| 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) |
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| 07/21/2005 | US20050155342 Methods and apparatus for assembling gas turbine engines |
| 07/21/2005 | US20050155224 Method of forming a fuel feed passage in the feed arm of a fuel injector |
| 07/21/2005 | DE19618313B4 Axialturbine eines Abgasturboladers An axial turbine of an exhaust turbocharger |
| 07/21/2005 | DE19501471B4 Turbine, insbesondere Gasturbine Turbine, in particular a gas turbine |
| 07/21/2005 | DE10360226A1 Gasturbine, insbesondere Flugtriebwerk Gas turbine, in particular aircraft engine |
| 07/21/2005 | DE10355353A1 Method for cooling a gas stream supplied to a turbomachine, e.g. a gas turbine being used for electricity generation, includes controlling purity of cooling liquid by discharge of polluted fluid and supply of fresh fluid |
| 07/20/2005 | EP1555484A2 Process to operate a gas turbine combustor |
| 07/20/2005 | EP1555407A1 Method and system for controlling gas turbine engine |
| 07/20/2005 | EP1555406A1 Cooling system for hot elements of aircraft engines and aircraft engine equipped with such a cooling system. |
| 07/20/2005 | EP1555394A1 Device to control clearances in a gas turbine |
| 07/20/2005 | EP1555393A2 Gas turbine engine component having bypass circuit |
| 07/20/2005 | EP1555392A2 Cantilevered stator stage |
| 07/20/2005 | EP1555391A2 Hybrid ceramic matrix composite turbine blade |
| 07/20/2005 | EP1555390A1 Cooling air exit openings for turbine blade |
| 07/20/2005 | EP1555333A2 Thermal barrier coating system |
| 07/20/2005 | EP1554796A1 Method for running-up a shaft assembly and device for carrying out the method |
| 07/20/2005 | EP1554524A1 A fuel injector |
| 07/20/2005 | EP1458981B1 Compressor for gas turbines |
| 07/20/2005 | EP1345732B1 Method for smoothing the surface of a gas turbine blade |
| 07/20/2005 | CN1643237A Refrigeration power plant |
| 07/20/2005 | CN1641188A Turbine engine with semi-fixed turbine |
| 07/20/2005 | CA2492418A1 Methods and apparatus for operating gas turbine engines |
| 07/19/2005 | US6919121 For use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. |
| 07/19/2005 | US6918747 Method and system for detecting damage to the rotor of an aircraft engine |
| 07/19/2005 | US6918745 Gas turbine engine axial stator compressor |
| 07/19/2005 | US6918255 Cooling of liquid fuel components to eliminate coking |
| 07/14/2005 | WO2005063579A1 Ram air channel for the supply of ambient air in an aircraft |
| 07/14/2005 | WO2005063564A2 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 |
| 07/14/2005 | WO2004009978A3 Methods and compositions for on-line gas turbine cleaning |
| 07/14/2005 | US20050152778 For the axial compressor of a gas turbine engine in which the stator tips rub against an abrasive section on the rotor drum during initial running of the engine to abrade the tips of the stator to provide optimised stator tip running clearance |
| 07/14/2005 | US20050152758 Modular metal working tooling apparatus |
| 07/14/2005 | US20050151017 Fire shield apparatus and method |
| 07/14/2005 | US20050150970 Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling system |
| 07/14/2005 | US20050150632 Extended impingement cooling device and method |
| 07/14/2005 | US20050150234 Gas turbine engine component having bypass circuit |
| 07/14/2005 | US20050150232 Turbomachine |
| 07/14/2005 | US20050150229 Method for operating a gas turbine |
| 07/14/2005 | US20050150204 Aeroengine intake |
| 07/14/2005 | DE10355356A1 Gas flow cooling method, by cooling fluid for removing heat energy from gas flow to temperature below ambient temperature of turbomachine |
| 07/14/2005 | DE10355354A1 Gas flow cooling method for turbomachine, by mixing antifreeze agent with cooling fluid when there is risk of frost |
| 07/14/2005 | DE102004058404A1 Vorrichtung und Verfahren zum Berechnen der mechanischen Turbinen-Ausgangsleistung, und mit dieser ausgestattete Gasturbinen-Steuervorrichtung Device and method for calculating the mechanical turbine output, and equipped with this gas turbine control apparatus |
| 07/14/2005 | DE102004057985A1 Gas-turbine combustion apparatus for use in vehicle, has turbine bypass mechanism has a shut-off valve which controls displacement of exhaust by the circular pipe out of the compartment through the exhaust gas opening material |
| 07/13/2005 | EP1553344A2 Fuel system |
| 07/13/2005 | EP1553282A1 Device for feeding cooling air to flap nozzle |
| 07/13/2005 | EP1553276A1 Turboengine with a receptor and a low pressure compressor drived by a low pressure turbine |
| 07/13/2005 | EP1553275A2 A method and apparatus for starting a gas turbine using a polyphase electric power generator |
| 07/13/2005 | EP1553274A2 Repowering steam plant through addition of gas turbine and method for remodelling plant facilities |
| 07/13/2005 | EP1553261A2 Fanned trailing edge teardrop array |
| 07/13/2005 | EP1553019A1 Turbofan engine mountable on top of the rear portion of an aircraft fuselage |
| 07/13/2005 | EP1552132A1 Turbine engine apparatus and method |
