| 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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| 07/14/2011 | DE102010061593A1 Systeme und Vorrichtungen für eine Brennstoffsteuereinrichtung zur Verwendung in einer Gasturbine Systems and apparatus for a fuel control device for use in a gas turbine |
| 07/14/2011 | DE102010061592A1 Temperaturaktivierte Ventile für Gasturbinen Temperature-activated valves for gas turbines |
| 07/14/2011 | CA2786130A1 Contra-rotating propeller system for an aircraft turbine engine |
| 07/13/2011 | EP2343444A2 Fuel control arrangements for a gas turbine engine |
| 07/13/2011 | EP2343443A2 Steam turbine |
| 07/13/2011 | EP2343437A1 Turbine inlet air heat pump-type system |
| 07/13/2011 | EP2343401A1 Hydrophobic surface |
| 07/13/2011 | CN201896674U Intake cone of air-breathing pulse detonation engine |
| 07/13/2011 | CN201896664U Electricity generating device of miniature gas turbine |
| 07/13/2011 | CN102124198A Fuel injector sans support/stem |
| 07/13/2011 | CN102124197A Inner wall for the nacelle of a turbine engine |
| 07/13/2011 | CN102123942A Hydrogen production system and power generation system |
| 07/13/2011 | CN102121434A Low-entropy hybrid combustion circulating thermal power system |
| 07/13/2011 | CN102121420A Temperature activated valves for gas turbines |
| 07/12/2011 | US7975489 Catalyst module overheating detection and methods of response |
| 07/12/2011 | US7975465 Hybrid engine accessory power system |
| 07/12/2011 | CA2676831C Oil scavenge system having churning damper for gas turbine engines |
| 07/12/2011 | CA2660078C Internal fuel manifold having temperature reduction feature |
| 07/12/2011 | CA2503358C Sensor malfunction detection system for gas-turbine engine |
| 07/12/2011 | CA2479276C Methods and apparatus for operating gas turbine engines |
| 07/12/2011 | CA2475140C Low pressure turbomachinery turbine |
| 07/12/2011 | CA2469847C Noise-reducing turbomachine nozzle |
| 07/12/2011 | CA2452229C Article including a substrate with a metallic coating and a protective coating thereon, and its preparation and use in component restoration |
| 07/07/2011 | WO2011082243A1 Gas turbine engine and frame |
| 07/07/2011 | WO2011080433A2 Guiding of a spark plug into a turbine engine combustion chamber |
| 07/07/2011 | WO2011079997A1 Turbine for converting energy and method for operating the same |
| 07/07/2011 | WO2010127986A3 A flow control arrangement |
| 07/07/2011 | US20110162387 Turbine cooling system |
| 07/07/2011 | US20110162380 Method to increase net plant output of a derated igcc plant |
| 07/07/2011 | US20110162378 Tunable transition piece aft frame |
| 07/07/2011 | US20110162377 Turbomachine nozzle |
| 07/07/2011 | US20110162376 Gasification system and method using fuel injectors |
| 07/07/2011 | US20110162375 Secondary Combustion Fuel Supply Systems |
| 07/07/2011 | US20110162374 Articles having damping coatings thereon |
| 07/07/2011 | US20110162373 Fuel nozzle for a turbine engine with a passive purge air passageway |
| 07/07/2011 | US20110162372 Integral flange connection fuel nozzle body for gas turbine |
| 07/07/2011 | US20110162371 Fuel Nozzle with Integrated Passages and Method of Operation |
| 07/07/2011 | US20110162370 FUEL SYSTEM ACOUSTIC FEATURE TO MITIGATE COMBUSTION DYNAMICS FOR MULTI-NOZZLE DRY LOW Nox COMBUSTION SYSTEM AND METHOD |
| 07/07/2011 | US20110162340 Method for making a nacelle de-icing element |
| 07/07/2011 | US20110162339 Flow distribution of gas turbine exhaust using walls shaped to facilitate improved gas flow |
| 07/07/2011 | DE102010061637A1 Abstimmbarer Übergangsstück-Hinterrahmen A tunable transition piece rear frame |
| 07/07/2011 | DE102010061626A1 Brennstoffzuführsysteme für Sekundärverbrennung Fuel supply systems for secondary combustion |
| 07/07/2011 | DE102010037859A1 Einspritzsystem für heizwertarmen Brennstoff Injection system for low calorific fuel |
| 07/07/2011 | DE102009053000A1 Fan support disk for jet engine, has fan disk, nose cone which is formed of two annular elements arranged at angle to each other at transition, radial outer fan support and radial inner fastening section for fan disk |
| 07/07/2011 | DE102009040228A1 Verfahren zum Betrieb einer Mikrogasturbinenanordnung, sowie Mikrogasturbinenanordnung zur energetischen Biomasserverwertung Method for operating a micro gas turbine arrangement, as well as micro gas turbine arrangement for energy Biomasserverwertung |
| 07/07/2011 | CA2783721A1 Guiding of a spark plug into a turbine engine combustion chamber |
