Patents
Sitemap › F02 - Combustion engines; Hot-gas or combustion-product engine plants › F02C - Gas-turbine plants; Air intakes for jet-propulsion plants; Controlling fuel supply in air-breathing jet-propulsion plants › F02C 7 - Features, component parts, details or accessories, not provided for in, or of interest apart from, groups; Air intakes for jet-propulsion plants
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)
04/2014
04/29/2014US8707705 Impingement cooled transition piece aft frame
04/29/2014US8707703 Dual swirler
04/29/2014CA2714861C Gas turbine engine breather exhaust oil collector
04/24/2014WO2014062220A1 Structural guide vane circumferential load bearing shear pin
04/24/2014WO2014060860A1 Sealing system with air curtain for bearing
04/24/2014WO2014060656A1 Jet pump for depressurizing lubrication chambers of a turbomachine, having independent double injectors
04/24/2014WO2014035613A3 Attachment apparatus for ceramic matrix composite materials
04/24/2014WO2014028089A3 Geared architecture carrier torque frame assembly
04/24/2014WO2014025439A3 Floating segmented seal
04/24/2014WO2014011300A3 Dual spring bearing support housing
04/24/2014US20140112770 Turbojet engine cold stream flow path suspended from the exhaust case by radial crevice mounts and link rods
04/24/2014US20140112759 Gas turbine casing thermal control device
04/24/2014US20140109596 Arrangement for connecting a duct to an air-distribution casing
04/24/2014US20140109594 Deformable Mounting Assembly
04/24/2014US20140109593 Coil spring hanger for exhaust duct liner
04/24/2014US20140109592 Leaf spring hanger for exhaust duct liner
04/24/2014US20140109590 Gas turbine thermal control and related method
04/24/2014US20140109589 Gas turbine engine variable bleed valve for ice extraction
04/24/2014US20140109587 System and method for reducing modal coupling of combustion dynamics
04/24/2014US20140109586 Method for operating a gas turbine with sequential combustion and gas turbine for conducting said method
04/24/2014US20140109585 High Pressure Relief Valve Nozzle
04/24/2014US20140109584 Modulating electric liquid metering valve with flow sensing
04/24/2014US20140109582 Self-stabilized micromixer
04/24/2014US20140109580 Part load performance improvement using deformable bore plugs
04/24/2014US20140109577 Ducting arrangement for cooling a gas turbine structure
04/24/2014US20140109544 High Pressure Relief Valve Closure
04/24/2014CA2830683A1 Combustor transition
04/23/2014EP2722511A2 Turbine leak detection system
04/23/2014EP2722510A1 Gas turbine, and method for repairing gas turbine
04/23/2014EP2722508A1 Method for operating a gas turbine with sequential combustion and gas turbine for conducting said method
04/23/2014EP2722492A1 Method for operating a gas turbine with sequential combustion
04/23/2014EP2722415A1 Member covered with hard coating film
04/23/2014EP2721273A1 Combustion systems and combustion system components for rotary ramjet engines
04/23/2014EP2721272A1 Aircraft engine fuel system and method of operating the same
04/23/2014CN103748338A Split control unit
04/23/2014CN103748337A Adjustable supersonic air inlet
04/23/2014CN103742270A Purging pipeline monitoring method of combustor
04/23/2014CN103742269A Energy-saving system for using natural gas depressurization cold energy in fuel gas power plant
04/23/2014CN103742268A Impeller engine
04/23/2014CN102493873B Small-sized fuel adjuster of turbojet engine
04/23/2014CN101965443B Gas turbine and method of opening chamber of gas turbine
04/23/2014CN101889133B Gas turbine controlling method, and gas turbine power generating apparatus
04/23/2014CA2830031A1 Burner for a can combustor
04/22/2014US8702373 Lubrication of journal bearing during clockwise and counter-clockwise rotation
04/22/2014US8701418 Late lean injection for fuel flexibility
04/22/2014US8701383 Late lean injection system configuration
04/22/2014US8701382 Late lean injection with expanded fuel flexibility
04/22/2014US8701379 Combined cycle integrated combustor and nozzle system
04/17/2014WO2014058718A1 Bi-directional compression fan rotor for a gas turbine engine
04/17/2014WO2014058712A1 Bleed air slot
