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)
08/2014
08/28/2014DE102009010110B4 Erosionsschutz-Beschichtungssystem für Gasturbinenbauteile Erosion-resistant coating system for gas turbine components
08/27/2014EP2770183A1 Gas turbine variable focus laser ignition
08/27/2014EP2770182A1 Method for adjusting a natural gas temperature for a fuel supply line of a gas turbine engine
08/27/2014EP2768600A2 Filter systems for air intakes of aircraft engines and related methods
08/26/2014US8818657 Continuously variable transmission and shift control method
08/26/2014US8815371 Structure and method for forming detailed channels for thin walled components using thermal spraying
08/26/2014US8814562 Igniter/thruster with catalytic decomposition chamber
08/26/2014US8814512 Fan disk apparatus and method
08/26/2014US8814494 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
08/26/2014US8813506 Method for quickly connecting a steam generator
08/26/2014US8813505 Method for conditioning a power supply for starting a jet engine
08/26/2014US8813504 Assembly procedure for the adjustable pin-valve, fuel shut-off
08/26/2014US8813502 Cooling structure of gas turbine combustor
08/26/2014US8813501 Combustor assemblies for use in turbine engines and methods of assembling same
08/26/2014US8813473 Steam injected gas turbine engine
08/26/2014US8813471 System for fuel gas moisturization and heating
08/26/2014US8813470 Method for operating a fuel supply for a heat engine
08/26/2014US8813469 Planetary gear system arrangement with auxiliary oil system
08/26/2014CA2843425A1 Laser-ignition combustor for gas turbine engine
08/26/2014CA2619315C Acoustic splitter for turbojet fan case
08/26/2014CA2582629C Apparatus to inject a mixture of air and fuel, combustion chamber and turbine engine equipped with such an apparatus
08/26/2014CA2565743C Methods and apparatus for operating gas turbine engines
08/25/2014CA2843288A1 Engine architecture using electric machine
08/25/2014CA2841755A1 Method for adjusting a natural gas temperature for a fuel supply line of a gas turbine engine
08/21/2014WO2014127298A1 Turbo recharger
08/21/2014WO2014126961A1 Cooling manifold for turbine section
08/21/2014WO2014126899A1 Exhaust liner flange cooling
08/21/2014WO2014126788A1 Cooling hole for a gas turbine engine component
08/21/2014WO2014126708A1 Stress mitigation feature for composite airfoil leading edge
08/21/2014WO2014126704A1 Fan blade including external cavities
08/21/2014WO2014126696A1 Gas turbine engine geared architecture
08/21/2014WO2014126641A1 Compliant heat shield liner hanger assembly for gas turbine engines
08/21/2014WO2014126619A1 Combustor liners with u-shaped cooling channels
08/21/2014WO2014126565A1 Gas turbine engine component having surface indicator
08/21/2014WO2014124784A1 Through flow ventilation system for a power generation turbine package
08/21/2014WO2014105237A3 Geared turbofan primary and secondary nozzle integration geometry
08/21/2014WO2014105236A3 Airfoil with variable trip strip height
08/21/2014WO2014099105A3 Blast shield for high pressure compressor
08/21/2014WO2014099084A3 Fan drive gear system flexible support features
08/21/2014WO2014099075A3 Gas turbine engine asymmetric fuel nozzle combustor
08/21/2014WO2014099074A3 Gas turbine engine combustor with integrated combustor vane
08/21/2014WO2014099071A3 Real time model based compressor control
08/21/2014WO2014092835A3 Power cable and connector arrangement for a gas turbine engine
08/21/2014WO2014092608A3 Gas collector for gas turbine engine
08/21/2014WO2014084949A3 Cmc blade attachment shim relief
08/21/2014WO2014074195A3 Turbine engine support assembly including self anti-rotating bushing
08/21/2014US20140234090 Rear nacelle assembly for a turbojet engine
08/21/2014US20140234079 Geared Architecture for High Speed and Small Volume Fan Drive Turbine
08/21/2014US20140234078 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
08/21/2014US20140233769 Diaphragm arrangement for generating sound
08/21/2014US20140230452 Planetary gear system arrangement with auxiliary oil system