| 07/06/2011 | EP2341231A2 Frequency-tunable bracketless fluid manifold |
| 07/06/2011 | EP2341230A2 Fuel metering system electrically servoed metering pump |
| 07/06/2011 | EP2341217A1 Turbine for converting energy and method for operating the same |
| 07/06/2011 | CN201891507U Gas turbine support component and gas turbine generator set provided with same |
| 07/06/2011 | CN201891506U Container-type generator set of gas turbine |
| 07/06/2011 | CN1971011B Methods and apparatus for cooling combustion turbine engine components |
| 07/06/2011 | CN1788143B System and devices for collecting and treating waste water from engine washing |
| 07/06/2011 | CN1683772B Turbine shroud |
| 07/06/2011 | CN102119280A Thrust bearing lubrication nozzle |
| 07/06/2011 | CN102119268A Transition with a linear flow path with exhaust mouths for use in a gas turbine engine |
| 07/06/2011 | CN102116201A Disc-type rod fastening rotor structure for heavy-duty gas turbine |
| 07/06/2011 | CN102116200A Air intake filter system |
| 07/06/2011 | CN102116199A Anti-icing system using radiant infrared energy from turbine exhaust flues |
| 07/06/2011 | CN101680059B Ni-based single crystal superalloy and turbine vane using the same |
| 07/06/2011 | CN101374722B Dual flow turbine engine equipped with a precooler |
| 07/05/2011 | US7973421 Jet engine comprising an integrated electric motor/generator unit |
| 07/05/2011 | US7971423 Gas turbine engine comprising a starter in the auxiliary gear box |
| 07/05/2011 | CA2615296C Turbine spring clip seal |
| 06/30/2011 | WO2011077801A1 Multistage radial turbine |
| 06/30/2011 | WO2011076973A1 Arrangement in a gas turbine process |
| 06/30/2011 | US20110155508 On-demand lubrication system for improved flow management and containment |
| 06/30/2011 | US20110154831 Aircraft engine assembly comprising a turbojet engine with reinforcing structures connecting the fan casing to the central casing |
| 06/30/2011 | US20110154829 Burner, combustor and remodeling method for burner |
| 06/30/2011 | US20110154824 Frequency-tunable bracketless fluid manifold |
| 06/30/2011 | CA2725932A1 Methods for inhibiting corrosion of high strength steel turbine components |
| 06/30/2011 | CA2725891A1 Turbomachine nacelle and anti-icing system and method therefor |
| 06/30/2011 | CA2725856A1 Frequency-tunable bracketless fluid manifold |
| 06/29/2011 | EP2339147A2 Fuel supply control system for an aircraft engine |
| 06/29/2011 | EP2339146A1 Coupling system for a star gear train in a gas turbine engine |
| 06/29/2011 | EP2339145A2 Method of starting a turbomachine |
| 06/29/2011 | EP2339144A2 Heat exchanger mounting assembly in a gas turbine |
| 06/29/2011 | EP2339128A2 Method for starting a turbomachine |
| 06/29/2011 | EP2339123A1 Inner side of the annular bypass duct of a turbojet engine and method for assembling such an annular duct |
| 06/29/2011 | EP2337940A1 Thermal management system |
| 06/29/2011 | EP2337931A1 Method and system for lubricating a turbine engine |
| 06/29/2011 | EP2337929A1 Ventilation of a high-pressure turbine in a turbomachine |
| 06/29/2011 | EP1499800B1 Fuel premixing module for gas turbine engine combustor |
| 06/29/2011 | EP1287247B1 Method and system for generating power |
| 06/29/2011 | CN201884129U Nuclear engine |
| 06/29/2011 | CN201884128U Hydrogen-mixed gas fuel power machine |
| 06/29/2011 | CN201884127U Vortex gas-steam turbine |
| 06/29/2011 | CN102112704A Gas turbine and operating method therefor |
| 06/29/2011 | CN102112703A Gas turbine facility |
| 06/29/2011 | CN102112372A Method for making deicing system on nacelle panel |
| 06/29/2011 | CN102108900A Method of mounting heat exchanger in gas turbine engine assembly |
| 06/28/2011 | US7967559 Stator-rotor assembly having surface feature for enhanced containment of gas flow and related processes |
| 06/28/2011 | US7967551 Suction filter, turbocompressor, and method for compact assembling of the same |
| 06/28/2011 | US7966832 Combustor |
| 06/28/2011 | US7966818 Gas turbine combustion chamber with fuel injection over an entire combustion chamber annulus |
| 06/28/2011 | US7966807 Vapor cooled static turbine hardware |
| 06/28/2011 | US7966804 Method and apparatus for testing gas turbine engines |
| 06/23/2011 | WO2011075013A1 Arrangement and method for closed flow cooling of a gas turbine engine component |
| 06/23/2011 | WO2011074048A1 Gas turbine combined cycle power plant and method |
| 06/23/2011 | WO2011072756A1 Air intake for a plant |