| 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) |
|---|
| 06/05/2008 | US20080127627 Compact recirculating lubrication system for a miniature gas turbine engine |
| 06/05/2008 | DE102007054926A1 Schutzvorrichtung für Turbinendichtungen Protection device for turbine seals |
| 06/04/2008 | EP1928216A1 Inlet electromagnetic flow control |
| 06/04/2008 | EP1927740A2 Gearbox with removable oil tank |
| 06/04/2008 | CN101194091A System for deicing the leading edge of a nose inlet cowl for a turbine engine |
| 06/04/2008 | CN101194090A Gas turbine fuel preparation and introduction method |
| 06/04/2008 | CN100392220C Water treatment and pressurization system for the adiabatic cooling of comburent air |
| 06/03/2008 | US7380402 Method for operating a gas turbine and gas turbine system for carrying out the method |
| 05/30/2008 | CA2603636A1 Methods and system for recuperated cooling of integral turbine nozzle and shroud assemblies |
| 05/30/2008 | CA2603312A1 Method and system to facilitate cooling turbine engines |
| 05/30/2008 | CA2603174A1 Methods and system for cooling integral turbine nozzle and shroud assemblies |
| 05/30/2008 | CA2602311A1 Method and system to facilitate enhanced local cooling of turbine engines |
| 05/30/2008 | CA2601686A1 Methods and system for cooling integral turbine shroud assemblies |
| 05/30/2008 | CA2601612A1 Method and system to facilitate preferentially distributed recuperated film cooling of turbine shroud assembly |
| 05/29/2008 | WO2008064197A2 Systems and methods for producing power using positive displacement devices |
| 05/29/2008 | WO2008063153A2 Managing low pressure turbine maximum speed in a turbofan engine |
| 05/29/2008 | WO2008063152A2 Turbofan engine |
| 05/29/2008 | WO2008062678A1 Intake air heating control apparatus for gas turbine |
| 05/29/2008 | WO2008062148A1 Ice protection system with noise abatement |
| 05/29/2008 | WO2008061686A1 A gas intake system |
| 05/29/2008 | WO2008029062A3 Device for improving the effectiveness of acoustic treatments in an aircraft drive duct |
| 05/29/2008 | US20080120960 Carbon dioxide recirculation |
| 05/29/2008 | CA2612031A1 Turbofan engine assembly and method of assembling same |
| 05/28/2008 | EP1925833A1 Damper element of bearing, method of manufacturing damper element, bearing, and gas turbine engine |
| 05/28/2008 | EP1925551A1 Ice protection system with noise abatement |
| 05/28/2008 | EP1924761A1 System and method for augmenting power output from a gas turbine engine |
| 05/28/2008 | CN101189411A Gas turbine with a gap blocking device |
| 05/28/2008 | CN100390389C Seal assembly |
| 05/28/2008 | CN100390021C Device for stabilizing the engine inlet flow in static tests of engines |
| 05/28/2008 | CA2610641A1 Device linking two rotary shafts in a turbomachine |
| 05/28/2008 | CA2610639A1 Device linking two rotary shafts, specifically in a turbomachine |
| 05/27/2008 | US7377749 Device for balancing a rotating part, in particular a turbojet rotor |
| 05/27/2008 | US7377748 Fanned trailing edge teardrop array |
| 05/27/2008 | US7377417 Repair process |
| 05/27/2008 | US7377305 Method and apparatus for production of a cast component |
| 05/27/2008 | US7377117 Transition piece for gas turbine |
| 05/27/2008 | US7377115 Approach to extending life of gas turbine engine |
| 05/27/2008 | US7377114 Turbine engine pulsed fuel injection utilizing stagger injector operation |
| 05/27/2008 | US7377112 Fuel deoxygenation for improved combustion performance |
| 05/27/2008 | US7377110 Deoiler for a lubrication system |
| 05/27/2008 | US7377100 Bypass duct fluid cooler |
| 05/27/2008 | US7377098 Gas turbine engine frame with an integral fluid reservoir and air/fluid heat exchanger |
| 05/27/2008 | CA2434920C Superalloy for single crystal turbine vanes |
| 05/27/2008 | CA2282010C Film-cooling hole and method of producing it |
| 05/22/2008 | WO2008059971A1 Multilayer alloy coating film, heat-resistant metal member having the same, and method for producing multilayer alloy coating film |
| 05/22/2008 | WO2008059620A1 Film cooling structure |
| 05/22/2008 | WO2008059168A2 Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
| 05/22/2008 | US20080115502 System for vaporization of liquid fuels for combustion and method of use |
| 05/22/2008 | US20080115501 Triple annular counter rotating swirler |
| 05/22/2008 | US20080115499 Combustor heat shield with variable cooling |
| 05/22/2008 | US20080115496 System and method for regulating fuel flow into a turbine |
