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) |
---|
12/25/2013 | CN203362321U Film hole used for cooling of gas turbine engine |
12/25/2013 | CN103477054A Anti-fire seal assembly and nacelle comprising such a seal |
12/25/2013 | CN103477053A Solar collector including a solar turbine or a turbocompressor |
12/25/2013 | CN103477032A 燃气轮机 Gas turbine |
12/25/2013 | CN103471286A Multiple renewable energy complementary distributed energy system |
12/25/2013 | CN103470379A Combined type energy-saving gas turbine inlet air cooling system |
12/25/2013 | CN103470378A Method and device for improving oil-supplying reliability of lubricating-oil system of power generating set |
12/25/2013 | CN103470377A Transition piece for a gas turbomachine |
12/25/2013 | CN103470375A Cast superalloy pressure containment vessel |
12/25/2013 | CN102748135B Method for designing fixed-geometry two-dimensional mixed-compression type supersonic velocity air inlet channel |
12/25/2013 | CN102269059B Accessory case transmission device and aircraft engine comprising same |
12/25/2013 | CN102143889B Method for making acoustic panel for air intake lip of nacelle |
12/25/2013 | CN102143888B Method for making nacelle de-icing element |
12/25/2013 | CA2813972A1 Contamination resistant butterfly valve |
12/24/2013 | US8613199 Cooling fluid metering structure in a gas turbine engine |
12/24/2013 | DE102013210994A1 Turboladerverdichtergeräuschminderungssystem und -Verfahren Turbocharger compressor noise reduction system and method |
12/19/2013 | WO2013188723A1 Fluid conduit |
12/19/2013 | WO2013188722A1 High durability turbine exhaust case |
12/19/2013 | WO2013188325A1 Shaft alignment tools and methods |
12/19/2013 | WO2013188324A1 Shaft alignment tools and methods |
12/19/2013 | WO2013188115A1 Rotor assembly with interlocking tabs |
12/19/2013 | WO2013188074A1 Turbomachine flow control device |
12/19/2013 | WO2013188033A1 Gas turbine control systems and methods |
12/19/2013 | WO2013187961A1 Manifold for flow distribution |
12/19/2013 | WO2013187103A1 Blade root spring insertion tool and blade root spring insertion method |
12/19/2013 | WO2013165518A3 Gas turbine engine component with cusped, lobed cooling hole |
12/19/2013 | WO2013165517A3 Gas turbine engine component with diffusive cooling hole |
12/19/2013 | WO2013165512A3 Variable area turbine |
12/19/2013 | WO2013103469A3 Process of producing ceramic matrix composites and ceramic matrix composites formed thereby |
12/19/2013 | US20130336758 Variable blade outer air seal |
12/19/2013 | US20130336757 Active control of bucket cooling supply for turbine |
12/19/2013 | US20130333393 Gas turbine control systems and methods |
12/19/2013 | US20130333390 Cooling air inlet, engine bleed air system and method for operating a cooling air inlet |
12/19/2013 | US20130333389 Cross fire tube retention system for a gas turbine engine |
12/19/2013 | US20130333388 Combustor liner cooling assembly for a gas turbine system |
12/19/2013 | CA2875800A1 Fluid conduit |
12/18/2013 | EP2674593A2 Active control of bucket cooling supply for a turbine by means of an adjustable gas flow valve comprising a shape memory material |
12/18/2013 | EP2674590A1 Power plant with solar energy system and method for operating the power plant |
12/18/2013 | EP2673490A1 Radiation shield for a gas turbine combustor |
12/18/2013 | EP1384856B1 Endface gap sealing of steam turbine packing seal segments and retrofitting thereof |
12/18/2013 | EP1108857B2 Abradable seal |
12/18/2013 | CN203347963U Split fuel pump |
12/18/2013 | CN103459807A Generator apparatus for aircraft |
12/18/2013 | CN103459806A Aircraft engine |
12/18/2013 | CN103459805A Fuel circuit comprising means for controlling a pump |
12/18/2013 | CN103459804A Process for cooling the turbine stage and gas turbine having a cooled turbine stage |
12/18/2013 | CN103459781A 涡轮排气结构及燃气轮机 Structure and the turbine exhaust gas turbine |
12/18/2013 | CN103459778A Gas turbine comprising a heat shield and method of operation |
12/18/2013 | CN103459776A Vane member and rotary machine |
