| 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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| 06/20/2012 | EP2464830A1 Turbo engine having steam tapping |
| 06/20/2012 | CN202280517U 供油装置 Oil installations |
| 06/20/2012 | CN102505993A Novel pulse jet engine |
| 06/20/2012 | CN102505992A Out-of-operation oil seal test system of engine and control method thereof |
| 06/20/2012 | CN102505991A Power generation device for condensed steam type double-working-medium gas turbine circulation system |
| 06/20/2012 | CN102505990A Power generation method of condensing double-working medium gas turbine circulation system |
| 06/20/2012 | CN101490390B Turbine engine for aircraft |
| 06/19/2012 | US8204631 Method and device for increasing the operational flexibility of a current-generating system, in particular a gas turbine or steam turbine |
| 06/19/2012 | US8201414 Assistance device for transient acceleration and deceleration phases |
| 06/19/2012 | US8201389 Oil distributing unit |
| 06/19/2012 | CA2668750C Film cooling structure |
| 06/19/2012 | CA2630721C Gas turbine engine premix injectors |
| 06/19/2012 | CA2606975C Combustor heat shield |
| 06/19/2012 | CA2492166C Turbojet engine comprising an ancillaries connecting arm and the ancillaries connecting arm |
| 06/17/2012 | CA2761315A1 Aerodynamically enhanced fuel nozzle |
| 06/17/2012 | CA2760118A1 Cooling flowpath dirt deflector in fuel nozzle |
| 06/17/2012 | CA2760046A1 Improved fuel atomization dual orifice fuel nozzle |
| 06/17/2012 | CA2760035A1 Low-ductility turbine shroud flowpath and mounting arrangement therefor |
| 06/14/2012 | WO2012057994A3 Gas turbine combustor with mounting for helmholtz resonators |
| 06/14/2012 | US20120145254 Air inlet for aircraft propulsion unit having a structure resistant to excess pressure and a process for repairing an air inlet of an aircraft propulsion unit |
| 06/14/2012 | US20120144843 Gas turbine engine and cooling system |
| 06/14/2012 | US20120144841 Core diffuser for deoiler/breather |
| 06/14/2012 | US20120144839 Method for starting a combined cycle power plant |
| 06/14/2012 | US20120144838 Combined cycle power augmentation by efficient utilization of atomizing air energy |
| 06/14/2012 | US20120144835 Combustion chamber |
| 06/14/2012 | DE102011102599A1 Verfahren zum Betrieb einer Kleingasturbinenanordnung, sowie Kleingasturbinenanordnung selbst Method for operating a small gas turbine arrangement, as well as small gas turbine assembly itself |
| 06/14/2012 | DE102010063071A1 Kühlvorrichtung für ein Strahltriebwerk A cooling apparatus for a jet engine |
| 06/14/2012 | DE102010062968A1 Radial compressor for exhaust gas turbocharger for fuel cell system of combustion engine in motor car, has axial spacer attached to intake guide such that spacer measures distance between intake guide and bearing housing |
| 06/14/2012 | DE102010061186A1 Zwangdurchlaufdampferzeuger mit Wandheizfläche und Verfahren zu dessen Betrieb Forced once-through steam generator with Wandheizfläche and method for its operation |
| 06/13/2012 | EP2463507A1 Igniter with integral pressure sensing line |
| 06/13/2012 | EP1825117B1 Turbine engine with differential gear driven fan and compressor |
| 06/13/2012 | CN202273751U Internal combustion engine provided with cylinder cover and turbine |
| 06/13/2012 | CN102498274A Mounting/dismounting jig for combustor tail pipe and tail pipe installation method |
| 06/13/2012 | CN102493874A Gas turbine package with fire protection, thermal insulation, ventilation and sound insulation functions |
| 06/13/2012 | CN102493873A Small-sized fuel adjuster of turbojet engine |
| 06/13/2012 | CN102493872A Method for fixing thermal insulation bag |
| 06/13/2012 | CN101981382B Gas turbine and method of forming insertion hole for combustor of gas turbine |
| 06/13/2012 | CN101201016B Fuel compression system with internal reheat for dew point suppression |
| 06/12/2012 | US8196385 Turbomachine control system |
| 06/07/2012 | WO2012073542A1 Electric power generation plant |
| 06/07/2012 | WO2012072659A1 Gas turbine assembly and method therefor |
| 06/07/2012 | WO2012072589A1 Method for stripping the polyurethane coating from a composite-material nose cone of a jet engine by using a gas laser |
| 06/07/2012 | WO2012072457A1 An air intake system for an air vehicle |
| 06/07/2012 | WO2012072352A1 Method for operating a gas turbine in the case of load shedding, a device for controlling the operation of a gas turbine and a power plant |
| 06/07/2012 | WO2009126721A3 Repair of fuel nozzle component |
| 06/07/2012 | US20120137705 Shroud supporting structure for gas turbine engine |
| 06/07/2012 | US20120137703 Method for operating an air-staged diffusion nozzle |
| 06/07/2012 | US20120137701 Method and device for converting thermal energy from biomass into mechanical work |
