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)
03/2007
03/27/2007CA2204693C Microwave air-path clearance sensor
03/26/2007CA2552214A1 Blades for a gas turbine engine with integrated sealing plate and method
03/22/2007WO2007032738A1 System and method for augmenting power output from a gas turbine engine
03/22/2007WO2007032311A1 Blade tip clearance control structure of gas turbine
03/22/2007US20070063098 Passive cooling system for auxiliary power unit installation
03/22/2007US20070062202 Cooled support boss for a combustor in a gas turbine engine
03/22/2007US20070062201 Methods and apparatus for injecting cleaning fluids into combustors
03/22/2007US20070062200 Method of operating a thermal power plant, preferably a gas turbine power plant
03/22/2007US20070062196 Method and apparatus to detect onset of combustor hardware damage
03/22/2007CA2621958A1 Gas turbine engine combustion systems
03/21/2007EP1764495A2 Method and apparatus for housing gas turbine engines
03/21/2007EP1764484A2 Turbine cooling air sealing with associated turbine engine and method for reengineering a gas turbine engine
03/21/2007EP1646814B1 Slide ring and slide-ring seal assembly for jet engines
03/21/2007EP1411136B1 METHOD OF PREPARING A Ni-BASE SINTERED ALLOY
03/21/2007EP1269047B1 Improved brush-seal designs for turbines and similar rotary apparatus
03/21/2007CN1932343A Fluid static-pressure type fingertip sealing structure
03/21/2007CN1932263A Counterflow film cooled wall
03/20/2007US7192462 usable in existing aircraft without substantial modifications; seal permits relative movement between the duct and the assembly in any direction while maintaining a seal between the duct and the assembly
03/20/2007US7192243 Gas turbine engine blade containment assembly
03/20/2007US7191736 Low emission energy source
03/20/2007US7191588 Combustor controller
03/19/2007CA2558921A1 Methods and apparatus for housing gas turbine engines
03/15/2007WO2007028693A1 Cooling a gas turbine group provided with a second combustion chamber
03/15/2007WO2007028689A1 Apparatus for mixing gas streams
03/15/2007US20070059160 Engine, vehicle provided with such an engine, and a connecting element between a first and a second element of an engine
03/15/2007US20070056292 Auxiliary power unit case flange to cone bolt adapter
03/15/2007DE102005034180A1 Swirl rectifier for gas turbine, has secondary air pipe with clip fastener at inner and outer end sections at rotor disk, where fastener has flange and slots that arranged at pipe circumference and spring ring engaged in groove and recess
03/14/2007EP1762714A2 Heater for a gas turbine engine strut, electrical connector for this heater and corresponding manufacturing method
03/14/2007EP1761736A2 Heat exchanger with header tubes
03/14/2007EP1474595B1 Method for operating a gas turbine group
03/14/2007EP1071867B1 Method of generating power using an advanced thermochemical recuperation cycle
03/14/2007CN1304742C Method for utilizing gas reserves with low methane concentrations and high inert gas concentrations for fueling gas turbines
03/14/2007CN1304741C Method for utilizing gas reserves with low methane concentrations and high inert gas concentrations for fueling gas turbines
03/14/2007CN1304740C Supercharging system for gas turbines
03/14/2007CN1304734C Combined cycle power generation plant and method of operating such a plant
03/13/2007US7189064 Friction stir welded hollow airfoils and method therefor
03/13/2007US7188476 Gas turbine combustor and operating method thereof
03/13/2007US7188466 Passive, high-temperature amplifier for amplifying spark signals detected in igniter in gas turbine engine
03/13/2007US7188465 Method and apparatus for actuating fuel trim valves in a gas turbine
03/13/2007US7188464 Methods for operating gas turbine engines
03/13/2007CA2303371C Microchannel laminated mass exchanger and method of making
03/08/2007WO2007025381A1 Hydrostatic flow barrier for flexible fuel manifold
03/08/2007US20070054147 Welding material, gas turbine blade or nozzle and a method of repairing a gas turbine blade or nozzle
03/08/2007US20070051112 Turbo set with starting device
03/08/2007US20070051111 System and method for lightoff detection in turbine engines
03/08/2007US20070051110 Igniter tube and method of assembling same
03/08/2007US20070051108 Method for increasing the efficiency of a gas turbine system and gas turbine system suitable therefor
