| 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) |
|---|
| 03/25/2010 | US20100071377 Combustor Apparatus for Use in a Gas Turbine Engine |
| 03/25/2010 | US20100071376 Combustor Assembly in a Gas Turbine Engine |
| 03/25/2010 | US20100071375 Apparatus for observing combustion conditions in a gas turbine engine |
| 03/25/2010 | US20100071374 Spiral Cooled Fuel Nozzle |
| 03/25/2010 | US20100071369 Processing biomass |
| 03/25/2010 | US20100071343 Compact cyclone combustion torch igniter |
| 03/25/2010 | DE102009044026A1 Brennstoffdüsenspitzen-Baugruppe Fuel nozzle tip assembly |
| 03/25/2010 | DE102008048126A1 Exhaust gas turbocharger i.e. supercharger, for use in vehicle, has rotor provided with compressor part and turbine part, where rotor is radially and/or axially mounted only at axial ends in pivotable manner |
| 03/25/2010 | CA2738093A1 Method and system for lubricating a turbine engine |
| 03/24/2010 | EP2166213A2 Air filter mounting system and method for fabricating the same |
| 03/24/2010 | EP2166196A2 Continuous supply oil tank for zero and negative G operation |
| 03/24/2010 | CN201428518Y Gas turbine self-cleaning air inlet screen monitor |
| 03/24/2010 | CN201428517Y Auxiliary power device |
| 03/24/2010 | CN101681616A Acoustic septum cap honeycomb |
| 03/24/2010 | CN101680662A Gum-like substance monitoring apparatus and detecting method and gas turbine equipment |
| 03/24/2010 | CN101680306A Blade structure for turbine |
| 03/24/2010 | CN101680097A Heat resistant component |
| 03/24/2010 | CN101680059A Ni-based single crystal superalloy and turbine vane using the same |
| 03/24/2010 | CN101676537A System and method for cooling using system exhaust |
| 03/24/2010 | CN101676536A Elastic mounting flange used for combustion gas turbine engine |
| 03/24/2010 | CN101676535A Fuel nozzle tip assembly |
| 03/23/2010 | US7681403 Forward sleeve retainer plate and method |
| 03/23/2010 | US7681402 Aeroengine oil tank fire protection system |
| 03/23/2010 | CA2451318C Method and apparatus to decrease gas turbine engine combustor emissions |
| 03/23/2010 | CA2426351C System for closing the opening of a pipe, particularly the opening of an air inlet into a ramjet combustion chamber |
| 03/23/2010 | CA2403720C Safety device for a washing system for liquid fuel burners in gas turbines |
| 03/23/2010 | CA2364181C Two-level pressurization valve controlled by a fuel meter |
| 03/23/2010 | CA2363632C Brush seal and method of making same |
| 03/23/2010 | CA2313260C Acoustic liner and method of making an acoustic liner |
| 03/18/2010 | WO2010030448A1 Intershaft seal system |
| 03/18/2010 | US20100068051 Integrated inlet fan case |
| 03/18/2010 | US20100068043 Cooling structure for outer surface of a gas turbine case |
| 03/18/2010 | US20100068036 Auxiliary power unit inlet duct with acoustic silencing |
| 03/18/2010 | US20100068035 Apparatus and method for cooling a turbine |
| 03/18/2010 | US20100068033 Turbine Airfoil Cooling System with Curved Diffusion Film Cooling Hole |
| 03/18/2010 | US20100068032 Turbine Airfoil Cooling System with Diffusion Film Cooling Hole |
| 03/18/2010 | US20100064694 Combustor, method of supplying fuel to same, and method of modifying same |
| 03/18/2010 | US20100064690 Fuel nozzle tip assembly |
| 03/18/2010 | US20100064658 Modular fuel supply device for a gas turbine |
| 03/18/2010 | US20100064655 System and method for managing turbine exhaust gas temperature |
| 03/18/2010 | DE102008046946A1 Axial bearing for shaft of exhaust turbocharger, has disk-shaped bearing box, which has bearing element, where bearing box is made of inner bearing flange carrying bearing element |
| 03/17/2010 | EP2163749A1 Blast furnace gas burning facility and its operation method |
| 03/17/2010 | EP2163748A1 Integrated inlet fan case |
| 03/17/2010 | CN101675228A Gas turbine combustor |
| 03/17/2010 | CN101675227A Cooling structure for gas-turbine combustor |
| 03/17/2010 | CN101675226A Acoustic panel having a variable acoustic characteristic |
| 03/17/2010 | CN101675225A Gas turbine plant |
| 03/17/2010 | CN101672483A Gas turbine |
| 03/17/2010 | CN101672291A Gas turbine powered air compressor |
| 03/17/2010 | CN101672290A Novel air compressor |
| 03/16/2010 | US7677048 Turbine last stage blade with forced vortex driven cooling air |
| 03/16/2010 | US7677047 Inverted stiffened shell panel torque transmission for loaded struts and mid-turbine frames |
| 03/16/2010 | US7677046 Method for starting a pressure storage plant |
| 03/11/2010 | WO2010026305A1 Method for making an acoustic panel for the air intake lip of a nacelle |
| 03/11/2010 | WO2010026304A1 Method for making a nacelle de-icing element |
| 03/11/2010 | WO2010026182A1 Method for making a circular revolution thermomechanical part comprising a carrier substrate containing titanium coated with steel or a superalloy, and titanium fire-resistant compressor casing for a turbine engine obtained by said method |