12/18/2013 | CN103459080A Hollow curved plate, method for manufacturing same, and burner for gas turbine |
12/18/2013 | CN103452838A Gear pump, pumping apparatus including the same, and aircraft fuel system including gear pump |
12/18/2013 | CN103452704A Miniature turbojet midair windmill ignition device |
12/18/2013 | CN103452672A Electrical unit for gas turbine and electrical equipment wiring method of electrical unit |
12/18/2013 | CN103452671A Gas turbine compressor inlet pressurization and flow control system |
12/18/2013 | CN103452595A Novel air film hole with improved cooling efficiency |
12/18/2013 | CN102562314B Plasma catalysis based chemical heat extraction cycle gas turbine device |
12/18/2013 | CN102072022B Heat exchange matrix of double-wave primary surface recuperator for micro gas turbine |
12/18/2013 | CN102007282B Propulsion unit for aircraft and air intake structure for such unit |
12/18/2013 | CN101858254B Filter retention systems and devices |
12/18/2013 | CN101629518B Turbomachine filter system having drain with one-way valve |
12/18/2013 | CN101576009B Operation of dual gas turbine fuel system |
12/17/2013 | US8607577 Attaching ceramic matrix composite to high temperature gas turbine structure |
12/17/2013 | CA2576698C Radially compact bearing assembly between a turbine shaft and a turbine engine compressor shaft |
12/12/2013 | WO2013185044A1 Fan blade platform |
12/12/2013 | WO2013184619A1 Single turbine driving dual compressors |
12/12/2013 | WO2013184608A1 Vibration data collection and processing for a gas turbine engine |
12/12/2013 | WO2013184568A1 Compressor power and torque transmitting hub |
12/12/2013 | WO2013184504A1 Combustor liner with reduced cooling dilution openings |
12/12/2013 | WO2013184502A1 Combustor liner with improved film cooling |
12/12/2013 | WO2013184454A1 Seal land for static structure of a gas turbine engine |
12/12/2013 | WO2013184436A1 Insulated tubing |
12/12/2013 | WO2013184431A1 Manufacturing a family of airfoils |
12/12/2013 | WO2013184430A1 Turbine rotor cover plate lock |
12/12/2013 | WO2013184429A1 Front bearing support for a fan drive gear system |
12/12/2013 | WO2013184426A1 Nacelle bifurcation for gas turbine engine |
12/12/2013 | WO2013184400A1 Thermally insulative attachment |
12/12/2013 | WO2013184336A1 Active clearance control for gas turbine engine |
12/12/2013 | WO2013184330A1 Nacelle inner flow structure leading edge latching system |
12/12/2013 | WO2013184329A1 Compressor tip clearance management for a gas turbine engine |
12/12/2013 | WO2013184264A1 Integrated fuel pump and control |
12/12/2013 | WO2013184015A1 Installation for treating a fuel to increase its caloric power |
12/12/2013 | WO2013183618A1 Fuel injection device |
12/12/2013 | WO2013182797A1 Turbine engine comprising an upstream attachment means for a deoiling pipe |
12/12/2013 | WO2013182697A1 Modular gas turbine plant with a heavy duty gas turbine |
12/12/2013 | WO2013182655A1 Combination of two gas turbines to drive a load |
12/12/2013 | WO2013182492A1 High pressure ratio compressors with multiple intercooling and related methods |
12/12/2013 | WO2013130157A3 Adaptive eductor system |
12/12/2013 | US20130327061 Turbomachine bucket assembly and method of cooling a turbomachine bucket assembly |
12/12/2013 | US20130327059 Draining device |
12/12/2013 | US20130327058 Device for suspending a turbojet engine |
12/12/2013 | US20130327057 Combustor liner with improved film cooling |
12/12/2013 | US20130327056 Combustor liner with decreased liner cooling |
12/12/2013 | US20130327055 Transition piece for a gas turbomachine |
12/12/2013 | US20130327054 Hybrid slinger combustion system |
12/12/2013 | US20130327052 Exhaust system for gas turbines |
12/12/2013 | US20130327046 Combustor assembly having a fuel pre-mixer |
12/12/2013 | US20130327045 Gas turbine combustion chamber with fuel nozzle, burner with such a fuel nozzle and fuel nozzle |
12/12/2013 | US20130327044 Fuel metering valve fail-fixed and back-up control system |
12/12/2013 | US20130327012 Gas turbine anti-icing system |
12/12/2013 | US20130327011 Method And Apparatus For A Fuel Nozzle Assembly For Use With A Combustor |