| 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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| 09/15/2005 | US20050199271 Mobile flushing unit and process |
| 09/15/2005 | US20050199270 Mobile flushing unit and process |
| 09/15/2005 | US20050198964 Controlled pressure fuel nozzle system |
| 09/15/2005 | US20050198941 Turbojet architecture with two fans at the front |
| 09/15/2005 | DE10393125T5 Kühlanordnung eines Übergangsstücks einer Gasturbine Cooling structure of a transition piece of a gas turbine |
| 09/15/2005 | CA2500044A1 Method and apparatus of determining as turbine shaft speed |
| 09/14/2005 | EP1575154A1 Turbo set |
| 09/14/2005 | EP1574764A2 High recovery sonic gas valve |
| 09/14/2005 | EP1574689A1 Methods and apparatus for operating gas turbine engines |
| 09/14/2005 | EP1574688A1 Mechanical drive system for an accessory gearbox |
| 09/14/2005 | EP1574687A1 Mechanical drive system for an accessory gearbox |
| 09/14/2005 | EP1574686A1 Mechanical drive system for an accessory gearbox |
| 09/14/2005 | EP1574675A2 Mobile flushing unit and process |
| 09/14/2005 | EP1574670A2 A mounting arrangement for turbine blades |
| 09/14/2005 | EP1573239A1 Honeycomb seal |
| 09/14/2005 | EP1180208A4 A thermodynamic apparatus |
| 09/14/2005 | EP1032811B1 Velocity adaptive control test method |
| 09/14/2005 | CN1667318A Working method of gas turbine-combustor |
| 09/13/2005 | US6942462 Gas turbine engine nose cone |
| 09/13/2005 | US6942449 Trailing edge cooling |
| 09/13/2005 | US6942203 Spring mass damper system for turbine shrouds |
| 09/13/2005 | US6942181 Passive cooling system for auxiliary power unit installation |
| 09/13/2005 | US6941760 Start system for expendable gas turbine engine |
| 09/13/2005 | US6941758 Internally coolable screw |
| 09/13/2005 | US6941633 Tooling provision for split cases |
| 09/12/2005 | CA2499675A1 Methods and apparatus for operating gas turbine engines |
| 09/12/2005 | CA2499674A1 Mobile flushing unit and process |
| 09/09/2005 | WO2005083248A1 Internal fuel manifold for gas turbine engine or gas turbine fuel nozzle assembly |
| 09/08/2005 | US20050196277 Gas turbine bucket tip cap |
| 09/08/2005 | US20050196270 Device for axially holding a ring spacer sector of a high-pressure turbine of a turbomachine |
| 09/08/2005 | US20050196268 High modulus metallic component for high vibratory operation |
| 09/08/2005 | US20050196088 Turbomachine with a compact roller bearing |
| 09/08/2005 | US20050194747 Sealing arrangement |
| 09/08/2005 | US20050193741 Liquid fuel nozzle apparatus with passive water injection purge |
| 09/08/2005 | US20050193738 Gas turbine plant and gas turbine power generator plant |
| 09/08/2005 | US20050193714 Gas turbine engine |
| 09/08/2005 | DE19828562B4 Triebwerk mit gegenläufig drehenden Rotoren Engine with counter-rotating rotors |
| 09/07/2005 | EP1571396A2 Sealing body for gas turbine combustor |
| 09/07/2005 | EP1571297A2 High elasticity modulus turbine metallic component for high vibratory operation |
| 09/07/2005 | EP1571294A1 Hook-shaped sideplate for a rotor disc |
| 09/07/2005 | EP1570566A1 Gas turbine engine starter generator with multiple windings on each exciter stator pole |
| 09/07/2005 | EP1570162A1 Hermetic motor and gas booster |
| 09/07/2005 | CN1665960A Highly oxidation resistant component |
| 09/07/2005 | CN1665959A Highly oxidation resistant component |
| 09/07/2005 | CN1665623A Diffusion bond mixture for healing single crystal alloys |
| 09/07/2005 | CN1664332A Catalytic treatment of fuel to impart coking resistance |
| 09/07/2005 | CN1664331A Closed circuit blade-cooled turbine |
| 09/07/2005 | CN1664319A Turbomachine rolling bearing assembly having a reduced space requirement |
| 09/07/2005 | CN1664318A Axial maintenance device to support the strut of a stator ring of the high-pressure turbine of a turbomachine |
| 09/07/2005 | CN1664316A Gas turbine bucket tip cap |
| 09/07/2005 | CN1663663A Multi-stage fuel deoxygenator |
| 09/06/2005 | US6939392 removing oxygen from a fuel stream fed to an engine used to drive an aircraft, transferring heat from a heat generating sub-system to the fuel and combusting the fuel |
