| 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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| 04/21/2007 | CA2564488A1 Device for extracting mechanical power between the hp and lp shafts of a twin-spool turbine engine |
| 04/21/2007 | CA2564485A1 Driving device for accessory machines for a gas turbine engine |
| 04/19/2007 | WO2007044020A2 Two-stage fuel delivery for gas turbines |
| 04/19/2007 | WO2007041997A2 Device and method for axially displacing a turbine rotor |
| 04/19/2007 | US20070084218 Fan static structure |
| 04/19/2007 | US20070084216 Device for supporting and housing auxiliaries in a bypass turbojet |
| 04/19/2007 | US20070084214 Torque control for starling system |
| 04/19/2007 | US20070084213 Annular gas turbine combustor |
| 04/19/2007 | US20070084212 Method for the Operation of a Compressor of a Gas Turbine With Evaporative Cooling of the Compressor Induction Air |
| 04/19/2007 | DE102005048027A1 Fuel supply device for gas turbine e.g. windmill, has fuel system with low pressure and high pressure fuel pumps, where fuel of inlet pipeline of low pressure fuel pump is fed back by feedback pipeline that is provided with closing unit |
| 04/19/2007 | CA2563482A1 Gas turbine engine assembly and methods of assembling same |
| 04/18/2007 | EP1775514A2 Fuel system and method of reducing emission |
| 04/18/2007 | EP1775445A2 Method of repair for inlet caps of turbine engines |
| 04/18/2007 | EP1773662A1 Aircraft propulsion system |
| 04/18/2007 | EP1611465A4 Method and apparatus for converting or otherwise utilizing radiation pressure to generate mechanical work |
| 04/18/2007 | CN1950601A Apparatus and method for storing thermal energy and generating electricity |
| 04/18/2007 | CN1950595A Turbine nozzle segment, turbine nozzle, turbine, and gas turbine engine |
| 04/18/2007 | CN1948835A Fuel system and method of reducing emission |
| 04/18/2007 | CN1948732A Bolting configuration for joining ceramic combustor liner to metal mouting attachments |
| 04/18/2007 | CN1948731A Active clearance control system for gas turbine engines |
| 04/18/2007 | CN1948730A Volume type continuously burning type engine |
| 04/18/2007 | CN1311195C Thermal shield for component carrying hot gases, especially for structural components of gas turbines |
| 04/17/2007 | US7204926 Mounting blisk in a multiaxis electrochemical machine;electrochemically machining in a first sequence a first row of blades in one stage of blisk while mounted in machine; andelectrochemically machining in a second sequence a second row of blades in another stage of blisk while mounted in machine |
| 04/17/2007 | US7204675 Cooled gas turbine engine vane |
| 04/17/2007 | US7204090 Modulated current gas turbine engine starting system |
| 04/17/2007 | US7204077 Atmospheric pressure combustion turbine system |
| 04/17/2007 | US7204019 Method for repairing an apertured gas turbine component |
| 04/12/2007 | WO2007039638A1 Process and device for monitoring the formation of deposits of solid particles, in particular in a fuel line and in the fuel valves of a gas turbine |
| 04/12/2007 | WO2007003587A3 Molding compound for producing a refractory lining |
| 04/12/2007 | US20070082201 USE OF BIASED FABRIC TO IMPROVE PROPERTIES OF SiC/SiC CERAMIC COMPOSITES FOR TURBINE ENGINE COMPONENTS |
| 04/12/2007 | DE10332043B4 Antriebssystem für Turbolader mit elektrischer Maschine Drive System for turbocharger with electric machine |
| 04/12/2007 | DE102005048019A1 Aircraft engine e.g. gas turbine, oil supplying method, involves leading oil into oil cooler, where oil cooler controls oil supply temperature to respective storage chamber such that same oil outlet temperature results for storage chambers |
| 04/12/2007 | DE102005048017A1 Fuel and oil system for gas turbine, has oil pump with outlet pipeline connected with heat exchanger, and another heat exchanger arranged in fuel rear guiding pipeline for guiding high pressure fuel pump from pump outlet to pump inlet |
| 04/12/2007 | DE102005045839A1 Verfahren zum Reinigen von Hohlräumen an Gasturbinenbauteilen A method for cleaning cavities on gas turbine components |
| 04/11/2007 | EP1772673A1 Method and Device for Monitoring the Deposition of Solid Particles, in particular in the Fuel Line of a Gas Turbine |
| 04/11/2007 | EP1390606B1 Device for cooling coolant in a gas turbine and gas and steam turbine with said device |
| 04/11/2007 | CN1946967A Liquid fuel injection with purge air |
| 04/11/2007 | CN1309938C Method and device for cooling inflow of shaft of steam turbine |
| 04/11/2007 | CN1309937C Metallic honeycomb cellular seal-structure for turbomachine |
| 04/10/2007 | US7201882 Configured to employ the properties of steady streams carrying an acoustic condition so as to construct a reaction system in which all the free particles adopt coherent behaviour subject to the laws of acoustics. |
| 04/10/2007 | US7201564 Turbine vane system |
| 04/10/2007 | US7201559 Stationary ring assembly for a gas turbine |
| 04/10/2007 | US7200998 Gas turbine combustor and operating method thereof |
