| 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) |
|---|
| 02/21/2006 | US7000895 Valve having pressure balancing piston and method involving same |
| 02/21/2006 | US7000406 Gas turbine combustor sliding joint |
| 02/21/2006 | US7000405 Gas turbine apparatus and a starting method thereof |
| 02/21/2006 | US7000404 Heat exchanger on a turbine cooling circuit |
| 02/21/2006 | US7000403 Primary fuel nozzle having dual fuel capability |
| 02/21/2006 | US7000399 System for warming pressurized gas |
| 02/16/2006 | WO2006015613A1 Turbocharger |
| 02/16/2006 | US20060034693 Twin-spool turbojet with means for driving ancillary machines |
| 02/16/2006 | US20060034682 Ducted fan with containment structure |
| 02/16/2006 | US20060032988 Boundary layer control arrangement |
| 02/16/2006 | US20060032234 Combined power main engine start system |
| 02/16/2006 | US20060032211 Gas turbine installation |
| 02/16/2006 | US20060032210 Methods and apparatus for assembling a gas turbine engine |
| 02/16/2006 | DE102004036331A1 Einströmgehäuse für axiale Strömungsmaschinen Inflow for axial flow machines |
| 02/16/2006 | CA2573658A1 Compressed-air generating system |
| 02/15/2006 | EP1626170A1 Turbomachine with counter-rotating fan |
| 02/15/2006 | EP1626160A2 Degassing pipe for low pressure turbine shaft |
| 02/15/2006 | EP1132594B1 Gas turbine power generation equipment and air humidifying apparatus |
| 02/15/2006 | CN1242162C Oxygen separation method integrated with gas turbine |
| 02/14/2006 | US6998728 Method and apparatus for controlling output current of turbine/alternator on common shaft |
| 02/14/2006 | US6998568 Method for fabricating, modifying or repairing of single crystal or directionally solidified articles |
| 02/14/2006 | US6997437 Valve for dynamic control of fuel flow rate in gas turbine power plant, power plant and components thereof employing such valve, and method of constructing such valve |
| 02/14/2006 | US6996991 Fuel injection system for a turbine engine |
| 02/14/2006 | US6996970 High accuracy fuel metering system for turbine engines |
| 02/14/2006 | US6996969 Multi-mode shutdown system for a fuel metering unit |
| 02/14/2006 | US6996968 Bifurcated oil scavenge system for a gas turbine engine |
| 02/14/2006 | CA2291374C A dual fuel nozzle |
| 02/11/2006 | CA2513053A1 Controlled gap carbon seal |
| 02/09/2006 | US20060029723 repairing a coated high pressure turbine blade, which has been exposed to engine operation, to restore coated airfoil contour dimensions of the blade, and improve upon the prior bond coat |
| 02/09/2006 | US20060029493 Noise control |
| 02/09/2006 | US20060027705 Engine mounting structure under an aircraft wing |
| 02/09/2006 | US20060026967 Compact quick attach starter-generator installation |
| 02/09/2006 | US20060026966 Support system for a pilot nozzle of a turbine engine |
| 02/09/2006 | US20060026963 Approach to extending life of gas turbine engine |
| 02/09/2006 | US20060026947 Regulator feeding control with two flow rate laws |
| 02/09/2006 | DE202005019320U1 Exhaust gas turbine for superchargers of internal combustion engines has thermal protection layer covering turbine blades and turbine disk |
| 02/09/2006 | DE19844843B4 Planetengetriebe Planetary gear |
| 02/08/2006 | EP1624246A1 Metering control with two different control laws for a backup control valve |
| 02/08/2006 | EP1624041A1 System for reforming heavy oil , method thereof, and combined cycle power system |
| 02/08/2006 | EP1623104A1 Device for damping sound in a duct |
| 02/07/2006 | US6994920 welding two alloys; one alloy being free of an element that can form a continuous layer of a brittle intermetallic; repairing turbine engine blades |
| 02/07/2006 | US6994744 Filter arrangement and methods |
| 02/07/2006 | US6994524 Hollow fan blade for gas turbine engine |
| 02/07/2006 | US6993916 Burner tube and method for mixing air and gas in a gas turbine engine |
| 02/07/2006 | US6993915 Solid propellant gas generators in power systems |
| 02/07/2006 | US6993914 Convergent-divergent turbojet nozzle |
| 02/07/2006 | US6993913 Gas turbine plant |
| 02/07/2006 | US6993910 Fluid machine |
| 02/07/2006 | US6993821 Manufacturing cell using tooling apparatus |
