Patents
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)
11/2007
11/28/2007EP1860302A1 Gas turbine engine starting method and control device
11/28/2007EP1860301A2 Micro-perforated acoustic liner
11/28/2007EP1860300A2 High humidity gas turbine equipment
11/28/2007EP1860284A1 Casings assembling
11/28/2007EP1860283A2 Fan casing for a gas turbine engine
11/28/2007EP1670564B1 Separator systems
11/28/2007CN101078372A Wet middle cooling-wet rear cooling-backheating cycle combustion turbine
11/28/2007CN101078371A Wet middle cooling-wet rear cooling-backheating-preheating cycle combustion turbine
11/28/2007CN101078370A Wet compression-rear surface cooling-regenerative cycle combustion turbine
11/28/2007CN101078369A Wet compression-regenerative cycle combustion turbine
11/28/2007CN101078368A Method for gas turbine operation during under-frequency operation through use of air extraction
11/28/2007CN100351507C Fuel metering device with compensation regulator valve in turbine engine
11/28/2007CN100351496C Continuous radial loader for steam turbine reaction blade and its method
11/27/2007US7300708 shape memory alloy to decrease the rate of wear/erosion of the blade due to contact of the blade with its surrounding shroud
11/27/2007US7299638 Combined heat and power system
11/27/2007US7299620 Tornado torch igniter
11/27/2007US7299619 Vaporization of liquefied natural gas for increased efficiency in power cycles
11/27/2007US7299618 Gas turbine combustion apparatus
11/22/2007US20070269608 Rotor repair method and rotor repair apparatus
11/22/2007DE102006023580A1 Schmiermittelsystem Lubrication system
11/22/2007DE102006023237A1 Gasturbine Gas turbine
11/22/2007DE102006022683A1 Flugtriebwerk-Baugruppe, nämlich Verdichter oder Turbine eines Flugtriebwerks, Flugtriebwerk-Bauteil sowie Verfahren zur Herstellung oder Instandsetzung eines Flugtriebwerk-Bauteils Aircraft engine assembly, namely the compressor or turbine aircraft engine, aircraft engine component and methods for making or repairing an aircraft engine-component
11/21/2007EP1857656A2 Multi-splice acoustic liner
11/21/2007EP1857655A2 A liner panel
11/21/2007EP1857638A2 Thermal management system for turbofan engines
11/21/2007EP1025053B1 Performance-based control system
11/21/2007CN200978722Y Support and clamping device for large diameter fuel main pipe
11/21/2007CN200978721Y R0110 heavy gas turbine five-stage gas-discharging system
11/21/2007CN101076659A Acoustic absorber for aircraft engines
11/21/2007CN100350134C Method and apparatus to facilitate sealing within turbines
11/21/2007CN100350132C 透平叶片 Turbine blades
11/21/2007CN100350075C High-temperature protection layer
11/20/2007US7297260 System and devices for collecting and treating waste water from engine washing
11/20/2007US7296415 Labyrinth seal device for gas turbine engine
11/20/2007US7296413 Power generating system and method
11/20/2007US7296412 Nitrogen purge for combustion turbine liquid fuel system
11/20/2007US7296398 Counter-rotating turbine engine and method of assembling same
11/20/2007CA2482388C Sealing arrangement for an axial turbine wheel
11/20/2007CA2477627C Electric thrust reverser actuation system
11/20/2007CA2301151C Turbocharger integrated bearing system
11/19/2007CA2588956A1 Accessory gear case in an aircraft engine such as a turbojet engine
11/15/2007WO2007128280A1 Gas turbine engine
11/15/2007WO2007128098A1 Gas turbine engine oil system operation
11/15/2007US20070261421 Packaged Chilling Systems For Building Air Conditioning And Process Cooling
11/15/2007US20070261411 Tailorable design configuration topologies for aircraft engine mid-turbine frames
11/15/2007US20070261408 Gas turbine having exhaust recirculation
11/15/2007DE102006021436A1 Gasturbinentriebwerk A gas turbine engine
11/14/2007EP1855054A2 Method for supplying fuel to a premix burner
11/14/2007EP1853805A1 Aircraft engine fuel supply
