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)
09/2006
09/13/2006EP1700008A2 Common radial plane motor cooling
09/13/2006EP1699698A1 Ram air channel for the supply of ambient air in an aircraft
09/13/2006EP1699697A2 Air guiding flap of an aircraft comprising control of the pressure forces impinging thereon, process for adjusting the position of an air guiding flap and ram air system including such an air guiding flap
09/13/2006EP1407194B1 A method of combustor cycle airflow adjustment
09/13/2006EP1402161B1 Power generator with low co2 emissions and associated method
09/13/2006EP1348071B1 Installation for the generation of energy
09/13/2006EP1257680B1 Iron base high temperature alloy
09/13/2006CN1833099A Water treatment and pressurization system for the adiabatic cooling of comburent air
09/13/2006CN1274943C Heat-barrier coating series
09/12/2006US7107169 Device for estimating the mass flow of fuel
09/12/2006US7104751 Hot gas path assembly
09/12/2006US7104750 Fogging device for gas turbines
09/12/2006US7104749 Intake silencer for gas turbines
09/12/2006US7104072 Combined power main engine start system
09/12/2006US7104071 Method for operating a gas turbine group
09/12/2006US7104070 Liquid fuel nozzle apparatus with passive water injection purge
09/12/2006US7104067 Combustor liner with inverted turbulators
09/12/2006US7104065 Damping arrangement for reducing combustion-chamber pulsation in a gas turbine system
09/12/2006CA2404453C Shaft seal structure and turbine
09/07/2006US20060196483 Fuel vaporization systems for vaporizing liquid fuel
09/07/2006US20060196192 Turbine engine and a method of operating a turbine engine
09/07/2006US20060196191 Gas turbine engine
09/06/2006EP1698774A2 A turbine engine and a method of operating a turbine engine
09/06/2006EP1698763A1 Gas turbine combined plant
09/06/2006EP1698762A2 Sealing of an aircraft engine accessory lubrication system
09/06/2006EP1697687A1 Method for determining fluctuating fuel properties during the operation of a power plant
09/06/2006EP1697623A1 Gas turbine, in particular aircraft engine and method for generating electrical energy in a gas turbine
09/06/2006CN1273724C Method and device for adjusting cooling blast supply system of turbine
09/06/2006CN1273723C Gate gurgle plug
09/06/2006CN1273240C Device and method for casting a workpiece and workpiece
09/05/2006US7101173 Plug sealing device that is not welded to the chamber wall
09/05/2006US7101154 Turbomachine blade, in particular a fan blade, and its method of manufacture
09/05/2006US7100359 Gas turbine installation
09/05/2006US7100358 Turbine exhaust case and method of making
09/05/2006US7100356 Heat recovery apparatus with aerodynamic diffusers
09/02/2006CA2534383A1 Low leakage finger seal
08/2006
08/31/2006WO2006091379A2 Gas turbine fuel preparation and introduction method
08/31/2006WO2006090466A1 Fuel injection valve, combustor using the fuel injection valve, and fuel injection method for the fuel injection valve
08/31/2006US20060194526 Apparatus for smoothing the surface of a gas turbine blade
08/31/2006US20060191910 Apparatus and methods for repairing tenons on turbine buckets
08/31/2006US20060191268 Method and apparatus for cooling gas turbine fuel nozzles
08/30/2006EP1696135A1 Intercooled turbocompressor
08/30/2006EP1694944A1 Gas turbine, particularly an aircraft engine
08/30/2006EP1611337A4 Anti-detonation fuel delivery system
08/30/2006EP1590072A4 Evaporative duplex counterheat exchanger
08/30/2006EP1285161A4 Recuperator for use with turbine/turbo-alternator
08/30/2006CN1826456A Turbine component, gas turbine engine, method of manufacture turbine component, surface processing method, blade component, metal component and steam turbine engine
08/30/2006CN1826431A Method for repairing and manufacture machine part and manufacture method for forming restored machine part
08/30/2006CN1272525C Turbine installation
08/29/2006US7097783 Method for inspecting a titanium-based component
08/29/2006US7097425 Microcircuit cooling for a turbine airfoil