| 02/07/2006 | US6993811 System for applying a diffusion aluminide coating on a selective area of a turbine engine component |
| 02/02/2006 | WO2006011465A1 Wheel chamber casing and gas turbine |
| 02/02/2006 | US20060024154 Zero acoustic splice fan case liner |
| 02/02/2006 | US20060024152 Intake housing for axial fluid flow engines |
| 02/02/2006 | US20060021354 Apparatus and method for gas turbine engine fuel/air premixer exit velocity control |
| 02/02/2006 | US20060021350 Fuel injection apparatus |
| 02/02/2006 | US20060021349 Fuel injection system for a turbine engine |
| 02/02/2006 | US20060021323 Turbine engine arrangement |
| 02/02/2006 | CA2574641A1 Combined rankine and vapor compression cycles |
| 02/01/2006 | EP1621949A2 Pressure regulator |
| 02/01/2006 | EP1621817A1 Afterburner with assured ignition |
| 02/01/2006 | EP1621752A2 Noise attenuation at a splice in a fan case liner |
| 02/01/2006 | EP1621744A1 A turbine engine nose cone |
| 02/01/2006 | EP1621743A1 Inlet housing for axial turbomachines |
| 02/01/2006 | EP1621742A1 Gas turbine heat exchanger assembly and method for fabricating same |
| 02/01/2006 | EP1621741A1 Gas turbine system |
| 02/01/2006 | EP1299621B1 Drainage system for gas turbine supporting bearings |
| 02/01/2006 | CN1729589A Power generating system |
| 02/01/2006 | CN1727698A Noise attenuation at a splice in a fan case liner |
| 02/01/2006 | CN1727645A High efficiency stator for the first phase of a gas turbine |
| 02/01/2006 | CN1727642A High temperature gas flow passage component with mesh type and impingement cooling |
| 02/01/2006 | CN1727641A High efficiency rotor for a gas turbine |
| 02/01/2006 | CN1240079C Brayton cycle nuclear power plant and a method of starting the brayton cycle |
| 01/31/2006 | US6991433 Drum, in particular a drum forming a turbomachine rotor, a compressor, and a turboshaft engine including such a drum |
| 01/31/2006 | US6991429 Sealing structure of spindle bolt, and gas turbine |
| 01/31/2006 | US6991026 Heat exchanger with header tubes |
| 01/31/2006 | US6990815 Gas turbine and gas turbine high temperature section cooling method |
| 01/31/2006 | US6990798 Hybrid inlet |
| 01/31/2006 | US6990797 Methods and apparatus for operating gas turbine engines |
| 01/31/2006 | CA2381659C Gas turbine combined plant |
| 01/28/2006 | CA2513783A1 Turbo engine inlet bullet fairing |
| 01/27/2006 | CA2507082A1 Zero acoustic splice fan case liner |
| 01/26/2006 | WO2006009971A2 Heat exchanger with header tubes |
| 01/26/2006 | WO2006008353A1 Revolving toroidal motor |
| 01/26/2006 | WO2006008221A1 Method for operating a gas turbine group |
| 01/26/2006 | US20060016932 Variable position intake for an aircraft mounted gas turbine engine |
| 01/26/2006 | US20060016527 performing recovery, solution and aging heat treatments of the nickel based alloy component; hot isostatic pressing; improved creep life, ductility or toughness |
| 01/26/2006 | US20060016199 Gas turbine combustor and operating method thereof |
| 01/26/2006 | US20060016198 Apparatus and method for providing an off-gas to a combustion system |
| 01/26/2006 | US20060016195 Bypass and injection method and apparatus for gas turbines |
| 01/26/2006 | US20060016190 Methods and apparatus for cooling turbine engine combustor ignition devices |
| 01/26/2006 | US20060016173 Securing arrangement |
| 01/26/2006 | US20060016169 Laser augmented turbojet propulsion system |
| 01/26/2006 | DE102004031783A1 Gas turbine for aircraft engine has fuel supply system which exhibits wave-channel in which turbine shaft is swivel mounted and part of fuel supply takes place through shaft alley, which exhibits fuel outlets at its outer circumference |
| 01/26/2006 | CA2573206A1 Aircraft propulsion system |
| 01/25/2006 | EP1619370A1 Generator assembly |
| 01/25/2006 | EP1619369A2 Methods and apparatus for cooling turbine engine combustor ignition devices |
| 01/25/2006 | EP1334286B1 Rotary machine with axial stop incorporating a current generator |
| 01/25/2006 | CN1724851A Method and system for operating rotary machines |
| 01/25/2006 | CN1724849A 透平叶片 Turbine blades |
| 01/25/2006 | CN1724116A Oxygen separator and oxygen separation method |