04/17/2014WO2014058692A1 Improved v-panel filter
04/17/2014WO2014058541A1 Duplex bearing lubrication
04/17/2014WO2014058509A2 Casting cores and manufacture methods
04/17/2014WO2014058505A2 Threaded full ring inner air-seal
04/17/2014WO2014058493A2 Suction side turbine blade tip cooling
04/17/2014WO2014058483A2 Corrugated mid-turbine frame thermal radiation shield
04/17/2014WO2014058478A1 Geared low fan pressure ratio fan exit guide vane stagger angle
04/17/2014WO2014058466A1 Geared turbofan engine with optimized diffuser case flange location
04/17/2014WO2014058463A1 Geared turbofan engine with inter-shaft deflection feature
04/17/2014WO2014058455A1 Bearing support stiffness control
04/17/2014WO2014058453A1 Geared turbine engine with relatively lightweight propulsor module
04/17/2014WO2014025440A3 Turbine blade root with microcircuit cooling passages
04/17/2014WO2014025427A3 Turbomachine geared architecture support assembly
04/17/2014WO2014018137A3 Aircraft engine driveshaft vessel assembly and method of assembling the same
04/17/2014WO2014014536A3 Systems and methods for preventing fuel leakage in a gas turbine engine
04/17/2014WO2014006467A3 Tip fabrication for rotor blade or stator vane airfoil
04/17/2014US20140105737 Gas turbine engine comprising three rotary bodies
04/17/2014US20140102114 In-line removable heat shield for a turbomachine suspension yoke
04/17/2014US20140102113 Exhaust heat recovery for a gas turbine system
04/17/2014US20140102110 Mid-turbine frame with tensioned spokes
04/17/2014US20140102105 System and method for heating combustor fuel
04/17/2014US20140102071 System and method for heating fuel in a combined cycle gas turbine
04/17/2014DE102013111223A1 Kühlfilmlochplateau für Heißgaspfadkomponente Film cooling hole plateau for hot gas path component
04/17/2014DE102011004856B4 Gleitlager zur Verwendung in Turboladern von Verbrennungsmotoren Plain bearings for use in turbochargers of internal combustion engines
04/16/2014EP2719927A1 Oil scavenge arrangement
04/16/2014EP2719879A2 System and method for heating fuel in a combined cycle gas turbine
04/16/2014EP2719878A2 System and method for heating combustor fuel
04/16/2014EP2718554A1 Method for operating a static gas turbine, and intake duct for intake air of a gas turbine
04/16/2014EP2718546A1 Turbine engine comprising a floating bearing for guiding a shaft of the turbine engine
04/16/2014EP2718185A1 System and method for mounting an aircraft engine
04/16/2014CN203547925U Gas-steam combined cycle power plant
04/16/2014CN203547924U Combined type energy-saving gas turbine inlet air cooling system
04/16/2014CN203547923U Heavy-duty type gas turbine bearing stator with adjustable flow
04/16/2014CN203547922U Shunt ring, engine anti-icing device and turbofan engine
04/16/2014CN103732886A Member-assembling device for rotary machine
04/16/2014CN103727561A System and method for separating fluids
04/16/2014CN103726932A System and method for heating fuel in a combined cycle gas turbine
04/16/2014CN103726931A System and method for heating combustor fuel
04/16/2014CN102562313B Chemically recuperated cycle gas turbine
04/16/2014CN102365120B Filter cassette, filter arrangement, and gas turbine with such filter cassette
04/16/2014CN102132010B Fixed vane assembly for turbine engine having reduced weight, and turbine engine including at least one such fixed vane assembly
04/16/2014CN102124197B Inner wall for the nacelle of a turbine engine
04/16/2014CN101994571B System for conditioning the airflow entering turbomachine
04/16/2014CN101629520B Combustor transition piece aft end cooling and related method
04/16/2014CN101446211B Gas turbine fuel injector with insulating air shroud
04/15/2014US8695348 Combustor and gas turbine
04/15/2014CA2743593C Nacelle and method of assembling the same
04/15/2014CA2580476C Structure for separating the internal areas of a high pressure and a low pressure turbine
04/15/2014CA2566802C Methods and apparatus for injecting fluids into turbine engines
04/15/2014CA2531741C Methods and apparatus for operating gas turbine engines
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