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)
03/2014
03/13/2014WO2014039274A1 Threaded seal for a gas turbine engine
03/13/2014WO2014039256A1 Combustion turbine flashback sensing system employing fiber bragg grating sensors
03/13/2014WO2014039187A1 Turbine engine transmission gutter
03/13/2014WO2014037672A1 Device for sealing an opening of an enclosure wall for access to a rotary shaft
03/13/2014WO2014037650A1 Accessory drive gearbox for controlling the flaps of an aircraft
03/13/2014WO2014037649A1 Method and system for starting an aircraft turboengine
03/13/2014WO2014037547A2 Brush-type circular seal
03/13/2014WO2014011252A3 Geared architecture with speed change device for gas turbine engine
03/13/2014WO2014007891A3 Seal with non-metallic interface
03/13/2014WO2014007886A3 Turbomachine thermal management
03/13/2014WO2014007882A3 Thread load distribution
03/13/2014WO2013180897A3 Gas turbine engine compressor stator seal
03/13/2014US20140072457 Fuel metering system electrically servoed metering pump
03/13/2014US20140069738 Damping system for combustor
03/13/2014US20140069109 Electrical grounding for blades
03/13/2014US20140069107 Turboprop engine with compressor turbine shroud
03/13/2014US20140069106 Sliding u-joint hanger for gas turbine engine nozzle
03/13/2014US20140069103 Seal for use between injector and combustion chamber in gas turbine
03/13/2014US20140069102 Gas turbine engine fuel system metering valve
03/13/2014US20140069077 Electrical grounding for blade sheath
03/13/2014DE112012002692T5 Vorrichtung und Verfahren zur Reduzierung des Luftmassenflusses zur emissionsarmen Verbrennung über einen erweiterten Bereich in einwelligen Gasturbinen Apparatus and method for reducing the air mass flow to low-emission combustion over an extended range in single-shaft gas turbines
03/13/2014DE102013109552A1 System und Verfahren zur Versorgung einer Gasturbine mit Öl System and method to supply a gas turbine with oil
03/13/2014DE102013109205A1 Metallschaum zur Umfangsabstützung in Hochtemperatur/Vibrationsanwendungen Metal foam for circumferential support in high temperature / vibration applications
03/13/2014DE102013109204A1 Gasturbinen-Einlass-Nebelsystem mit elektrohydrodynamischer Zerstäubung (EHD) Gas turbine inlet-fog system with electrohydrodynamic atomization (EHD)
03/13/2014DE102013109203A1 Wirbelunterbrechende Dichtungszähne für eine Dichtungsanordnung Eddy Interrupting seal teeth for a seal assembly
03/13/2014DE102013109151A1 Schaufelanordnung für eine Turbomaschine Blade assembly for a turbomachine
03/12/2014EP2706197A2 Outer race locating washer
03/12/2014EP2705219A1 Turbine nozzle guide vane assembly in a turbomachine
03/12/2014DE202013010992U1 Beipass für Turbo Bypass for Turbo
03/12/2014CN203476511U Heat insulating hood
03/12/2014CN203476510U Connecting structure for power turbine disc of combustion gas turbine
03/12/2014CN203476509U Ejector of combustion gas turbine
03/12/2014CN203476508U Anti-icing screw-plug assembly structure
03/12/2014CN103635958A Acoustic panel and associated assembly method
03/12/2014CN103628986A Turbomachine windmill bypass valve
03/12/2014CN103628985A System for heating natural gas by using waste heat of waste heat boiler in gas turbine power plant
03/12/2014CN103628984A Loop heating system for gas turbine anti-freezing device and working method of loop heating system
03/12/2014CN103628983A Radiation light path dustproof device of turbine blade of gas turbine
03/12/2014CN102378855B Rotating inlet cowl for turbine engine, including eccentric front end
03/12/2014CN102325980B Gas turbine engine and system for servicing gas turbine engine
03/12/2014CN102099556B Air intake structure for turbojet engine nacelle with pneumatic de-icing
03/12/2014CN101878359B Heat shield and turbocharger having heat shield
03/12/2014CN101793409B Systems and methods for mitigating flashback condition in premixed combustor
03/12/2014CN101660450B Filtration system for gas turbines
03/12/2014CA2826419A1 Mounting device and method of assembling the same
03/12/2014CA2826353A1 Method for operating a thermal power plant
03/11/2014US8668441 Deformable structural framework for a turbofan nacelle
