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)
11/2012
11/20/2012US8313593 Method of heat treating a Ni-based superalloy article and article made thereby
11/20/2012US8312729 Flow discouraging systems and gas turbine engines
11/20/2012US8312727 Vibration damper
11/20/2012US8312726 Gas turbine engine systems involving I-beam struts
11/20/2012US8312702 Oil recovery device
11/20/2012CA2729528C Mounting apparatus for low-ductility turbine shroud
11/15/2012WO2012153056A1 Turbojet engine cold stream flow path suspended from the exhaust case by radial crevice mounts and link rods
11/15/2012WO2012153040A1 Device for mounting a spark plug in a combustion engine of a gas turbine engine
11/15/2012WO2012097797A3 Heat exchanger and jet engine comprising same
11/15/2012US20120285175 Steam injected gas turbine engine
11/15/2012US20120285172 Premixed burner for a gas turbine combustor
11/15/2012US20120285137 Gas turbine engine and reheat system
11/15/2012DE102011101342A1 Fluggasturbinentriebwerk mit Ölkühler in der Triebwerksverkleidung Aircraft gas turbine engine with oil cooler in the engine cowling
11/15/2012DE102011101197A1 Aircraft gas turbine engine for use with auxiliary accessory drive, has engine shaft that is operatively connected to fluid pump, where fluid pump is connected with component through supply line and return line
11/15/2012CA2835275A1 Turbojet engine cold stream flow path suspended from the exhaust case by radial crevice mounts and link rods
11/14/2012EP2522833A2 Gas turbine engine with bleed air removal device
11/14/2012EP2522832A1 Axial Accessory Gearbox
11/14/2012EP2522831A2 Turbojet engine with oil cooler in the engine nacelle
11/14/2012EP2522830A1 Gas turbine
11/14/2012EP2522819A2 Fixing of a bearing axial disc in a turbo engine with magnetic bearings by means of a shrink disc connection
11/14/2012EP2522813A2 A controller, for use in a power plant having a liquid cooling system and an air cooling system
11/14/2012EP2521851A1 Contra-rotating propeller system for an aircraft turbine engine
11/14/2012EP2521848A2 Dual-pump supply system with by-pass-controlled flow regulator
11/14/2012CN202531290U Device for improving operational efficiency of natural gas pipeline gas turbine generating set
11/14/2012CN102782261A Turbomachine comprising a vertical shaft
11/14/2012CN102782257A Split-ring cooling structure and gas turbine
11/14/2012CN102777263A Fuel injection device of gas turbine
11/14/2012CN102777262A Method for preassembling heavy gas turbine in combination of vertical and horizontal assembling
11/14/2012CN102777261A Base plate used for inlet ventilation door and inlet ventilation door including it
11/14/2012CN102777252A High-pressure gas source compression system
11/14/2012CN102777215A Two-piece side seal assembly with covers
11/14/2012CN101622174B Acoustic lining for an aircraft, including a frost treatment system using the joule effect
11/14/2012CN101092907B Method and device for controlling cooling air temperature of gas turbine engine
11/13/2012US8307658 Flame holder for an afterburner duct of a jet engine with a spacer shoe, afterburner duct, and jet engine comprising an afterburner duct
11/13/2012US8307653 Combined catalysts for the combustion of fuel in gas turbines
11/13/2012US8307626 Auxiliary pump system for fan drive gear system
11/13/2012CA2673733C Dynamic impeller oil seal
11/13/2012CA2502791C High efficiency stator for the first phase of a gas turbine
11/13/2012CA2491260C Fire shield apparatus and method
11/13/2012CA2435342C Nickel-base alloy
11/08/2012WO2012150418A1 Exhaust case for a turbomachine with a flexible hub
11/08/2012US20120279231 Regenerative braking for gas turbine systems
11/08/2012US20120279228 Gas cooler and method for cooling gas
11/08/2012US20120279226 Hula seal with preferential cooling
11/08/2012US20120279223 Fuel Injector and Support Plate
11/08/2012US20120279195 Gas turbine igniter
11/07/2012EP2520863A1 Method for protecting a gas turbine engine against high dynamical process values and gas turbine engine for conducting said method
11/07/2012EP2520765A2 Two-piece side seal with covers