08/29/2006US7097424 Micro-circuit platform
08/29/2006US7097418 Double impingement vane platform cooling
08/29/2006US7097415 Low-pressure turbine of a turbomachine
08/29/2006US7097413 Bearing support
08/29/2006US7097412 Turbine engine bearing support
08/29/2006US7096673 Blade tip clearance control
08/29/2006US7096671 Catalytic combustion system and method
08/29/2006US7096670 Method for igniting the combustion chamber of a gas turbine unit and an ignition device for carrying out the method
08/29/2006US7096658 Centrifugal pump fuel system and method for gas turbine engine
08/29/2006CA2445409C Method of repairing a turbine blade tip
08/24/2006WO2006087803A1 Method for controlling calorific value of gas and apparatus for controlling calorific value of gas
08/24/2006WO2006087377A1 Aircraft engine fuel supply
08/24/2006US20060188379 Apparatus and method of balancing a shaft
08/24/2006US20060185334 Suction filter, turbo compressor, and method of packaging the compressor
08/24/2006DE112004001703T5 Wärmetauscher mit geformten Scheiben Heat exchanger with shaped discs
08/24/2006DE102005007940A1 Foreign body e.g. stone, trapping device for use in turbo-prop driving mechanism, is fixed in inlet region of turbo-prop engine and traps foreign body sucked along with air when body hits device at specific velocity
08/24/2006DE102005006415A1 Gasturbinentriebwerk A gas turbine engine
08/24/2006CA2597938A1 Aircraft engine fuel supply
08/23/2006EP1692420A1 Air turbine starter having a low differential check valve
08/23/2006EP1692380A1 Hybrid vane island diffuser
08/23/2006EP1399659B1 Method and installation for energy production by means of a gas turbine associated with an air separation unit
08/23/2006EP1366271B1 Method and apparatus for cooling gas turbine engine blade tips
08/23/2006EP1348067B1 Metallic honeycomb cellular seal-structure for a turbomachine
08/23/2006CN1821445A Diffusion barrier for assemblies with metallic and silicon containing components and method therefor
08/23/2006CN1271179C Nickel compound used as vanadium corrosion inhibitor and burning method using it
08/22/2006US7094475 MCrAlY-coating
08/22/2006US7094444 Method for repairing coated components using NiAl bond coats
08/22/2006US7094033 Methods and apparatus for assembling gas turbine engines
08/22/2006US7094027 Row of long and short chord length and high and low temperature capability turbine airfoils
08/22/2006US7094024 Performance and durability improvement in compressor structure design
08/22/2006US7093996 Methods and apparatus for mounting a gas turbine engine
08/22/2006US7093835 Floating brush seal assembly
08/22/2006US7093450 Method for operating a compressor
08/22/2006US7093444 Simultaneous combustion with premixed and non-premixed fuels and fuel injector for such combustion
08/22/2006US7093437 Extended operability aircraft fuel delivery system
08/22/2006US7093423 Methods and apparatus for operating gas turbine engines
08/22/2006US7093422 Detecting spark in igniter of gas turbine engine by detecting signals in grounded RF shielding
08/22/2006US7093421 Spark igniter for gas turbine engine
08/22/2006US7093420 Flow divider and ecology valve
08/22/2006US7093419 Methods and apparatus for operating gas turbine engine combustors
08/22/2006US7093418 Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump
08/22/2006CA2533956A1 Trip manifold
08/22/2006CA2310110C Retaining arrangement for a bearing, in particular for a high pressure compressor shaft
08/17/2006WO2006085920A2 Pneumatic valve control using downstream pressure feedback and an air turbine starter incorporating the same
08/17/2006WO2006084809A1 Method for activating a pressure storage system, and a pressure storage system
08/17/2006WO2006084438A1 Method for machining an integrally bladed rotor
08/17/2006WO2006084437A1 Gas-turbine plant
08/17/2006US20060182624 Sealing arrangement, in particular for the blade segments of gas turbines
08/17/2006US20060179847 Ejector for cooling air supply pressure optimization