| 06/07/2012 | US20120137699 Method and device for purging a gas turbine liquid fuel injection system |
| 06/07/2012 | US20120137696 Air-staged diffusion nozzle |
| 06/07/2012 | US20120137695 Fuel nozzle with gas only insert |
| 06/07/2012 | US20120137694 Burner and gas turbine combustor |
| 06/07/2012 | US20120137693 Power plant |
| 06/07/2012 | US20120137691 Gas turbine assembly and method therefor |
| 06/07/2012 | US20120137690 Wide frequency response tunable resonator |
| 06/07/2012 | US20120137651 Gas turbine system |
| 06/07/2012 | US20120137650 Fluid impingement arrangement |
| 06/07/2012 | CA2820122A1 An air intake system for an air vehicle |
| 06/06/2012 | EP2461004A1 Advanced optics and optical access for laser ignition systems for combustion engines |
| 06/06/2012 | EP2461003A2 Fluid impingement arrangement |
| 06/06/2012 | EP2460729A1 An air intake system for an air vehicle |
| 06/06/2012 | EP2459933A2 Method and assembly for supplying fuel to a combustion chamber of a gas turbine plant |
| 06/06/2012 | EP2459859A1 Flow rate measuring device and method |
| 06/06/2012 | EP2254747B1 Method for joining cellular acoustic panels |
| 06/06/2012 | DE112009003818T5 System zum Halten und Warten eines Gasturbinenmotors System for holding and maintaining a gas turbine engine |
| 06/06/2012 | DE112009003817T5 Gasturbinenmotor und System zum Warten eines Gasturbinenmotors The gas turbine engine and system for maintaining a gas turbine engine |
| 06/06/2012 | DE102011056058A1 Verfahren zum Betreiben einer luftgestuften Diffusionsdüse Method of operating a stepped diffusion nozzle air |
| 06/06/2012 | DE102010053170A1 Verfahren zur Herstellung einer Kantenschutzbeschichtung für Rotorblätter einer Windenergieanlage und entsprechende Kantenschutzbeschichtung A method for producing a protective coating edges for rotor blades of a wind turbine and the corresponding edge protection coating |
| 06/06/2012 | DE102010053057A1 Aufladeeinrichtung für eine Verbrennungskraftmaschine Charging for an internal combustion engine |
| 06/06/2012 | DE102010052892A1 Lageranordnung für eine Welle eines Turbinenrades Bearing arrangement for a shaft of a turbine wheel |
| 06/06/2012 | CN101228069B Propulsion unit for aircraft and aircraft comprising at least one such propulsion unit |
| 06/06/2012 | CN101113689B Heat transfer system and method for turbine engine using heat pipes |
| 06/05/2012 | US8191686 Device and method of standby lubrication for an engine |
| 06/05/2012 | US8191373 Interlocking retention strip |
| 06/05/2012 | CA2552118C Low smoke and emissions fuel nozzle |
| 06/03/2012 | CA2760454A1 Gas turbine rotor containment |
| 05/31/2012 | WO2012071271A1 Systems and methods for air intake filter assemblies |
| 05/31/2012 | WO2012069773A1 Device for uncoupling a bearing carrier |
| 05/31/2012 | WO2012069745A1 Monitoring of a filter of the fuel-supply system of an aircraft engine |
| 05/31/2012 | US20120134779 Gas turbine of the axial flow type |
| 05/31/2012 | US20120131929 Flexible seal for gas turbine engine system |
| 05/31/2012 | US20120131928 Flexible seal for gas turbine engine system |
| 05/31/2012 | US20120131927 Advanced Optics and Optical Access for Laser Ignition for Gas Turbines Including Aircraft Engines |
| 05/31/2012 | US20120131926 Advanced laser ignition systems for gas turbines including aircraft engines |
| 05/31/2012 | US20120131900 Inlet particle separator system |
| 05/31/2012 | US20120131898 Integrated solar-gas turbine cogeneration plant |
| 05/31/2012 | US20120131897 Carbon Dioxide Compression Systems |
| 05/31/2012 | DE102011055830A1 Spülsysteme für Rotationsmaschinen und Verfahren für deren Einbau Flushing systems for rotary machinery and methods for their installation |
| 05/31/2012 | DE102011055692A1 Textildichtung für Turbomaschinen Textile gasket for turbomachinery |
| 05/31/2012 | DE102010062125A1 Verfahren zum Abtragen der Polyurethanbeschichtung von einem aus Verbundwerkstoff bestehenden Nasenkonus eines Strahltriebwerks A method for removing the plastic coating from a composite material consisting of nose cone of a jet engine |
| 05/31/2012 | CA2816508A1 Monitoring of a filter of the fuel-supply system of an aircraft engine |
| 05/30/2012 | EP2458180A1 Method for operating a gas turbine during load control, device for regulating the operation of a gas turbine and power plant |
| 05/30/2012 | EP2458177A1 Advanced laser ignition systems for gas turbines including aircraft engines |
| 05/30/2012 | EP2458176A2 Torque protection device for fire blanket and associated method |
| 05/30/2012 | EP2458175A2 Nose cone assembly |
| 05/30/2012 | EP2458161A1 Method for monitoring the oil system of a turbomachine |
| 05/30/2012 | EP2458158A1 Lubrication system for a turbomachine |
| 05/30/2012 | EP2458155A2 Gas turbine of the axial flow type |
| 05/30/2012 | EP2458146A1 Nose cone assembly |
| 05/30/2012 | EP2457632A1 Inlet particle separator system |