11/07/2012EP2520764A1 Blade with cooled root
11/07/2012EP2519727A2 Gas turbine engine and high speed rolling element bearing system
11/07/2012EP2519726A1 Gas turbine engine and frame
11/07/2012EP2519725A2 Gas turbine engine component construction
11/07/2012EP2519724A2 Gas turbine engine and cooling system
11/07/2012EP2519723A2 Gas turbine engine and heat exchange system
11/07/2012EP2519720A2 Integrated aero-engine flowpath structure
11/07/2012CN102767404A System and method of gas turbine for utilizing low-concentration gas
11/07/2012CN101802243B Heat-shielding coating material
11/06/2012US8303243 Turbine wash port for a gas turbine engine
11/03/2012CA2775251A1 Gas turbine engine module adapter to a carrier
11/01/2012WO2012148319A1 Method for adjusting a supersonic air inlet
11/01/2012WO2012148318A1 Adjustable supersonic air inlet
11/01/2012WO2012147802A1 Moulded article
11/01/2012WO2012147792A1 Power generation system and method for operating same
11/01/2012WO2012147723A1 Friction bonding method and bonding structure
11/01/2012WO2012147618A1 Carbon dioxide membrane separation system in coal gasification process, and coal gasification combined cycle power generation facility using same
11/01/2012WO2012146481A1 Casing cooling duct
11/01/2012WO2012145836A1 Apparatus and method for controlling a pressure gain combustor
11/01/2012US20120272662 Head part of an annular combustion chamber
11/01/2012US20120272661 Head part of an annular combustion chamber
11/01/2012US20120272660 Method and assembly for retrofitting a gas turbine combustor end cover
11/01/2012US20120272659 Reheat burner injection system
11/01/2012US20120272658 Thermal management system for gas turbine engine
11/01/2012CA2834285A1 Apparatus and method for controlling a pressure gain combustor
11/01/2012CA2834021A1 Friction joining method and joined structure
11/01/2012CA2832743A1 Molded part
10/2012
10/31/2012EP2518296A2 Fan drive gear system integrated carrier and torque frame
10/31/2012EP2518295A2 Integrated tailcone muffler assemblies and methods for using the same
10/31/2012EP2518282A2 External threaded mount attachment for fan case
10/31/2012EP2518280A1 Multistage radial turbine
10/31/2012EP2518279A2 Fan drive planetary gear system integrated carrier and torque frame
10/31/2012EP2518278A1 Turbine casing cooling channel with cooling fluid flowing upstream
10/31/2012EP2516810A1 Arrangement in a gas turbine process
10/31/2012EP2516806A2 Laval nozzle
10/31/2012DE10305467B4 Ausbauwerkzeug zum Extrahieren von spiralförmigen Gewindeeinsätzen sowie Anwendung des Ausbauwerkzeugs Removal tool for extracting helical thread inserts and use the removal tool
10/31/2012CN202510225U Micro gas turbine power generation system with wave rotor top regenerative cycle
10/31/2012CN102762844A Gas-guiding pipe comprising a noise-attenuating covering with variable porosity
10/31/2012CN102758691A Acoustic cleaning assembly for use in power generation systems and method of assembling same
10/31/2012CN102758667A Integrated tailcone muffler assemblies and methods
10/31/2012CN102758651A Component and methods of fabricating a coated component using multiple types of fillers
10/31/2012CN101267986B Aircraft engine assembly comprising an engine and a suspension pylon for such an engine
10/30/2012CA2500986C Blocking system for a main motor shaft with integrated bearing
10/30/2012CA2500959C Turbine casing with refractory clips obtained via mdp process
10/30/2012CA2500548C Turbine engine for example a gas turbine engine for an aircraft
10/28/2012CA2775491A1 Turbine engine and load reduction device thereof
10/27/2012CA2775145A1 Seal arrangement for segmented gas turbine engine components
10/26/2012WO2012145141A1 Multi-degree of freedom resonator array
10/26/2012WO2012145063A1 Closed gas generator and micro power unit including the same
10/26/2012WO2012144244A1 Vane member and rotary machine
10/26/2012WO2012144242A1 Turbine stator vane and gas turbine
10/26/2012WO2012087952A3 Method and tooling for partial disassembly of a bypass turbofan engine
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