03/08/2007US20070051090 Control logic for fuel controls on APUs
03/08/2007DE102005040575A1 Tubular vortex in construction of tubes for cooling air guide in compressor of gas turbine, has secondary air tube with attachment shoulder which fits in radial inner side opposite to an attachment of compressor disc
03/08/2007DE10022967B4 Flüssigkeitsgekühlter Abgasturbolader Liquid-cooled exhaust gas turbocharger
03/08/2007CA2620415A1 Hydrostatic flow barrier for flexible fuel manifold
03/08/2007CA2558897A1 Redundant fuel manifold sealing arrangement
03/07/2007EP1760293A2 Hydrostatic flow barrier for flexible fuel manifold
03/07/2007EP1760292A2 Method and system for detecting gas turbine inlet filter rupture
03/07/2007EP1760291A2 Methods and apparatus for operating gas turbine engines
03/07/2007EP1759160A1 Heat exchange device and method
03/07/2007EP1759103A1 Method for operating a gas turbine compressor while cooling the compressor intake air by evaporation
03/07/2007EP1646560B1 Dual action inlet door and method for use thereof
03/07/2007EP1451450B1 Gas turbo group
03/07/2007CN1925902A A fluid separation device
03/07/2007CN1924321A Method and system for detecting gas turbine inlet filter rupture
03/07/2007CN1924320A Methods and apparatus for operating gas turbine engines
03/07/2007CA2554309A1 Deoxygenated fuel-cooler environmental control system pre-cooler for an aircraft
03/06/2007US7188019 Gas turbine control apparatus, gas turbine system and gas turbine control method
03/06/2007US7186084 Hot gas path component with mesh and dimpled cooling
03/06/2007US7186082 Cooled rotor blade and method for cooling a rotor blade
03/06/2007US7186078 Turbine shroud segment
03/06/2007US7186072 Recirculation structure for a turbocompressor
03/06/2007US7185663 Contacting the surfaces to be cleaned with a cleaning formulation comprising selected from the group consisting of graphite particles and molybdenum-based particles
03/06/2007US7185499 Device for passive control of the thermal expansion of the extension casing of a turbo-jet engine
03/06/2007US7185498 Modular gas turbine
03/06/2007US7185496 Synchronizing stationary clutch of compression braking with a two spool gas turbine engine
03/06/2007US7185483 Methods and apparatus for exchanging heat
03/01/2007WO2007023734A1 Seal structure of gas turbine combustor
03/01/2007WO2007023702A1 Damper element of bearing, method of manufacturing damper element, bearing, and gas turbine engine
03/01/2007WO2007023326A1 Cogeneration plant
03/01/2007WO2007002599A3 Reformer and reforming process for production of hydrogen from hydrocarbon fuel
03/01/2007US20070049454 Gas turbine gearbox
03/01/2007US20070044872 Precipitation-strengthened nickel-iron-chromium alloy and process therefor
03/01/2007US20070044478 Combustion engine
03/01/2007US20070044477 Fuel nozzle for gas turbine engines
03/01/2007US20070044476 Trapped vortex cavity afterburner
03/01/2007US20070044449 Improved Plasma Torch for Ignition, Flameholding and Enhancement of Combustion in High Speed Flows
03/01/2007DE19738671B4 Dichtungsanordnung Seal assembly
03/01/2007CA2557066A1 Methods and apparatus for operating gas turbine engines
03/01/2007CA2557047A1 Fuel nozzle for gas turbine engines
02/2007
02/28/2007EP1757777A1 Method to assemble a turbomachine
02/28/2007EP1756408A1 Reversible gas turbine gear box
02/28/2007EP1756407A1 Engine, vehicle provided with such an engine, and a connecting element between a first and a second element of an engine
02/28/2007EP1756399A1 System and devices for collecting and treating waste water from engine washing
02/28/2007EP1755952A1 System for washing an aero gas turbine engine
02/28/2007EP1755830A2 Seal removal tool for a seal having a grooved inner peripheral surface
02/28/2007EP1755788A1 Air/oil separation system and method
02/28/2007EP1499800A4 Fuel premixing module for gas turbine engine combustor
02/28/2007CN1302198C Stationary blade in gas turbine and gas turbine comprising the same
02/28/2007CN1302156C Method for producing mono-crystalline structures
02/28/2007CA2557944A1 Turbine engine combustion chamber
02/28/2007CA2551584A1 Dirt separator for gas turbine air supply
02/27/2007US7182576 Hot gas path component with mesh and impingement cooling
02/27/2007US7182519 Methods and apparatus for assembling a bearing assembly