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)
02/2000
02/02/2000EP0975435A1 Modular coating fixture
02/02/2000CN1243194A Heat-barrier coating series
02/02/2000CN1048913C Pulse combusted acoustic agglomeration method
02/01/2000US6019579 Gas turbine rotating blade
02/01/2000US6019575 Erosion energy dissipater
02/01/2000US6019574 Mismatch proof variable stator vane
02/01/2000US6019573 Heat recovery type gas turbine
02/01/2000US6019397 Hydraulic fittings for a hydraulic unit with a security connection system
02/01/2000US6018950 Combustion turbine modular cooling panel
02/01/2000US6018942 Combined cycle power station with gas turbine cooling air cooler
02/01/2000US6018941 Electric starter system for turbine aircraft engines
02/01/2000CA2209850C Heat recovery type gas turbine rotor
01/2000
01/27/2000WO2000004309A1 Sealing system, especially for a rotary machine
01/26/2000EP0974789A1 Method of operating the combustion chamber of a liquid-fuel gas turbine
01/26/2000EP0974737A1 Combined cycle power plant
01/26/2000EP0974735A2 Dimpled impingement baffle
01/26/2000EP0974733A2 Turbine nozzle having purge air circuit
01/26/2000EP0974515A2 Aircraft airconditioning energy recovery device
01/26/2000CN1242883A Electrical system for turbin/alternator on common shaft
01/25/2000USRE36524 Steam attemperation circuit for a combined cycle steam cooled gas turbine
01/25/2000US6016658 Low emissions combustion system for a gas turbine engine
01/25/2000CA2012243C A gas turbine engine rotor assembly
01/19/2000EP0973021A1 Procedure for testing of fuel passages
01/19/2000EP0972992A2 Combustor liner
01/19/2000EP0972922A2 Modified bottoming cycle for cooling inlet air to a gas turbine combined cycle plant
01/19/2000EP0972853A1 Article having a thermal barrier coating based on a phase-stable solid solution of two ceramics and apparatus and method for making the article
01/18/2000USRE36497 Combined cycle with steam cooled gas turbine
01/18/2000US6014863 Waste processing system and fuel reformer used in the waste processing system
01/18/2000US6014855 Light hydrocarbon fuel cooling system for gas turbine
01/13/2000WO2000001934A1 Operating a gas turbine with supplemental compressed air
01/13/2000WO2000001929A1 Combined cycle power generating system
01/12/2000EP0971111A1 Particle trap for a turbomachine
01/12/2000EP0835364A4 Non-polluting, open brayton cycle automotive power unit
01/12/2000EP0832398B1 Catalytic combustion chamber for a gas turbine
01/11/2000US6012684 Braze bracket for a turbine engine
01/11/2000US6012533 Fire safety system
01/11/2000US6012281 Noise suppressing fluid mixing system for a turbine engine
01/11/2000US6012279 Gas turbine engine with water injection
01/07/2000WO2000001928A1 Gas turbine blade
01/06/2000WO2000000773A1 A method for starting a combustion device
01/06/2000WO2000000772A2 DRY, LOW NOx CATALYTIC PILOT
01/06/2000WO2000000730A1 Driving mechanism with counter-rotating rotors
01/05/2000EP0969192A1 Method to equalize the fuel distribution in a gas turbine with several burners
01/05/2000EP0969116A1 Thermal barrier coating system with localized deposition of a bond coat
01/05/2000EP0968918A2 Auxiliary power unit passive cooling system
01/05/2000EP0968358A1 Pulse width modulated low pressure fuel control
01/05/2000EP0968355A1 Cooling supply manifold assembly for cooling combustion turbine components
01/05/2000EP0968317A1 Method of forming internal passages within articles and articles formed by same
01/05/2000DE19829088A1 Stromerzeugung in einem Verbundkraftwerk mit einer Gas- und einer Dampfturbine Generating electricity in a combined power plant with a gas and a steam turbine