| 03/11/2010 | WO2010026181A1 Method for making a circular revolution thermomechanical part comprising a carrier substrate containing titanium coated with steel or a superalloy, and titanium fire-resistant compressor casing for a turbine engine obtained by said method |
| 03/11/2010 | WO2010026180A1 Compressor casing resistant to titanium fire, high pressure compressor including such a casing, and aircraft engine including such a compressor |
| 03/11/2010 | WO2010026179A1 Method for making a circular revolution thermomechanical part including a carrier substrate containing titanium coated with steel or a superalloy, and titanium fire-resistant compressor casing for a turbine engine obtained by said method |
| 03/11/2010 | WO2010007220A3 Turbomachine structural casing |
| 03/11/2010 | US20100061839 Shaft coupling arrangement |
| 03/11/2010 | US20100061836 Process for producing a turbine blade or vane with an oxide on a metallic layer, use of such a turbine blade or vane, a turbine and a method for operating a turbine |
| 03/11/2010 | US20100058770 Method and System for Controlling Fuel to a Dual Stage Nozzle |
| 03/11/2010 | US20100058768 Axial diffusor for a turbine engine |
| 03/11/2010 | US20100058763 Segmented annular combustor |
| 03/11/2010 | US20100058761 Fuel gas conditioning system |
| 03/11/2010 | US20100058733 Ecology valve fuel return system for gas turbine engine |
| 03/11/2010 | US20100058730 Gas turbine power generation system and method of detecting calorific abnormality of the same |
| 03/11/2010 | US20100058729 Lubricant scavenge arrangement |
| 03/11/2010 | DE102009043865A1 Strömungssperre für das Gehäuse einer Turbomaschine Flow barrier for the casing of a turbomachine |
| 03/11/2010 | DE102009038707A1 Brennstoffverteilungsverteilersystem für Gasturbinenmotoren Fuel distribution manifold system for gas turbine engines |
| 03/11/2010 | DE102009026274A1 System und Vorrichtungen zum Vorheizen von Brennstoff in einem Kombizykluskraftwerk System and apparatus for preheating of fuel in a combined cycle power plant |
| 03/11/2010 | DE102008046582A1 Exhaust gas turbocharger for internal combustion engine, particularly motor vehicle, has shaft, which is pivoted in housing of exhaust gas turbocharger |
| 03/11/2010 | DE102008046219A1 Exhaust gas turbocharger for use in airplane, has rotor arranged at rotor axle, which is inclined with respect to horizontal plane at inclination angle, where inclination angle is of specific range |
| 03/11/2010 | CA2735981A1 Compressor casing resistant to titanium fire, high pressure compressor including such a casing, and aircraft engine including such a compressor |
| 03/11/2010 | CA2733701A1 Method for making an acoustic panel for the air intake lip of a nacelle |
| 03/11/2010 | CA2733427A1 Method for making a nacelle de-icing element |
| 03/10/2010 | EP2161464A2 Steam turbine with magnetic storage cooling |
| 03/10/2010 | EP2161431A2 Inlet nose cone for an aircraft gas turbine powerplant |
| 03/10/2010 | EP1590072B1 Evaporative duplex counterheat exchanger |
| 03/10/2010 | CN201420603Y Miniature gas turbine rotor system by adopting floating ring ball bearing |
| 03/10/2010 | CN201420571Y Miniature gas turbine rotor system by adopting tile type tilting bearing |
| 03/09/2010 | US7673461 Structural turbine engine casing |
| 03/09/2010 | US7673459 System and method for providing air to a compressor of an aircraft auxiliary gas turbine engine |
| 03/09/2010 | US7673455 Gas turbine combustor and fuel supply method for same |
| 03/04/2010 | WO2010024989A2 Multi passage fuel manifold and methods of construction |
| 03/04/2010 | WO2010023204A1 Fixed vane assembly for a turbine engine having a reduced weight, and turbine engine including at least one such fixed vane assembly |
| 03/04/2010 | WO2009139801A3 Offset ambient level fuel feed system |
| 03/04/2010 | US20100054926 System and method for thermal management of a gas turbine inlet |
| 03/04/2010 | US20100051112 Intake cone for a gas-turbine engine |
| 03/04/2010 | US20100050653 Combustor system and method of reducing combustion instability and/or emissions of a combustor system |
| 03/04/2010 | US20100050650 Gas turbine engine reverse-flow combustor |
| 03/04/2010 | US20100050649 Combustor device and transition duct assembly |
| 03/04/2010 | US20100050648 Combustor and the method of fuel supply and converting fuel nozzle |
| 03/04/2010 | US20100050647 Swirler for a fuel injector |
| 03/04/2010 | US20100050645 Fuel distribution manifold system for gas turbine engines |
| 03/04/2010 | US20100050644 Fuel injector |
| 03/04/2010 | US20100050641 Integrated fuel gas characterization system |
| 03/04/2010 | US20100050593 Flow equalizing override assembly for fuel divider system |
| 03/04/2010 | DE202009014218U1 CNA Abdeckung CNA cover |