| 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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| 12/30/2004 | US20040261395 Reliable LNG vaporizer |
| 12/30/2004 | US20040261285 Drying machine system utilizing gas turbine, and method of use |
| 12/30/2004 | US20040261265 Method for improving the wear resistance of a support region between a turbine outer case and a supported turbine vane |
| 12/30/2004 | DE102004026696A1 Turbinendichtungsanordnung und zugehöriges Verfahren Turbine seal assembly and associated method |
| 12/29/2004 | WO2003104511A3 Thermal spray compositions for abradable seals |
| 12/29/2004 | EP1491806A1 Device for fixing and holding electrical harness on a jet engine |
| 12/29/2004 | EP1491781A1 Connecting rod between two mechanical members |
| 12/29/2004 | EP1491778A1 Fastening by screw and nuts |
| 12/29/2004 | EP1491752A1 Ventilation channels in the confluence plate of an afterburning chamber |
| 12/29/2004 | EP1491725A2 Bearing device for an adjustable vane |
| 12/29/2004 | EP1491720A1 Method for improving the wear resistance of a support region between a turbine outer case and a supported turbine vane |
| 12/29/2004 | EP1491643A2 Heat treatment for workpieces |
| 12/29/2004 | EP1491283A1 Repair process |
| 12/29/2004 | EP1025053A4 Performance-based control system |
| 12/29/2004 | EP0814869B1 Radiotherapy apparatus for treating a patient |
| 12/29/2004 | CN1558099A Air-bleed transmission equipment of combustion turbine |
| 12/28/2004 | US6836086 Controlled starting system for a gas turbine engine |
| 12/28/2004 | US6835044 Draining and cooling system for gas turbine cushions |
| 12/28/2004 | US6834831 Hybrid solid oxide fuel cell aircraft auxiliary power unit |
| 12/28/2004 | US6834507 Convoluted seal with enhanced wear capability |
| 12/28/2004 | US6834505 Hybrid swirler |
| 12/28/2004 | US6834502 Combustion turbine power generation system and method of controlling the same |
| 12/28/2004 | US6834495 Multi-fan system separated core engine type turbofan engine |
| 12/25/2004 | CA2470570A1 Method for improving the wear resistance of a support region between a turbine outer case and a supported turbine vane |
| 12/25/2004 | CA2470268A1 Ventilation duct on the confluence plate of an afterburner |
| 12/23/2004 | WO2004111413A1 Water treatment and pressurization system for the adiabatic cooling of comburent air |
| 12/23/2004 | WO2004111412A1 Electric power supply equipment |
| 12/23/2004 | WO2004110639A2 Water distribution and vaporization assembly |
| 12/23/2004 | US20040258839 Heat treatment of silicon treated carbon/carbon composite to impregnate the initial coating layer, and cracks in the initial coating layer, with Si; thereby forming a silicon carbide layer and silicon layer |
| 12/23/2004 | US20040258539 Fluid machine |
| 12/23/2004 | US20040258523 Sealing assembly |
| 12/23/2004 | US20040258522 Methods and apparatus for assembling gas turbine engines |
| 12/23/2004 | US20040258520 Gas turbine engine |
| 12/23/2004 | US20040258517 Hot gas path assembly |
| 12/23/2004 | US20040258516 Methods and apparatus for supplying cooling fluid to turbine nozzles |
| 12/23/2004 | US20040255781 Filter arrangement and methods |
| 12/23/2004 | US20040255604 Heat extraction system for cooling power transformer |
| 12/23/2004 | US20040255596 Gas turbine |
| 12/23/2004 | US20040255594 Method and system for controlling gas turbine engine |
| 12/23/2004 | US20040255590 Differential geared turbine engine with torque modulation capability |
| 12/23/2004 | US20040255589 Gas turbine combustor and fuel supply method for same |
| 12/23/2004 | US20040255571 Cooling-air cooler for a gas-turbine plant and use of such a cooling-air cooler |
| 12/23/2004 | US20040255460 Nanophase composite duct assembly |
| 12/23/2004 | US20040255422 Methods and apparatus for injecting cleaning fluids into combustors |
| 12/22/2004 | EP1489360A1 Gasket assembly for igniter tube non-welded to the chamber wall |
| 12/22/2004 | EP1489358A2 A gas turbine combustor and fuel supply method for same |
| 12/22/2004 | EP1489340A1 Method of manufacturing axis seals, axis seals, axis seals members and rotary machine using axis seals |
| 12/22/2004 | EP1489269A2 Methods and apparatus for injecting cleaning fluids into combustors |
| 12/22/2004 | EP1489265A2 Methods and apparatus for supplying cooling fluid to turbine nozzles |
| 12/22/2004 | EP1488082A1 Modification of lubricant properties in a recirculating lubricant system |