08/21/2014US20140230449 Valve control device, gas turbine, and valve control method
08/21/2014US20140230446 Reducing Oxygen in a Gas Turbine Exhaust
08/21/2014US20140230441 Heat shield manifold system for a midframe case of a gas turbine engine
08/21/2014US20140230403 Gas turbine engine shaft bearing configuration
08/21/2014US20140230402 Turbine conduit purge systems
08/21/2014US20140230400 Heat retention and distribution system for gas turbine engines
08/21/2014DE10231827B4 Verfahren zum Betrieb einer Gasturbine sowie Gasturbine zur Durchführung des Verfahrens A method of operating a gas turbine and gas turbine for carrying out the method
08/21/2014DE102014202401A1 Lager mit einem vorbelastungselement und verfahren zum betreiben des lagers Bearings with a unbiassed element and process for operating the camp
08/21/2014DE102014101147A1 System und Verfahren zur Reduktion des Gegendrucks in einem Gasturbinensystem System and method for reducing the back pressure in a gas turbine system
08/21/2014DE102013202841A1 Abgasturbolader Exhaust gas turbocharger
08/21/2014DE102013202616A1 Vorrichtung zum Reinigen der Core Engine eines Strahltriebwerks Device for cleaning the core engine of a jet engine
08/21/2014DE102013202520A1 Gasturbine Gas turbine
08/21/2014DE102013002605A1 Turbolader und Axiallagerscheibe für einen Turbolader Turbocharger and axial bearing for a turbocharger
08/21/2014CA2843285A1 Liquid cooling system with thermal valve defector
08/20/2014EP2767705A1 System for in-flight restarting of a multi-shaft turboprop engine
08/20/2014EP2767699A1 Gas turbine with fuel composition control
08/20/2014EP2767698A1 Ceramic matrix composite member and method for producing same
08/20/2014EP2767697A1 Gas turbine with fuel composition control
08/20/2014EP2767677A1 Fan containment system, corresponding fan assembly and gas turbine engine
08/20/2014EP2767676A1 Fan containment system, corresponding fan assembly and gas turbine engine
08/20/2014EP2767675A1 Through flow ventilation system for a power generation turbine package
08/19/2014US8807916 Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
08/19/2014US8806874 Axial turbine and power plant
08/19/2014US8806873 Method for operating a gas turbine plant
08/19/2014US8806872 Procedure for igniting a turbine engine combustion chamber
08/19/2014CA2650537C Turbine generator
08/19/2014CA2620806C Oil-based de-icing system for the nose cone of an aircraft turbine engine
08/19/2014CA2619142C Gas turbine engine with a gearbox-mounted starter
08/19/2014CA2578565C Method and apparatus for gas turbine engines
08/14/2014WO2014123857A1 Multi-circuit lubrication system for a turbine engine
08/14/2014WO2014123850A1 Gas turbine engine component with upstream-directed cooling film holes
08/14/2014WO2014123841A1 Removable film for airfoil surfaces
08/14/2014WO2014123838A1 Gas turbine engine with thermoplastic for smoothing aerodynamic surfaces
08/14/2014WO2014123772A1 Hybrid duplex ball bearing assembly
08/14/2014WO2014123740A1 Oil control module
08/14/2014WO2014123704A1 Oil baffles in carrier for a fan drive gear system
08/14/2014WO2014123685A1 Hybrid spinner support
08/14/2014WO2014092833A3 Gas turbine engine fan blade airfoil profile
08/14/2014WO2014088672A3 Mid-turbine frame heat shield
08/14/2014US20140227084 Compound star gear system with rolling element bearings
08/14/2014US20140227080 Seal support of titanium aluminide for a turbomachine
08/14/2014US20140225334 Combustor seal structure and a combustor seal
08/14/2014US20140223920 Consumable assembly mistake proofing tool for a gas turbine engine
08/14/2014US20140223917 Oil and fuel circuits in a turbine engine
08/14/2014US20140223913 Forged fuel injector stem
08/14/2014US20140223885 Turbo screen
08/14/2014DE102013211042B3 Flugtriebwerk-Gasturbine Aircraft engine gas turbine
08/14/2014DE102013020945A1 Verfahren zum Montieren eines Abgasturboladers A method of assembling an exhaust gas turbocharger
08/14/2014DE102005017148B4 Drehdichtungsanordnung für Kühlkreisläufe von Turbinenschaufeln Rotary seal assembly for cooling circuits of turbine blades
1 ... 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 ... 309