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