| 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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| 12/29/2005 | US20050287298 Gas distributor for vapor coating method and container |
| 12/29/2005 | US20050287001 Shroud and vane segments having edge notches |
| 12/29/2005 | US20050286997 Airfoil insert with castellated end |
| 12/29/2005 | US20050286823 Methods and apparatus for assembling a bearing assembly |
| 12/29/2005 | US20050284690 High admittance acoustic liner |
| 12/29/2005 | US20050284442 Tornado torch igniter |
| 12/29/2005 | US20050284214 Electric engine start system with inspection mode |
| 12/29/2005 | US20050284150 Integrated gearless and nonlubricated auxiliary power unit |
| 12/29/2005 | US20050284149 Fuel control module |
| 12/29/2005 | US20050284148 Centrifugal pump fuel system and method for gas turbine engine |
| 12/29/2005 | DE102004027435A1 Exhaust driven turbocharger for IC engine has the air filter mounted directly onto the input of the compressor |
| 12/29/2005 | DE102004020753A1 Vorrichtung zur Ausnutzung der Abwärme von Verdichtern Apparatus for utilizing the waste heat of compressors |
| 12/29/2005 | CA2510670A1 Venting tube for low-pressure shaft of a turbine engine |
| 12/28/2005 | EP1610606A1 Hingeless flapper valve for flow control |
| 12/28/2005 | EP1609958A1 Gasturbine with compressor and recuperator |
| 12/28/2005 | EP1609957A2 Gas turbine engine start system with inspection mode |
| 12/28/2005 | EP1609955A1 Methods and apparatus for monitoring a bearing assembly |
| 12/28/2005 | EP1609950A2 Airfoil insert with castellated end |
| 12/28/2005 | EP1609948A2 Integrally bladed rotor airfoil fabrication and repair techniques |
| 12/28/2005 | CN1233925C Accessory multifunctional water jetting manifold and operation thereof |
| 12/27/2005 | US6979979 Gas turbine engine starter-generator exciter starting system and method including a capacitance circuit element |
| 12/27/2005 | US6978623 Gas turbine, driving method thereof and gas turbine combined electric power generation plant |
| 12/27/2005 | US6978622 Turbomachine |
| 12/27/2005 | US6978621 Turbo recuperator device |
| 12/27/2005 | US6978620 Start-up method for power plant |
| 12/27/2005 | US6978619 Premixed burner with profiled air mass stream, gas turbine and process for burning fuel in air |
| 12/27/2005 | US6978618 Bulkhead panel for use in a combustion chamber of a gas turbine engine |
| 12/27/2005 | US6978597 Flame detecting apparatus for gas turbine |
| 12/24/2005 | CA2831868A1 Methods and apparatus for assembling a bearing assembly |
| 12/24/2005 | CA2504173A1 Methods and apparatus for assembling a bearing assembly |
| 12/22/2005 | WO2005122389A1 Method for operation of a power station |
| 12/22/2005 | WO2005121684A1 Heat exchange device and method |
| 12/22/2005 | WO2005121509A1 System and devices for collecting and treating waste water from engine washing |
| 12/22/2005 | WO2005120953A1 System for washing an aero gas turbine engine |
| 12/22/2005 | US20050281663 Double impingement vane platform cooling |
| 12/22/2005 | US20050279959 Valve having pressure balancing piston and method involving same |
| 12/22/2005 | US20050279862 Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same |
| 12/22/2005 | US20050279481 Method and device for producing precision investment-cast ne metal alloy members and ne metal alloys for carrying out said method |
| 12/22/2005 | US20050279103 Hingeless flapper valve for flow control |
| 12/22/2005 | US20050279102 Modulated current gas turbine engine starting system |
| 12/22/2005 | US20050279101 Method of controlling the injection of liquid into an inflow duct of a prime mover or driven machine |
| 12/22/2005 | US20050279098 Method of power generation for airborne vehicles |
| 12/22/2005 | US20050279080 Heat exchanger with header tubes |
| 12/22/2005 | US20050279079 Method to transfer fuel in a fuel system for a gas turbine engine |
| 12/22/2005 | DE102005025823A1 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 |
| 12/22/2005 | DE102005024475A1 Verfahren zur Beschichtung von Gasturbinentriebwerkskomponenten A process for coating of gas turbine engine components |
| 12/22/2005 | DE102005023536A1 Vormischbrenner mit aufprallgekühltem Mittelkörper und Verfahren zum Kühlen des Mittelkörpers Premix burner with aufprallgekühltem central body and method of cooling of the centerbody |
| 12/22/2005 | CA2714809A1 System for washing an aero gas turbine engine |