| 12/22/2004 | EP1488080A1 Refrigeration power plant |
| 12/22/2004 | EP0926314B1 Seal structure for gas turbines |
| 12/22/2004 | EP0895031B1 Steam cooling type gas turbine combustor |
| 12/22/2004 | CN1180918C Method for making and repairing wing surface of integral propeller rotator |
| 12/21/2004 | US6833328 Method for removing a coating from a substrate, and related compositions |
| 12/21/2004 | US6833203 Thermal barrier coating utilizing a dispersion strengthened metallic bond coat |
| 12/21/2004 | US6832889 Integrated bridge turbine blade |
| 12/21/2004 | US6832486 Electrical machine |
| 12/21/2004 | US6832470 Recuperator configuration |
| 12/16/2004 | WO2004109064A1 Turbofan jet engine turbine case cooling valve |
| 12/16/2004 | WO2004108354A1 A turbine blade |
| 12/16/2004 | US20040251379 Rear fastening device for aircraft engine |
| 12/16/2004 | US20040251378 Variable position intake for an aircraft mounted gas turbine engine |
| 12/16/2004 | US20040250547 Differential pressure induced purging fuel injector with asymmetric cyclone |
| 12/16/2004 | DE19812834B4 Verfahren zum Zünden der Brenner von Brennkammern in Gasturbinenanlagen Method for igniting the burner combustion chambers in gas turbine systems |
| 12/16/2004 | DE102004016028A1 Verfahren und System zum Vermindern von Turbinenaustrittsturbulenz Method and system for reducing turbine exhaust turbulence |
| 12/15/2004 | EP1486654A2 Gas turbine with control box mounting device |
| 12/15/2004 | EP1486643A2 Gas turbine rotor cooling |
| 12/15/2004 | EP1486286A2 Process for repairing turbine components |
| 12/15/2004 | EP1485601A1 Multi-spool by-pass turbofan engine |
| 12/15/2004 | EP1485594A2 Air turbine starter with fluid flow control |
| 12/15/2004 | EP1485592A1 Gas turbine apparatus |
| 12/15/2004 | EP1485591A1 Compressed air energy storage system with a heat maintenance system |
| 12/15/2004 | EP1485289A1 Apparatus and method for variation of a wall skin |
| 12/15/2004 | EP1317608A4 Nested core gas turbine engine |
| 12/15/2004 | EP1307641B1 Method and device for converting thermal energy into mechanical work |
| 12/15/2004 | EP1227905A4 Multipiece core assembly for cast airfoil |
| 12/15/2004 | CN1554858A Valve rod for turbine valve and its heat treatment method |
| 12/15/2004 | CN1180126C Erosion-corrosion protective coating for high-temp. components |
| 12/14/2004 | US6830827 Alloy coating, method for forming the same, and member for high temperature apparatuses |
| 12/14/2004 | US6830437 Assembly containing a composite article and assembly method therefor |
| 12/14/2004 | US6830240 Methods and apparatus for securing components for manufacture |
| 12/14/2004 | US6829899 Jet fuel and air system for starting auxiliary power unit |
| 12/14/2004 | US6829898 Gas turbine combined plant and method of operating the same |
| 12/14/2004 | US6829883 Turbo fan gas turbine engine having a rotor containment assembly |
| 12/14/2004 | CA2342685C Cooling system for gas turbine combustor |
| 12/14/2004 | CA2315359C Method for obtaining thin, light and rigid metal parts |
| 12/14/2004 | CA2206154C Process and bearing mount allowing a turbine engine for aircraft to be maintained in operation after the occurrence of accidental imbalance in a rotor |
| 12/09/2004 | WO2004106718A1 A method for operation of a gas turbine group |
| 12/09/2004 | WO2004106161A1 Aircraft ground run-up enclosure |
| 12/09/2004 | US20040247922 Method of forming a ceramic coating on a substrate by electron-beam physical vapor deposition |
| 12/09/2004 | US20040247442 Turbine blade |
| 12/09/2004 | US20040247430 Turbomachine seal assembly and method therefor |
| 12/09/2004 | US20040247429 Gas turbine stator |
| 12/09/2004 | US20040244380 Methods and apparatus for operating gas turbine engines |
| 12/09/2004 | DE10323731A1 Exhaust turbocharger for an internal combustion engine with temperature-loaded turbine casing, has shield element to reduce heat transfer between turbine casing and surrounding area |
| 12/09/2004 | DE10250302B4 Drallerzeugungseinrichtung für einen Verdichter Swirler for a compressor |
| 12/09/2004 | DE102004005476A1 Verfahren zum Betrieb einer Gasturbogruppe A method of operating a gas turbine group |
| 12/08/2004 | EP1484489A2 Intake air cooling system for a gas turbine engine |
| 12/08/2004 | EP1484427A2 Top coating system for industrial turbine nozzle airfoils and other hot gas path components and related method |