11/14/2007EP1853795A1 Method for manifacturing an integrally bladed rotor
11/14/2007CN200975284Y Air-intake heating apparatus of starters
11/14/2007CN101072935A Combined rankine and vapor compression cycles
11/14/2007CN100349319C Power generating system
11/13/2007US7294361 Method and device for gas phase diffusion coating of metal components
11/13/2007US7293415 Method of operating a gas turbine group
11/11/2007CA2584371A1 Electric power generation system and method
11/08/2007WO2007127329A2 Turbine generator
11/08/2007US20070258810 Wall Configuration of Axial-Flow Machine, and Gas Turbine Engine
11/08/2007US20070256426 Triggered pulsed ignition system and method
11/08/2007US20070256416 Combustor for Gas Turbine
11/08/2007DE3908166B4 Prallgekühltes Gebilde Impingement cooled structure
11/08/2007DE102007007090A1 Gas turbine has cooling air transfer system with several tubular nozzles which are independently arranged in a circle inside a chamber, encompass the rotor and can discharge cooling air
11/08/2007DE102006017377A1 Klappendichtung für eine Strömungsmaschine Flap seal for a turbomachine
11/08/2007CA2650537A1 Turbine generator
11/07/2007EP1852657A1 Fuel injection valve, combustor using the fuel injection valve, and fuel injection method for the fuel injection valve
11/07/2007EP1852590A2 A gas turbine engine
11/07/2007EP1852574A2 Method of operating a gas turbine engine oil system
11/07/2007EP1852346A1 Aeroengine mount
11/07/2007EP0919701B2 Sealing structure for joint surfaces of flanges of gas turbine
11/07/2007CN101069005A Gas turbine apparatus
11/07/2007CN101067381A Gas turbine has cooling air transfer system
11/07/2007CN100347426C Full steam-operation internal combustion engine
11/07/2007CN100347425C Electric power supply equipment
11/07/2007CN100347416C Steam and gas turbine installation
11/07/2007CN100347411C Gas-turbine engine turbon-nozzle arc section with single-branch open cavity hollow blade
11/06/2007US7291408 Thermal barrier coatings with low thermal conductivity
11/06/2007US7290982 Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle
11/06/2007US7290403 Intake of air into separation unit; extracting gas stream consisting of air gas, in particular oxygen or nitrogen; directing towards combustion chamber; controlling a parameter by acting on a compressor; assigning a variable set point value
11/06/2007US7290394 Fuel injector flexible feed with moveable nozzle tip
11/06/2007US7290385 Approach to extending life of gas turbine engine
11/06/2007CA2380914C Gas turbine combustor
11/05/2007CA2584628A1 Triggered pulsed ignition system and method
11/01/2007WO2007123612A1 Inlet distortion and recovery control system
11/01/2007WO2007122307A1 Air inlet lip for a pod with electric defrosting
11/01/2007WO2007121553A1 Fuel system of gas turbine engines
11/01/2007WO2007121551A1 Pre-heating of a liquid in an aircraft reservoir and associated apparatus
11/01/2007WO2007121550A1 Relighting a turbofan engine
11/01/2007US20070255459 Method and apparatus for operation of a power station
11/01/2007US20070251240 Forward sleeve retainer plate and method
11/01/2007CA2847641A1 Fuel system of gas turbine engines
11/01/2007CA2643465A1 Pre-heating of a liquid in an aircraft reservoir
11/01/2007CA2643463A1 Relighting a turbofan engine
11/01/2007CA2643392A1 Fuel system of gas turbine engines
11/01/2007CA2643023A1 Air inlet lip for a pod with electric defrosting
11/01/2007CA2585497A1 Methods and apparatus for assembling gas turbine engines
10/2007
10/31/2007EP1849987A2 Gas turbine engine with acoustic liners
10/31/2007EP1849975A2 Fuel System of Gas Turbine Engines
10/31/2007EP1849974A2 Turbine engine tailcone resonator
10/31/2007DE102007018420A1 System und Verfahren zur Konditionierung einer Gasturbinenzuluft System and method for conditioning a Gasturbinenzuluft
10/31/2007CN200968235Y Stamping type gas-turbine unit