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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09/01/2004 | CN1526143A Brayton cycle nuclear power plant and a method of starting the brayton cycle |
09/01/2004 | CN1526050A Method for operating a burner of a gas turbine and a power plant |
09/01/2004 | CN1525055A Methods and apparatus for assessing gas turbine damage |
09/01/2004 | CN1525049A Turbine nozzle segment cantilevered mount |
09/01/2004 | CN1525048A Gas turbine engine turbine nozzle bifurcated impingement baffle |
09/01/2004 | CN1525047A Turbine bucket damper pin |
08/31/2004 | US6785633 Method and apparatus for assessing performance of combined cycle power-plants |
08/31/2004 | US6783324 Compressor bleed case |
08/31/2004 | US6782692 Fuel metering unit with two integrated outlet ports |
08/31/2004 | US6782620 Methods for replacing a portion of a combustor dome assembly |
08/31/2004 | CA2272488C Cooling steam control method for combined cycle power generation plants |
08/31/2004 | CA2264076C Gas turbine moving blade tip shroud |
08/28/2004 | CA2455673A1 Methods and apparatus for assessing gas turbine engine damage |
08/26/2004 | WO2004072453A1 Method for operating a gas turbine group |
08/26/2004 | WO2004072452A1 Compressed air energy storage and method of operation |
08/26/2004 | WO2004072450A1 Method for producing gas turbines and gas turbine assembly |
08/26/2004 | US20040164059 Method for fabricating, modifying or repairing of single crystal or directionally solidified articles |
08/26/2004 | US20040163888 Honeycomb core acoustic unit with metallurgically secured deformable septum, and method of manufacture |
08/26/2004 | US20040163678 comprises coupling a nozzle assembly against the combustor, wherein the nozzle assembly includes an inlet end, a discharge end, a hollow nozzle body extending therebetween, and a centerbody positioned within the nozzle body |
08/26/2004 | US20040163536 Direct turbine air chiller/scrubber system |
08/26/2004 | US20040163394 Coolant recovery type gas turbine |
08/26/2004 | US20040163391 Method for operating a partially closed, turbocharged gas turbine cycle, and gas turbine system for carrying out the method |
08/26/2004 | US20040163390 Secondary air induction system |
08/25/2004 | EP1450005A1 Turbine discs cooling device |
08/25/2004 | EP1448875A1 Gas turbine arrangement |
08/25/2004 | CN1524160A Securing system for the rotor blades of axial flow turbo engines |
08/24/2004 | US6782317 Apparatus and method for testing jet engine fuel manifold flow distribution |
08/24/2004 | US6782314 Method of detecting in-range engine sensor faults |
08/24/2004 | US6780089 Method and apparatus for removing a predetermined amount of material from a bottom portion of a dovetail slot in gas turbine engine disk |
08/24/2004 | US6779973 Gas turbine |
08/24/2004 | US6779972 Flowpath sealing and streamlining configuration for a turbine |
08/24/2004 | US6779967 Device for air mass flow control |
08/24/2004 | US6779771 Dual extrusion snap closed ceiling sign hanger |
08/24/2004 | US6779336 Cooled variable geometry exhaust nozzle |
08/24/2004 | US6779332 Gas turbine |
08/24/2004 | US6779268 Outer and inner cowl-wire wrap to one piece cowl conversion |
08/24/2004 | CA2457970A1 Methods and apparatus for washing gas turbine engine combustors |
08/24/2004 | CA2263516C Cooled gas turbine blade |
08/24/2004 | CA2232169C Twin-spool turboprop powerplant with balanced pressure regulation |
08/19/2004 | WO2004070171A1 Gas turbine engine |
08/19/2004 | WO2004069749A2 Improved configuration and process for carbonyl removal |
08/19/2004 | WO2004069381A1 Configuration and process for carbonyl removal |
08/19/2004 | US20040161339 Gas turbine engine nose cone |
08/19/2004 | US20040161336 Annular platform for a nozzle of a low-pressure turbine of a turbomachine |
08/19/2004 | US20040161335 Coolant recovery type gas turbine |
08/19/2004 | US20040161334 Device for cooling turbine disks |
08/19/2004 | US20040161331 System for decoupling a fan from a turbojet by means of an explosive charge |
08/19/2004 | US20040160061 Gas-turbine engine with catalytic reactor |
08/19/2004 | US20040159552 coating the surface of a single crystal or directionally solidified article, especially on local areas of a gas turbine component; uniformity; good oxidation and fatigue resistance; may be used as a repair process |
08/19/2004 | US20040158984 Method for manufacturing a stator or rotor component |