| 07/13/2005 | EP1552111A1 Gas turbine ventilation circuitry |
| 07/13/2005 | EP1466037B1 High-temperature protective coating |
| 07/13/2005 | EP1152848A4 Method and apparatus for production of a cast component |
| 07/13/2005 | CN1639451A Multi-spool by-pass turbofan engine |
| 07/13/2005 | CN1637247A Extended impingement cooling device and method |
| 07/13/2005 | CN1636662A Hole-drilling guide and method |
| 07/13/2005 | CN1210088C Methods for filtering air for a gas turbine system |
| 07/13/2005 | CA2491935A1 Cooling system for hot parts of an aircraft engine, and aircraft engine equipped with such a cooling system |
| 07/12/2005 | US6916551 Zirconium or erbium oxide; wear resistance, stability, durability |
| 07/12/2005 | US6916429 Comprises treatment with fluosilic acid; for turbine engines/air foils |
| 07/12/2005 | US6916154 Diametrically energized piston ring |
| 07/12/2005 | US6916151 Ventilation device for a high pressure turbine rotor of a turbomachine |
| 07/12/2005 | US6915640 Method and a device for supplying fuel to a combustion chamber |
| 07/12/2005 | US6915638 Nozzle with fluted tube |
| 07/12/2005 | US6915626 Blanking-plug system for blanking off an orifice of a pipe, particularly for blanking off an orifice of a duct for introducing air into the combustion chamber of a ramjet |
| 07/08/2005 | CA2491437A1 Turbine engine with semi-fixed turbine driving a receiver controlled so as to preserve a roughly constant rotation speed |
| 07/07/2005 | WO2005061874A1 Gas turbine comprising a generator cooled by kerosene |
| 07/07/2005 | WO2005061873A1 Gas turbine engine architecture |
| 07/07/2005 | WO2005060371A2 Common radial plane motor cooling |
| 07/07/2005 | WO2005028815A3 Device for the generation of mechanical or electrical energy using any thermal potential |
| 07/07/2005 | WO2004077400B1 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
| 07/07/2005 | US20050149274 Method and system for active tip clearance control in turbines |
| 07/07/2005 | US20050147790 Method for making a soundproofing panel with at least one double resonator |
| 07/07/2005 | US20050145070 Producing metallic articles by reduction of nonmetallic precursor compounds and melting |
| 07/07/2005 | US20050144960 System and method to stage primary zone airflow |
| 07/07/2005 | US20050144958 Nitrogen purge for combustion turbine liquid fuel system |
| 07/07/2005 | US20050144957 Methods for operating gas turbine engines |
| 07/07/2005 | US20050144931 Integral heat recovery device |
| 07/07/2005 | DE4325802B4 Verfahren zum Betrieb einer Gasturbinenanlage mit flüssigem oder gasförmigem Brennstoff A method of operating a gas turbine plant with liquid or gaseous fuel |
| 07/07/2005 | DE102004059318A1 Combustion system for use in turbines has heat exchanger with first member defining catalysing path and second member defining cooling path along different axis but in thermal contact to absorb thermal energy |
| 07/07/2005 | DE102004052433A1 Gasturbinen-Steuer- bzw. Regelungsvorrichtung, Gasturbinensystem und Gasturbinensteuer- bzw. Regelungsverfahren Gas turbine control or control apparatus, gas turbine system and Gasturbinensteuer- or regulatory procedure |
| 07/06/2005 | EP1550791A2 Method and system for active tip clearance control in turbines |
| 07/06/2005 | EP1550737A1 Thermal barrier coatings with improved impact and erosion resistance |
| 07/06/2005 | EP1550644A1 Ceramic compositions useful in thermal barrier coatings having reduced thermal conductivity |
| 07/06/2005 | EP1550642A2 Ceramic compositions useful for thermal barrier coatings having reduced thermal conductivity |
| 07/06/2005 | EP1549842A1 A system for catalytic combustion |
| 07/06/2005 | EP1309778A4 Compressor starting torque converter |
| 07/06/2005 | EP1234105B1 Sequential use of steam |
| 07/05/2005 | US6914355 Common radial plane motor cooling |
| 07/05/2005 | US6914344 Integrated starter/generator for a turbomachine |
| 07/05/2005 | US6913636 Low power nitrogen enriched air generation system |
| 07/05/2005 | US6913442 Internal coating on an internal passage wall exposed at a passage opening through an article external surface is protected from removal during repair of the article, including removal of at least a portion of an external coating, by a |
| 07/05/2005 | US6912838 Coated crossfire tube assembly |
| 06/30/2005 | WO2005059418A1 Air turbine starter having a low differential check valve |
| 06/30/2005 | WO2005059331A2 Bearing system for high-speed rotating machinery |
| 06/30/2005 | WO2005059316A1 Gas turbine, particularly an aircraft engine |
| 06/30/2005 | WO2005058693A1 Pressurized oil supply for propeller engine system |
| 06/30/2005 | US20050142395 Ceramic compositions useful in thermal barrier coatings having reduced thermal conductivity |
| 06/30/2005 | US20050142392 zirconia and stabilizer with three metal oxides (yttria, lanthana and ytterbia); physical vapor deposition onto metal substrate exposed to high temperatures; columnar microstructure |
| 06/30/2005 | US20050141989 Deflector embedded impingement baffle |