| 04/10/2007 | US7200997 Water augmented regeneration (WAR) turbine system and cycle |
| 04/10/2007 | US7200985 Fuel delivery system having an ecology valve |
| 04/10/2007 | CA2407544C Combustion engine, gas turbine, and abrasive layer |
| 04/10/2007 | CA2293022C Repair of high pressure turbine shrouds |
| 04/05/2007 | WO2007037277A1 Nickel-base superalloy with excellent unsusceptibility to oxidation |
| 04/05/2007 | WO2007036964A1 Method for starting a gas turbine equipped with a gas burner, and axial swirler for said burner |
| 04/05/2007 | WO2007036523A1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
| 04/05/2007 | WO2007036522A1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
| 04/05/2007 | WO2007036520A2 Engine mounting structure for an aircraft engine |
| 04/05/2007 | WO2007036515A1 Two-shackle aircraft engine rear attachment |
| 04/05/2007 | WO2007036059A1 Turbine cleaning |
| 04/05/2007 | WO2007036014A1 Emergency fuel shutoff system and method |
| 04/05/2007 | US20070074519 Method and apparatus for controlling combustion device dynamics |
| 04/05/2007 | CA2624010A1 Aircraft engine assembly comprising an engine and a suspension pylon for such an engine |
| 04/05/2007 | CA2624005A1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine |
| 04/05/2007 | CA2623999A1 Two-shackle aircraft engine rear attachment |
| 04/05/2007 | CA2622006A1 Emergency fuel shutoff system and method |
| 04/04/2007 | EP1770811A2 Fuel-cell apparatus with coupled compressor and turbine |
| 04/04/2007 | EP1769208A2 Improved heat exchanger performance |
| 04/04/2007 | EP1769147A1 Method for operating a gas turbine group |
| 04/04/2007 | EP1649144B1 Electrical power generation system and method |
| 04/04/2007 | EP1514018B1 A turbine and a component |
| 04/04/2007 | CN2886097Y Shock-absorption mounting device for fuel manifold in gas turbine |
| 04/04/2007 | CN1308580C Gas turbine system comprising closed system of fuel and combustion gas using underground coal layer |
| 04/03/2007 | US7200538 Methods and apparatus for modeling gas turbine engines |
| 04/03/2007 | US7198483 Burner unit and method for operation thereof |
| 04/03/2007 | US7198463 Rotating blade body and rotary machine using rotating blade body |
| 04/03/2007 | US7198052 Mobile flushing unit and process |
| 04/03/2007 | US7197882 Turbojet diffuser |
| 04/03/2007 | US7197880 Lean blowoff detection sensor |
| 04/03/2007 | US7197879 Multiple electric fuel metering systems for gas turbine applications |
| 04/03/2007 | US7197877 Support system for a pilot nozzle of a turbine engine |
| 03/29/2007 | US20070072007 Hybrid ceramic matrix composite turbine blades for improved processibility and performance |
| 03/29/2007 | US20070068170 Emergency fuel shutoff system and method |
| 03/29/2007 | US20070068168 Method of operating a thermal power plant, preferably a gas turbine power plant |
| 03/29/2007 | US20070068167 Turbine exhaust catalyst |
| 03/29/2007 | US20070068164 Anti-coking injector arm |
| 03/29/2007 | US20070068135 Engine |
| 03/29/2007 | DE102006044147A1 Sealing arrangement and method for a stator cover ring in a multi-stage gas turbine has inner and outer covers with grooves and hooks and an elastic seal |
| 03/29/2007 | DE102005047696A1 Siphon-like hydraulic seal for use between e.g. high- and low pressure shafts of aircraft engine, has locking bar movably and axially held at circumference of inner shaft and formed in rotational direction of hydraulic fluid barrier |
| 03/29/2007 | DE102005046208A1 Jet propulsion unit, especially for aircraft, has integrated motor/generator unit in rotation plane of at least first compressor stage, stator around compressor housing, rotor formed by blade elements at least of first compressor stage |
| 03/29/2007 | DE102005042889A1 Gasturbogruppe Gas turbine group |
| 03/29/2007 | DE102005028296B4 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine |
| 03/28/2007 | EP1766488A2 Pneumatic valve control using downstream pressure feedback and an air turbine starter incorporating the same |
| 03/28/2007 | EP1766191A1 Method and device for monitoring a cooling air system of a turbine |
| 03/28/2007 | EP1470328B1 Turbofan exhaust nozzle and method of reducing noise in such a nozzle |
| 03/28/2007 | EP1227905B1 Multipiece core assembly for cast airfoil |
| 03/28/2007 | CN1938549A Multiple burner arrangement for operating a combustion chamber, and method for operating the multiple burner arrangement |
| 03/28/2007 | CN1936302A Process for processing ring-shape original surface heat regenerator for minisize gas turbine |
| 03/28/2007 | CN1936301A Gas turbine apparatus |
| 03/28/2007 | CA2561225A1 Anti-coking injection arm |
| 03/27/2007 | US7195448 Cooled rotor blade |
| 03/27/2007 | US7194866 Static structure for an expendable gas turbine engine |
| 03/27/2007 | US7194864 Approach to extending life of gas turbine engine |
| 03/27/2007 | US7194862 Resonator adopting counter-bored holes and method of suppressing combustion instabilities |
| 03/27/2007 | CA2364377C Gas turbine combustor, gas turbine, and jet engine |
| 03/27/2007 | CA2248736C Internally heatshielded nozzle |