03/11/2014US8667949 Engine driven power generator apparatus
03/11/2014US8667803 Turbine starter valve
03/11/2014US8667773 Counter-rotating turbomachinery
03/11/2014US8667772 Clutched turbine wheels
03/11/2014CA2752424C Cmc turbine stator blade
03/10/2014CA2826099A1 Acoustic damper arrangement for a combustor
03/06/2014WO2014036554A1 Assembly for mounting a turbine engine to a pylon
03/06/2014WO2014036258A1 Cycle turbine engine power system
03/06/2014WO2014036256A1 Cycle piston engine power system
03/06/2014WO2014035848A1 Gas turbine engine airfoil cooling circuit arrangement
03/06/2014WO2014035621A1 Blade outer air seal
03/06/2014WO2014035581A1 Face seal retaining assembly for gas turbine engine
03/06/2014WO2014034643A1 Gas turbine device
03/06/2014WO2014033972A1 Gas turbine
03/06/2014WO2014033416A1 Drive gearbox on a turbomachine, consisting of a drive train with gear lines extending into non-parallel planes
03/06/2014WO2014033400A1 Drainage method and purge collector of a carburation system of a helicopter
03/06/2014WO2014033220A1 Cooling method for operating a gas turbine
03/06/2014WO2014011279A3 Turbine engine exhaust nozzle flap
03/06/2014WO2014009839A3 A turbine cooling system
03/06/2014WO2014007889A3 Improved cooling for a turbine airfoil trailing edge
03/06/2014WO2013180778A3 Seal assembly
03/06/2014US20140065433 Coatings for dissipating vibration-induced stresses in components and components provided therewith
03/06/2014US20140064928 Engine casing of an aircraft gas turbine having sound-absorbing elements in the fan inflow region
03/06/2014US20140064908 Valve for controlling flow of a turbomachine fluid
03/06/2014US20140062034 Gas path leakage seal for a turbine
03/06/2014US20140062029 Threaded seal for a gas turbine engine
03/06/2014US20140062028 Gas seal for aerospace engines and the like
03/06/2014US20140060658 Multiple gas turbine forwarding system
03/06/2014US20140060083 Gas turbine engine aft bearing arrangement
03/06/2014US20140060080 Gas turbine engine aft bearing arrangement
03/06/2014US20140060079 Aeroengine arrangement
03/06/2014US20140060078 Combustor
03/06/2014US20140060077 Combustor
03/06/2014US20140060076 Antirotated piston rack
03/06/2014US20140060074 Systems and methods for driving an oil cooling fan of a gas turbine engine
03/06/2014US20140060072 Method of starting a gas turbine system
03/06/2014US20140060070 Method and apparatus for increasing combustion efficiency and reducing particulate matter emissions in jet engines
03/06/2014US20140060069 Combustor including combustion nozzle and an associated method thereof
03/06/2014US20140060063 Systems and Methods For Suppressing Combustion Driven Pressure Fluctuations With a Premix Combustor Having Multiple Premix Times
03/06/2014US20140060062 Method, apparatus and system for controlling swirl of exhaust in a gas turbine
03/06/2014US20140060061 Systems and Methods for Removing Impurities from Heavy Fuel Oil
03/06/2014US20140060058 Gas turbine system having an evaporative cooler
03/06/2014US20140060057 Method and apparatus for heating liquid fuel supplied to a gas turbine combustor
03/06/2014US20140060000 Gas turbine engine with radial diffuser and shortened mid section
03/06/2014DE102013109556A1 Einlass-Luft-Kühlsystem mit Feuchtigkeitssteuerung und Energierückgewinnung Inlet air cooling system with humidity control and energy recovery
03/06/2014DE102013109147A1 Leistungserhöhungssystem und Netzfrequenzsteuerung Performance enhancement system and frequency control
03/06/2014DE102013108862A1 Dichtungsdesign und aktive Spaltsteuerungsstrategie für Turbomaschinen Seal design and active clearance control strategy for turbomachinery
03/06/2014DE102012017491A1 Turbinenschaufel einer Gasturbine mit Drallerzeugungselement Turbine blade of a gas turbine with swirl generating element
03/05/2014EP2703624A1 Adjustable supersonic air inlet
03/05/2014EP2703294A2 Combined hub, counterweight and crank arm with single piece steel body
03/05/2014EP2703148A1 Moulded article
03/05/2014EP2703111A1 Friction bonding method and bonding structure
03/05/2014EP2702258A1 Apparatus and method for controlling a pressure gain combustor
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