01/05/2000DE19827961A1 Verfahren und Anordnung zum Konditionieren der Zuluft zu einer Gasturbinenanlage Method and apparatus for conditioning the supply air to a gas turbine plant
01/05/2000CN1240499A Ramjet engine for power generation
01/05/2000CN1240264A Pre-mixed fuel invector and operation method thereof
01/04/2000US6011617 System for inspecting internal zones of a machine by optical fibre endoscopy
01/04/2000US6010746 In-situ repair method for a turbomachinery component
01/04/2000US6009701 Ducted fan gas turbine engine having a frangible connection
01/04/2000CA2056480C Gas turbine engine fuel manifold
12/1999
12/30/1999DE19828562A1 Turbine plant with counter-rotating rotors
12/29/1999WO1999067614A1 Engine thrust with a strain gauge at a trunnion
12/29/1999WO1999067519A1 Device for compressing a gaseous medium and systems comprising such device
12/29/1999WO1999067518A1 Method and system for conditioning the inlet air of a gas turbine system
12/29/1999EP0967376A2 Air manifold system
12/29/1999EP0966594A1 Coal fuel gas turbine system
12/29/1999CN1240014A Abradable seal
12/28/1999US6007299 Recovery type steam-cooled gas turbine
12/23/1999DE19923431A1 Combustion engine containing catalytic reactor
12/22/1999EP0965391A1 Method and assembly for masking a flow directing assembly
12/22/1999EP0965390A1 Method and assembly for masking a flow directing assembly
12/22/1999EP0965389A1 Shield for masking a flow directing assembly
12/22/1999CA2275071A1 Air manifold system
12/21/1999US6004095 Reduction of turbomachinery noise
12/21/1999US6003302 Ramjet with adjustable working duct casings
12/21/1999US6003298 Steam driven variable speed booster compressor for gas turbine
12/16/1999WO1999064791A1 Combustor cooling method
12/16/1999WO1999064735A1 Filter construction resistant to the passage of water soluble materials and filtration method
12/16/1999WO1999064147A2 Microcomponent assembly for efficient contacting of fluid
12/15/1999EP0827566A4 Method and apparatus for increasing the operational capacity and efficiency of a combustion turbine
12/14/1999US6000909 Cooling medium path in gas turbine moving blade
12/14/1999US6000213 Combined cycle power plant
12/14/1999US6000210 Aircraft gas turbine engine with a liquid-air heat exchanger
12/09/1999WO1999063275A1 Film cooling strip for gas turbine engine combustion chamber
12/09/1999WO1999063274A1 Impingement and film cooling for gas turbine combustor walls
12/09/1999WO1999063271A1 A device for the supply of a liquid fuel to a burner member
12/09/1999WO1999063212A1 Exciter controlled by full authority digital electronic control (fadec) system
12/09/1999WO1999063211A1 Integral inertial particle separator for radial inlet gas turbine engine
12/09/1999WO1999063209A1 Oil supply system for a gas turbine
12/09/1999WO1999063205A1 Fluid deflecting and straining system
12/09/1999DE19825335A1 Procedure for operation of gas turbine
12/08/1999EP0963035A2 Turbogenerator/motor control system
12/08/1999EP0962659A2 Casing structure of a gas turbine
12/08/1999EP0962636A2 Compressor inlet air heating system for a gas turbine
12/08/1999EP0962545A1 Ceramic coating having a low thermal conductivity
12/08/1999CN1238019A Manufacture of paper
12/07/1999US5997247 Seal of stacked thin slabs that slide within reception slots
12/07/1999US5997245 Cooled shroud of gas turbine stationary blade
12/07/1999US5997244 Cooling airflow vortex spoiler
12/07/1999US5996334 Gas turbine engine having an external central frame
12/07/1999US5996331 Passive turbine coolant regulator responsive to engine load
12/02/1999WO1999061768A1 A rotor machine device
12/02/1999WO1999061767A1 Recuperator for gas turbine engine
12/02/1999WO1999061316A2 Biplanar scarfed nacelle inlet