relighting a Turbofan Engine |
| 03/17/2011 | US20110061395 Method of fuel staging in combustion apparatus |
| 03/17/2011 | US20110061394 Method of heat treating a ni-based superalloy article and article made thereby |
| 03/17/2011 | US20110061392 Combustion cavity layouts for fuel staging in trapped vortex combustors |
| 03/17/2011 | US20110061391 Vortex premixer for combustion apparatus |
| 03/17/2011 | US20110061390 Inlet premixer for combustion apparatus |
| 03/17/2011 | US20110061389 Radial Inlet Guide Vanes for a Combustor |
| 03/17/2011 | DE202011001683U1 Schalldämmmaterial Sound Absorbing Materials |
| 03/17/2011 | DE102010037052A1 Prallgekühlter hinterer Rahmen eines Übergangsstücks Impingement cooled rear frame of a transition piece |
| 03/17/2011 | DE102009039184A1 Turbomaschine Turbomachine |
| 03/16/2011 | EP2295861A1 Burner, especially for gas turbines |
| 03/16/2011 | EP2295767A2 An aerospace fuel metering unit (FMU) |
| 03/16/2011 | EP2295766A2 Combined-cycle steam turbine having novel steam cooling flow configuration |
| 03/16/2011 | EP2295765A1 Autonomous cooling process, adaptable to thermal engines including gas turbine engines |
| 03/16/2011 | EP2295763A2 Reversed-flow core for a turbofan with a fan drive gear system |
| 03/16/2011 | EP2295726A1 Gas turbine engine compressor with integrated starter/generator |
| 03/16/2011 | EP2295725A1 Fluid flow engine with steam removal |
| 03/16/2011 | EP2295166A1 Investment casting cores |
| 03/16/2011 | EP2294303A1 Exhaust washed structure and associated composite structure and method of fabrication |
| 03/16/2011 | EP2140121B1 Method and system for starting a turboshaft engine by cold weather |
| 03/16/2011 | EP2016266B1 Integrated engine exhaust systems and methods for drag and thermal stress reduction |
| 03/16/2011 | CN201763452U Air-collecting cavity for bleeding of heavy gas turbine compressor |
| 03/15/2011 | US7905082 Method and system for increasing Modified Wobbe Index control range |
| 03/15/2011 | CA2516958C System for gas turbine health monitoring data fusion |
| 03/15/2011 | CA2496755C Torsionally de-coupled engine mount system |
| 03/15/2011 | CA2494950C Nested channel ducts for nozzle construction and the like |
| 03/15/2011 | CA2470682C Foam wall combustor construction |
| 03/15/2011 | CA2466581C Off loading clutch for gas turbine engine starting |
| 03/10/2011 | WO2011026982A1 Method for switching over a gas turbine burner operation from liquid to gas fuel and vice-versa |
| 03/10/2011 | WO2011026960A1 Method of operating a gas turbine and gas turbine |
| 03/10/2011 | WO2011026732A1 Gas turbine group |
| 03/10/2011 | WO2011026636A2 Method for the operation of a micro gas turbine arrangement, and micro gas turbine arrangement for converting biomass into energy |
| 03/10/2011 | WO2010037450A3 Turbine cooling system |
| 03/10/2011 | US20110057056 Monolithic fuel injector and related manufacturing method |
| 03/10/2011 | US20110056213 Spool support structure for a multi-spool gas turbine engine |
| 03/10/2011 | US20110056212 System and method for applying energy externally for fuel gas for dew point heating in gas turbine power plant |
| 03/10/2011 | US20110056206 Fuel Injector for Use in a Gas Turbine Engine |
| 03/10/2011 | US20110056204 Self-Contained Oil Feed Heat Shield for a Gas Turbine Engine |
| 03/10/2011 | US20110056179 Turbine exhaust diffuser with region of reduced flow area and outer boundary gas flow |
| 03/10/2011 | DE102010037107A1 System und Verfahren zum externen Zuführen von Energie für ein Brennstoffgas zur Taupunktheizung in einem Gasturbinenkraftwerk System and method for supplying external energy for a fuel gas to Taupunktheizung in a gas turbine power plant |
| 03/10/2011 | DE102010037047A1 Stark umlenkende Diffusorstrebe mit Überströmschlitzen Strong deflecting diffuser strut with transfer ports |
| 03/10/2011 | DE102009035293A1 Aircraft safety device has flexible rod mounted in front direction of flight with radial sensors, which makes birds to swing to side, where one type of formed or rejuvenated semi-spherical dome is attached at front side |
| 03/10/2011 | CA2678324A1 Bearing suppport flexible ring |
| 03/08/2011 | US7900461 Combustor liner support and seal assembly |
| 03/08/2011 | US7900438 Heat transfer system and method for turbine engine using heat pipes |
| 03/08/2011 | US7900437 Heat transfer system and method for turbine engine using heat pipes |
| 03/03/2011 | WO2011025484A1 Hydrodynamic circumferential seal system for large translations |
| 03/03/2011 | WO2011024242A1 Split ring cooling structure and gas turbine |
| 03/03/2011 | WO2010133482A3 Method and apparatus for cooling a gaseous hydrocarbon stream |
| 03/03/2011 | WO2010126980A3 Transcritical thermally activated cooling, heating and refrigerating system |
| 03/03/2011 | WO2010018338A3 Fuel flow metering valve |
| 03/03/2011 | US20110054704 High fidelity integrated heat transfer and clearance in component-level dynamic turbine system control |
| 03/03/2011 | US20110053023 Method for operating a fuel cell and a fuel cell arrangement |
| 03/03/2011 | US20110052376 Inter-stage seal ring |
| 03/03/2011 | US20110049812 Seal System Between Transition Duct Exit Section and Turbine Inlet in a Gas Turbine Engine |
| 03/03/2011 | US20110048030 Impingement cooled transition piece aft frame |
| 03/03/2011 | US20110048029 Turbomachine core coupling assembly |
| 03/03/2011 | US20110048027 Turbine Driven By Predetermined Deflagration Of Anaerobic Fuel And Method Thereof |
| 03/03/2011 | US20110048026 System And Process For The Reduction Of Harmful Substances In Engine Exhaust Gases |
| 03/03/2011 | US20110048023 Fuel nozzle swirler assembly |
| 03/03/2011 | US20110048022 System and method for combustion dynamics control of gas turbine |
| 03/03/2011 | US20110048021 Acoustically stiffened gas turbine combustor supply |
| 03/03/2011 | US20110048020 Acoustic damper |