| 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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| 03/27/2013 | CN202832796U 燃料供应系统 The fuel supply system |
| 03/27/2013 | CN202832795U Sealing device and gas turbine with the same |
| 03/27/2013 | CN103003872A Acoustic panel for a turbojet engine nacelle, with in-built fasteners |
| 03/27/2013 | CN103003552A Fuel nozzle, gas turbine combustor equipped with same, and gas turbine equipped with this gas turbine combustor |
| 03/27/2013 | CN103003551A Power generation plant |
| 03/27/2013 | CN103003526A Internal cooling for a flow machine |
| 03/27/2013 | CN102997279A Fuel injector |
| 03/27/2013 | CN102996258A Non-continuous ring seal |
| 03/27/2013 | CN102996257A Integral combined cycle power generation system for direct combustion of pulverized coal |
| 03/27/2013 | CN102996256A Method and device for controlling temperature of gas turbine components |
| 03/27/2013 | CN102996255A Piping assembly and method for connecting inner and outer shell in turbine system |
| 03/27/2013 | CN102996254A Supersonic air intake duct and wall face determination method of supersonic air intake duct |
| 03/27/2013 | CN102996253A Supersonic air intake duct and wall face determination method of supersonic air intake duct |
| 03/27/2013 | CN102996250A Gas turbine inlet fogging system and method for inlet fogging control |
| 03/27/2013 | CN102996237A High-pressure working medium heat engine |
| 03/27/2013 | CN102052145B 内燃发动机 Internal combustion engine |
| 03/27/2013 | CN101832154B Method for cooling air film of turbine blade of aircraft engine |
| 03/27/2013 | CN101818689B Filter retention system |
| 03/27/2013 | CN101236041B 集成的设备冷却系统 The integrated cooling system equipment |
| 03/27/2013 | CN101230802B Variable coupling of high pressure rotor and low pressure rotor of turbofan engine |
| 03/27/2013 | CN101222172B Variable magnetic coupling of rotating machinery |
| 03/26/2013 | US8402771 Gas turbine engine |
| 03/26/2013 | US8402770 Turbine engine including an improved means for adjusting the flow rate of a cooling air flow sampled at the output of a high-pressure compressor using an annular air injection channel |
| 03/26/2013 | US8402769 Casing of a gas turbine engine having a radial spoke with a flow guiding element |
| 03/26/2013 | US8402767 Enhanced starting of turbine engines under various ambient conditions using oxidizer |
| 03/26/2013 | CA2525643C Transition piece for gas turbine |
| 03/21/2013 | WO2013039088A1 Gas turbine cooling system, and gas turbine cooling method |
| 03/21/2013 | WO2013038085A2 Method for monitoring the volumetric efficiency of an hp pump of a turbomachine hydraulic regulation system |
| 03/21/2013 | WO2012040195A3 System and method for high efficiency power generation using a nitrogen gas working fluid |
| 03/21/2013 | US20130073260 Method for anomaly detection/diagnosis, system for anomaly detection/diagnosis, and program for anomaly detection/diagnosis |
| 03/21/2013 | US20130071242 Thrust bearing system with inverted non-contacting dynamic seals for gas turbine engine |
| 03/21/2013 | US20130071231 Wall structure with noise damping insulation properties and gas turbine with such a wall structure |
| 03/21/2013 | US20130067932 Combustion sections of gas turbine engines with convection shield assemblies |
| 03/21/2013 | US20130067931 Gas turbine engine assemblies including strut-based vibration isolation mounts and methods for producing the same |
| 03/21/2013 | US20130067930 Axial bolting arrangement for mid turbine frame |
| 03/21/2013 | US20130067928 Method for operating a gas turbine plant and gas turbine plant for implementing the method |
| 03/21/2013 | US20130067926 Multiple Tube Premixing Device |
| 03/21/2013 | US20130067922 Ultrasonic Water Atomization System for Gas Turbine Inlet Cooling and Wet Compression |
| 03/21/2013 | US20130067920 Fuel injector and swirler assembly with lobed mixer |
| 03/21/2013 | US20130067919 Fuel supply device of gas turbine engine |
| 03/21/2013 | US20130067882 Bleed air duct joint insulation means |
| 03/21/2013 | DE202013100884U1 Flüssigkeitsgekühlte Turbine mit Lagergehäuse Liquid-cooled turbine with bearing housing |
| 03/21/2013 | DE102011082827A1 Luftturbinenanlage Air turbine installation |
| 03/21/2013 | CA2848466A1 Method for monitoring the volumetric efficiency of an hp pump of a turbomachine hydraulic regulation system |
| 03/21/2013 | CA2765334A1 Plug device for gas turbine engine shaft |
| 03/20/2013 | EP2570633A2 Thrust bearing system with inverted non-contacting dynamic seals for gas turbine engine |
| 03/20/2013 | EP2570631A2 Gas turbine inlet fogging system and method for inlet fogging control |
| 03/20/2013 | EP2570619A2 High temperature aluminum valve components |
| 03/20/2013 | CN202811083U 密封件 Seals |
| 03/20/2013 | CN202811082U Starting control device of engine |
| 03/20/2013 | CN202811081U Recuperative electric drive gas turbine with multiple gas compressors and main pipes |
| 03/20/2013 | CN202811077U Gas turbine system with inlet cooling and intercooling functions |