| 09/06/2005 | US6939107 Spanwisely variable density pedestal array |
| 09/06/2005 | US6938447 Apparatus and method of correcting deformation of gas turbine blade |
| 09/06/2005 | US6938424 Annular combustion chambers for a gas turbine and gas turbine |
| 09/06/2005 | US6938407 Bleed-off device in a bypass turbojet |
| 09/06/2005 | CA2265164C Removal of cooling air on the housing side of a diffuser of a compressor stage of gas turbines |
| 09/01/2005 | WO2005080772A1 Gas turbine plant |
| 09/01/2005 | WO2005047670A3 Method and apparatus for actuating fuel trim valves in a gas turbine |
| 09/01/2005 | WO2005042928A3 Heat shield for gas turbine engine |
| 09/01/2005 | US20050191755 Evaluating oxide layer on components of hot CO2/H2O gas turbines; predicting metal fatigue |
| 09/01/2005 | US20050191422 Applying mask material to cooling holes so that holes are at partially filled with mask material in portion closest to external surface and up to the level of the external surface, thickening portion of mask material within cooling holes, coating, removing thickened mask material |
| 09/01/2005 | US20050191169 Silencer for ventilation system and methods |
| 09/01/2005 | US20050191167 Fanned trailing edge teardrop array |
| 09/01/2005 | US20050191166 Passive improved air turbine starter lubrication system |
| 09/01/2005 | US20050188704 Aircraft gas turbine engines |
| 09/01/2005 | US20050188701 Solid propellant gas generators in power systems |
| 09/01/2005 | US20050188699 Apparatus for fuel transport and the like |
| 09/01/2005 | US20050188673 Gas turbine exhaust passage and damper system for same |
| 08/31/2005 | EP1568868A2 High by-pass ratio turbofan |
| 08/31/2005 | EP1568117A1 Electric starter motor with integral clutch |
| 08/31/2005 | EP1567756A1 Method for controlling the injection of liquid into an inflow channel of a prime mover or a machine-tool |
| 08/31/2005 | EP1456508B1 Hot gas path subassembly of a gas turbine |
| 08/31/2005 | EP1360342B1 Method for plasma coating a turbine blade and coating device |
| 08/31/2005 | CN1662735A Power fluctuation suppressing method and power generation facility using same |
| 08/31/2005 | CN1662734A Orbiting combustion nozzle engine |
| 08/31/2005 | CN1661200A Return blade rotary machinery using same |
| 08/31/2005 | CN1217092C Gas turbine, gas turbomachine and coolant collecting method for blades of the same |
| 08/31/2005 | CN1217091C Closed circulation cooling blade turbomachine |
| 08/30/2005 | USRE38784 Apparatus for the destruction of volatile organic compounds |
| 08/30/2005 | US6935837 Methods and apparatus for assembling gas turbine engines |
| 08/30/2005 | US6935834 Noise reduction conduit for static components in aircraft engines |
| 08/30/2005 | US6935831 Methods and apparatus for operating gas turbine engines |
| 08/30/2005 | US6935120 Approach to extending life of gas turbine engine |
| 08/30/2005 | US6935119 Methods for operating gas turbine engines |
| 08/30/2005 | US6935117 Turbine engine fuel injector |
| 08/30/2005 | CA2407155C Axis seal mechanism and turbine |
| 08/30/2005 | CA2344012C Cooling structure of combustor tail tube |
| 08/30/2005 | CA2266449C Gas turbine airfoil cooling |
| 08/25/2005 | WO2005077554A1 Method and apparatus for cleaning a turbofan gas turbine engine |
| 08/25/2005 | US20050187676 Approach to extending life of gas turbine engine |
| 08/25/2005 | US20050186069 Use of biased fabric to improve properties of SiC/SiC ceramic composites for turbine engine components |
| 08/25/2005 | US20050186067 Air turbine starter having a force balanced, pressure energized, weighted check valve |
| 08/25/2005 | US20050183540 Apparatus for driving an accessory gearbox in a gas turbine engine |
| 08/25/2005 | US20050183529 Apparatus for driving an accessory gearbox in a gas turbine engine |
| 08/25/2005 | US20050183423 Apparatus for driving an accessory gearbox in a gas turbine engine |
| 08/25/2005 | US20050183413 Pulse detonation engine and valve |
| 08/25/2005 | DE102005005472A1 Verbessertes Anfahrverfahren für Kraftwerke Improved start-up procedure for power plants |
| 08/24/2005 | EP1566530A1 Gas turbine |
| 08/24/2005 | EP1566529A1 Atmospheric pressure combustion turbine system |