| 05/22/2008 | US20080115477 Localized arc filament plasma actuators for noise mitigation and mixing enhancement |
| 05/22/2008 | CA2669941A1 Multilayer alloy coating film, heat-resistant metal member having the same, and method for producing multilayer alloy coating film |
| 05/22/2008 | CA2669178A1 Aircraft leading edge |
| 05/22/2008 | CA2669173A1 Acoustic lining for an aircraft, including a frost treatment system using the joule effect |
| 05/21/2008 | EP1923651A1 A gas intake system |
| 05/21/2008 | EP1923544A2 Fuel system and ecology valve for use therein |
| 05/21/2008 | EP1923542A2 Interdependant lubrication systems |
| 05/21/2008 | EP1923541A2 Lubrication scavenge system |
| 05/21/2008 | EP1923540A2 Oil Sump Housing |
| 05/21/2008 | CN101184912A 燃气涡轮发动机冷却系统和方法 A gas turbine engine cooling systems and methods |
| 05/21/2008 | CN100389252C Start control device and method for micro gas turbine high speed engine |
| 05/20/2008 | US7375531 Method of informing pilot of aircraft of spark detected in gas turbine engine |
| 05/20/2008 | US7374821 Low thermoconductivity and high high-temperature strength; for turbines; zirconia-based ceramic stabilized with trivalent oxide and oxygen vacancies reduced by pentavalent oxides, such as zirconia with yttria and niobium oxide |
| 05/20/2008 | US7373781 Methods and apparatus for injecting cleaning fluids into combustors |
| 05/20/2008 | US7373780 Method of scavenging oil within a gas turbine engine |
| 05/20/2008 | US7373779 Methods and apparatus for cooling gas turbine engines |
| 05/20/2008 | US7373773 Gas turbine installation, cooling air supplying method and method of modifying a gas turbine installation |
| 05/20/2008 | US7373772 Turbine combustor transition piece having dilution holes |
| 05/20/2008 | US7373771 Cooling arrangement for an accessory gearbox and method of cooling |
| 05/20/2008 | CA2450723C Method of repairing a ni-based alloy part |
| 05/20/2008 | CA2431286C A method and a device for supplying fuel to a combustion chamber |
| 05/20/2008 | CA2414021C Method and apparatus for directionally solidified casting |
| 05/15/2008 | WO2008056790A1 Gas turbine power generation system and method of detecting its calorie abnormality |
| 05/15/2008 | WO2008055397A1 Electric aero compressor |
| 05/15/2008 | US20080112797 Transpiration clearance control turbine |
| 05/15/2008 | US20080110178 Assembly procedure for the adjustable pin-valve, fuel shut-off |
| 05/15/2008 | US20080110177 Turbine engine pulsed fuel injection utilizing stagger injector operation |
| 05/15/2008 | US20080110151 Turbofan emergency generator |
| 05/15/2008 | DE112006001149T5 Verfahren und Vorrichtung für die Nasskompression Method and apparatus for the wet compression |
| 05/15/2008 | CA2609279A1 Compound clearance control engine |
| 05/15/2008 | CA2608304A1 Assembly procedure for the adjustable pin-valve, fuel shut-off |
| 05/14/2008 | EP1921292A2 Compound tubine cooled engine |
| 05/14/2008 | EP1921291A2 Gas turbine engine providing simulated boundary layer thickness increase |
| 05/14/2008 | EP1921276A2 Radially energised oil capture device for a geared turbofan |
| 05/14/2008 | EP1921275A2 Cooling arrangement for aircraft electronics |
| 05/14/2008 | EP1921271A2 Titanium foil as a structural heater element |
| 05/14/2008 | EP1921270A2 Compound nozzle cooled engine |
| 05/14/2008 | CN101178040A Method for manufacturing full-functional high-energy induction and catalyst combined type complete combustion device |
| 05/14/2008 | CN101178029A Interstage cooled turbine engine |
| 05/14/2008 | CN101178028A Compound tubine cooled engine |
| 05/14/2008 | CN101178027A Heat exchanger assembly for a gas turbine engine |
| 05/13/2008 | US7371426 lower growth environmental bond coating of an aluminum alloy applied to the remaining base metal substrate so that upon subsequent repair of the component, less of the remaining base metal substrate is removed because of less environmental coating growth into the substrate than prior bond coat |
| 05/13/2008 | US7370666 Power system with computer-controlled fuel system |
| 05/13/2008 | US7370478 Method of controlling a gas combustor of a gas turbine |
| 05/13/2008 | CA2364761C Methods and apparatus for controlling bearing loads within bearing assemblies |
| 05/13/2008 | CA2364159C Variable stator vane bushing |
| 05/10/2008 | CA2607878A1 Compound nozzle cooled engine |
| 05/10/2008 | CA2607675A1 Compound turbine cooled engine |
| 05/10/2008 | CA2607674A1 Dual interstage cooled engine |