| 03/20/2013 | CN202811076U Inter-cooled regenerative header type gas turbine unit with split compressors |
| 03/20/2013 | CN202811075U Inter-cooled header type gas turbine unit with split compressors |
| 03/20/2013 | CN102985665A Low emission triple-cycle power generation systems and methods |
| 03/20/2013 | CN102979627A Stepped conical honeycomb seal carrier |
| 03/20/2013 | CN102979626A High pressure air starting device for aero-engine |
| 03/20/2013 | CN102979625A Structure for aviation gas turbine rotor supporting point ball bearing axial pre-load |
| 03/20/2013 | CN102979624A Control device for baffle door of air inlet channel of combustion engine |
| 03/20/2013 | CN102979623A Supersonic air inlet and method for determining wall thereof |
| 03/20/2013 | CN102230420B Low-temperature gas exhausting engine |
| 03/20/2013 | CN101779171B Plant state monitoring method and plant state monitoring device |
| 03/20/2013 | CN101235730B Gas turbine engine with a gearbox-mounted starter |
| 03/20/2013 | CA2790351A1 Monitoring overfilling in an aeroplane engine lubrication system |
| 03/19/2013 | USRE44079 Method of chilling inlet air for gas turbines |
| 03/19/2013 | US8398016 Air intake arrangement for an aircraft |
| 03/19/2013 | US8397516 Apparatus and method for removing heat from a gas turbine |
| 03/19/2013 | US8397515 Fuel nozzle flashback detection |
| 03/19/2013 | US8397483 Inlet system for an EGR system |
| 03/19/2013 | US8397482 Dry 3-way catalytic reduction of gas turbine NOx |
| 03/19/2013 | CA2505058C Process for closing a hole in a metal part by means of friction welding, use of a metal bar and a bearing bracket to carry out the process |
| 03/14/2013 | WO2013036392A1 Fuel manifold cooling flow recirculation |
| 03/14/2013 | WO2013035391A1 Gas turbine |
| 03/14/2013 | WO2013034843A1 Turbo engine comprising a damping fluid film for damping a guide bearing of a shaft of the turbo engine and method of adjusting the thickness of such a damping fluid film |
| 03/14/2013 | WO2013034829A1 Oil and fuel circuits in a turbomachine and method for managing heat exchanges |
| 03/14/2013 | WO2013034704A1 Improved flame resistant shield |
| 03/14/2013 | US20130065077 Process for Applying a Heat Shielding Coating System on a Metallic Substrate |
| 03/14/2013 | US20130064657 Intermediate housing of a gas turbine having an outer bounding wall having a contour that changes in the circumferential direction upstream of a supporting rib to reduce secondary flow losses |
| 03/14/2013 | US20130061601 Control apparatus for angling guide vanes of a torque converter |
| 03/14/2013 | US20130061600 Method of controlling temperature of gas turbine components using a compressed moisurized coolant |
| 03/14/2013 | US20130061599 Fuel manifold cooling flow recirculation |
| 03/14/2013 | US20130061595 Speed Card-Controlled Override Fuel Pump Assist |
| 03/14/2013 | US20130061594 Turning guide for combustion fuel nozzle in gas turbine and method to turn fuel flow entering combustion chamber |
| 03/14/2013 | DE102012108281A1 Grenzschichtanblasen unter Verwendung von Dampfsperren-Leckstrom Grenzschichtanblasen using steam barrier leakage |
| 03/14/2013 | DE102012015659A1 Exhaust gas turbocharger for internal combustion engine of vehicle, has noise-reducing device that is bonded with wall of air duct or wall of air-conducting channel by bonding material |
| 03/14/2013 | DE102011082604A1 Arrangement for producing or processing through hole extending through thickness of wall of solid body, has contoured body, which is arranged in such way that body is hit directly by water jet |
| 03/14/2013 | DE102011082493A1 Sicherungssegment zur Schwingungsdämpfung von Turbinenlauf-schaufeln und Rotorvorrichtung Turbine blades backup segment for vibration damping and rotor assembly |
| 03/14/2013 | CA2846261A1 Fuel manifold cooling flow recirculation |
| 03/14/2013 | CA2845533A1 Turbo engine comprising a damping fluid film for damping a guide bearing of a shaft of the turbo engine and method of adjusting the thickness of such a damping fluid film |
| 03/13/2013 | EP2568218A2 Fuel gas pressure control system and method for reducing gas turbine fuel supply pressure requirements |
| 03/13/2013 | EP2568144A2 Wall structure with noise damping insulation properties and gas turbine with such a wall structure |
| 03/13/2013 | EP2568143A2 Piping assembly and method for connecting inner and outer shell in turbine system |
| 03/13/2013 | EP2568142A1 Biomass plant |
| 03/13/2013 | EP2568141A1 Method for accelerating the rotor of a stationary gas turbine to nominal speed |
| 03/13/2013 | EP2568124A1 Construction unit for an engine of a plane |
| 03/13/2013 | EP2568123A1 Apparatus and method for separating ice from fuel in a gas turbine engine |
| 03/13/2013 | EP2568122A2 Method and apparatus for extracting electrical power from a gas turbine engine |
| 03/13/2013 | EP2568116A2 An aerofoil assembly in a gas turbine |
| 03/13/2013 | EP2568115A1 Cooling system for gas turbine blades comprising a compressor positioned aft of the turbine stage in flow direction |
| 03/13/2013 | EP2567072A2 Brush ring seal |