| 12/22/2005 | CA2570243A1 System for washing an aero gas turbine engine |
| 12/21/2005 | EP1607603A2 Gas turbine engine inlet with noise reduction features |
| 12/21/2005 | EP1607583A1 Method and system for operating rotary machines |
| 12/21/2005 | EP1607581A1 Method and apparatus for fabricating a turbine nozzle assembly |
| 12/21/2005 | EP1607578A1 Cooled rotor blade |
| 12/21/2005 | EP1607379A1 Material for thermal barrier coating |
| 12/21/2005 | EP1388131A4 Improved fluid metering device |
| 12/21/2005 | EP1325276B1 Thermal shielding brick for lining a combustion chamber wall, combustion chamber and a gas turbine |
| 12/21/2005 | EP1309773B1 Turbine vane system |
| 12/21/2005 | CN1232761C Heat shielding device for hot fuel gas guide piece, particularly gas turbine structure piece |
| 12/21/2005 | CN1232720C Abradable seal |
| 12/20/2005 | US6977983 Nuclear power plant and a method of conditioning its power generation circuit |
| 12/20/2005 | US6976680 Shaft seal structure and turbine |
| 12/20/2005 | US6976655 Mounting arrangement |
| 12/20/2005 | US6976361 Ventilation channels in an afterburner chamber confluence sheet |
| 12/20/2005 | CA2357595C Combined cycle gas turbine system |
| 12/20/2005 | CA2244886C Capacitive gap measurement device |
| 12/18/2005 | CA2509863A1 Double impingement vane platform cooling |
| 12/17/2005 | CA2509798A1 Modulated current gas turbine engine starting system |
| 12/15/2005 | WO2005119032A1 Engine, vehicle provided with such an engine, and a connecting element between a first and a second element of an engine |
| 12/15/2005 | WO2005119031A1 Absorber silencer for compressors |
| 12/15/2005 | WO2005119029A1 Triple cycle power plant |
| 12/15/2005 | WO2005097412A3 Seal removal tool for a seal having a grooved inner peripheral surface |
| 12/15/2005 | US20050276692 Lightened interblade platform for a turbojet blade support disc |
| 12/15/2005 | US20050276691 Inter-vane platform with lateral deflection for a vane support of a turbine engine |
| 12/15/2005 | US20050276685 Pneumatic valve control using downstream pressure feedback and an air turbine starter incorporating the same |
| 12/15/2005 | US20050275224 Fluid actuated rotating device including a low power generator |
| 12/15/2005 | US20050274701 Homogeneous welding via pre-heating for high strength superalloy joining and material deposition |
| 12/15/2005 | US20050274489 Heat exchange device and method |
| 12/15/2005 | US20050274117 System & method for dumping surge flow into eductor primary nozzle for free turbine |
| 12/15/2005 | US20050274114 Ventilation channels in an afterburner chamber confluence sheet |
| 12/15/2005 | US20050274103 Gas turbine engine inlet with noise reduction features |
| 12/15/2005 | US20050274010 Method of replacing damaged aerofoil |
| 12/15/2005 | DE102004040183A1 Gas turbine with heat recovery system has two discharge pipes fro compressor |
| 12/14/2005 | EP1605208A1 Methods and apparatus for low emission gas turbine energy generation |
| 12/14/2005 | EP1605204A2 Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same |
| 12/14/2005 | EP1605152A1 Divergent flap for a gas turbine engine |
| 12/14/2005 | EP1605148A1 Method and system for the protection of fuel nozzles in a gas turbine engine |
| 12/14/2005 | EP1605138A2 Cooled rotor blade with leading edge impingement cooling |
| 12/14/2005 | EP1605137A1 Cooled rotor blade |
| 12/14/2005 | EP1605136A2 Cooled rotor blade |
| 12/14/2005 | EP1605074A1 Thermal recovery treatment for a service-degraded component of a gas turbine |
| 12/14/2005 | EP1605068A2 Homogeneous welding via pre-heating for high strength superalloy joining and material deposition |
| 12/14/2005 | EP1604770A2 Method of replacing damaged aerofoil |
| 12/14/2005 | EP1539573A4 Torsionally de-coupled engine mount system |
| 12/14/2005 | EP1114279B1 Dynamic control system and method for catalytic combustion process |
| 12/14/2005 | CN1707162A Gas turbine engine combustor mixer |
| 12/14/2005 | CN1707080A Methods and apparatus for low emission gas turbine energy generation |
| 12/14/2005 | CN1707077A Working method for turbocharger and turbocharger |
| 12/14/2005 | CN1707070A Turboreactor with fan mounted on a drive shaft supported by a first and a second bearing |
| 12/14/2005 | CA2763088A1 System and devices for collecting and treating waste water from engine washing |
| 12/13/2005 | US6973772 Gas turbine installation |