08/19/2004 | DE10392154T5 Turbinenanlage und Kombikraftwerk sowie Turbinenbetriebsverfahren Turbine plant and combined cycle power plant and turbine operating procedures |
08/19/2004 | DE102004005477A1 Verfahren zum Betrieb einer Gasturbogruppe A method of operating a gas turbine group |
08/18/2004 | EP1447543A2 Gas turbine engine bearing support |
08/18/2004 | EP1447525A1 Method for producing turbines having turbine blades of different adjusted resonant frequencies and method of adjusting the resonant frequency of a turbine blade |
08/18/2004 | EP1447121A1 DUST COLLECTING FILTER, DUST COLLECTING DEVICE, AND INTAKE DEVICE OF GAS TURBINE |
08/18/2004 | EP1446566A1 Off loading clutch for gas turbine engine starting |
08/18/2004 | EP1446565A1 Turbine engine with air cooled turbine |
08/18/2004 | EP1446556A1 Turbine unit |
08/18/2004 | EP1082530B1 A rotor machine device |
08/17/2004 | US6776583 Turbine bucket damper pin |
08/17/2004 | US6776577 Method and apparatus to facilitate reducing steam leakage |
08/17/2004 | US6776573 Bladed rotor disc side-plate and corresponding arrangement |
08/17/2004 | US6776213 System for casting a metal article |
08/17/2004 | US6776002 Magnetically coupled integrated power and cooling unit |
08/17/2004 | US6775990 Methods and apparatus for regulating gas turbine engine fluid flow |
08/12/2004 | WO2004038196A3 Gas turbine engine starting system and method |
08/12/2004 | WO2003048545A9 Method and apparatus for achieving power augmentation in gas turbines using wet compression |
08/12/2004 | WO2003048544A9 Method and apparatus for achieving power augmentation in gas turbines using wet compression |
08/12/2004 | US20040157081 Protective coatings; oxidation resistance |
08/12/2004 | US20040156739 gas turbine engine components; During solidification, aluminum matrix excludes gadolinium and other rare earth elements from aluminum matrix, forming eutectic gadolinium-containing dispersoids that strengthen the aluminum matrix |
08/12/2004 | US20040156722 Method and apparatus to facilitate reducing steam leakage |
08/12/2004 | US20040156708 Turbine balancing |
08/12/2004 | US20040154310 Rotary internal combustion engine |
08/12/2004 | US20040154309 Turbine engine |
08/12/2004 | US20040154302 Nozzle assembly with flow divider and ecology valve |
08/12/2004 | US20040154300 Apparatus for reducing gas turbine engines emissions |
08/12/2004 | US20040154152 Test model for a gas turbine combustor dome and method of fabricating |
08/12/2004 | DE102004003354A1 Turbinen-Laufschaufel und Gasturbine Turbine blade and gas turbine |
08/12/2004 | DE102004002888A1 Gasturbinen-Endrohrdichtung und diese verwendende Gasturbine Gas turbine exhaust tip seal and use this gas turbine |
08/12/2004 | DE102004002303A1 Verfahren zum Zweifach- oder Mehrfachbeschichten eines Kohlenstoff/Kohlenstoff-Verbundwerkstoffes A method for double or multiple coating a carbon / carbon composite material |
08/11/2004 | EP1445569A2 Heat exchanger |
08/11/2004 | EP1445540A1 Cooled purging fuel injectors |
08/11/2004 | EP1445539A1 Differential pressure induced purging fuel injectors |
08/11/2004 | EP1445466A2 Compact afterburners for gas turbine engines |
08/11/2004 | EP1445465A1 Combination of core engine with ramjet engine incorporating swirl augmented combustion |
08/11/2004 | EP1445464A1 Methods and apparatus for modeling pulsed detonation gas turbine engines |
08/11/2004 | EP1445428A1 Turbine and compressor assembly having a self-actuated air bearing flow shut-off valve |
08/11/2004 | EP1445425A2 A gas turbine blade comprising a ceramic thermal barrier coating |
08/11/2004 | EP1445424A2 Microcircuit cooling for a turbine blade tip |
08/11/2004 | EP1445422A2 Turbine balancing |
08/11/2004 | EP1445421A1 Apparatus for the ventilation of a high pressure turbine rotor |
08/11/2004 | EP1445057A1 Turbine element manufacture |
08/11/2004 | EP1444658A2 Fault management system for gas turbine engines |
08/11/2004 | EP1444491A2 Vibration monitoring system for gas turbine engines |
08/11/2004 | EP1444428A1 Method and apparatus for adaptive acceleration schedules in gas turbine engine control systems |
08/11/2004 | EP1444427A1 Method for ignition and start up of a turbogenerator |
08/11/2004 | EP1444417A1 High pressure turbine blade cooling scoop |
08/11/2004 | EP1444388A1 Mcraly-coating |
08/11/2004 | EP1394390A9 Gas turbine plant |
08/11/2004 | EP1278947A4 Oxygen separation method integrated with gas turbine |