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)
09/2000
09/14/2000WO2000025067A3 Fuel air mixer for a radial dome in a gas turbine engine combustor
09/14/2000DE10010117A1 Compression system for turbochargers and gas turbine machines has a compressor and a sand-cast compressed air outlet in which the flow path is coated with heat-resistant material, e.g. epoxy resin
09/14/2000CA2366013A1 Method of operation of a gas turbine engine power plant and a gas turbine engine power plant
09/12/2000US6116018 Gas turbine plant with combustor cooling system
09/12/2000US6116017 Combined cycle power plant with steam cooled gas turbine
09/12/2000US6116016 Gas turbine apparatus using fuel containing vanadium
09/12/2000CA2214826C Gas turbine stationary blade
09/08/2000WO2000051761A1 Method and apparatus for production of a cast component
09/08/2000WO2000008326A9 Methods and apparatus for water injection in a turbine engine
09/08/2000CA2714871A1 Method and apparatus for production of a cast component
09/08/2000CA2663076A1 Method and apparatus for production of a cast component
09/07/2000DE19856843C1 Pipe connection checking device, e.g. for correct pipe connection of nuclear reactor neutron flux measuring system, comprises sleeve on one pipe which can slide over body on other pipe when sleeve and body shapes match
09/06/2000EP1033484A2 Gas turbine cooling system
09/06/2000EP1033477A2 Gas turbine shroud
09/06/2000EP1033476A2 Heat exchange flow circuit for a turbine rotor
09/06/2000EP1032811A1 Velocity adaptive control test system
09/06/2000EP1032791A1 Combustion chamber and method for cooling a combustion chamber with vapour
09/06/2000EP1032779A1 Planetary gear
09/06/2000EP0724658B1 Protective coating
09/06/2000CN1265448A Compressor system and method for reducing cooling airflow
09/05/2000US6112514 Fan noise reduction from turbofan engines using adaptive Herschel-Quincke tubes
08/2000
08/30/2000EP1031717A2 Gas turbine engine
08/30/2000EP1031715A2 Gas turbine engine bearing arrangement
08/30/2000EP1031702A1 Automatic clearance control system for gas turbine stationary blade
08/30/2000EP1031546A1 Method to prevent recession loss of silica and silicon-containing materials in combustion gas environments
08/29/2000US6109873 Shield for masking a flow directing assembly
08/29/2000US6109783 Optic pyrometer for gas turbines
08/29/2000US6109019 Steam cooled gas turbine system
08/24/2000WO2000028191A3 Gas turbine power generating system including a battery source for supplying startup power
08/24/2000WO2000022287A3 Gas turbine engine
08/23/2000EP1029104A1 GAZ JET PVD METHOD FOR PRODUCING A LAYER WITH MoSi 2?
08/22/2000US6107693 Self-contained energy center for producing mechanical, electrical, and heat energy
08/22/2000US6106959 For use in gas turbine applications
08/22/2000US6106229 Heat exchanger system for a gas turbine engine
08/22/2000US6105372 Gas turbine combustor
08/22/2000US6105371 Control of cooling flows for high-temperature combustion chambers having increased permeability in the downstream direction
08/22/2000US6105370 Method and apparatus for rejecting waste heat from a system including a combustion engine
08/22/2000US6105363 Cooling scheme for turbine hot parts
08/22/2000US6105362 Combined cycle power plant with gas turbine cooling system
08/17/2000WO2000047874A1 Method of generating power using an advanced thermochemical recuperation cycle
08/17/2000WO2000047792A1 Method for producing fibre reinforced metallic components
08/16/2000EP1028237A2 Gas turbine engine
08/16/2000EP1028230A1 Cooled gas turbine component with adjustable cooling
08/16/2000EP1027560A1 Fuel nozzle for gas turbine engine
08/15/2000US6103402 The power density is reduced and the interaction time is increased, which allows for a significant increase in temperature of the substrate immediately adjacent the molten pool at the time that solidifiction occurs, reduces cracking
08/15/2000US6102656 Segmented abradable ceramic coating
08/15/2000US6102577 Isolated oil feed
08/15/2000US6101982 Method and apparatus for preheating the fuel for a firing plant
08/10/2000WO2000046488A2 Turbine engine
08/10/2000WO2000046420A1 Thermal barrier coating resistant to sintering
08/10/2000DE10005250A1 Fiber-reinforced metal component of complicated shape, e.g. a turbine blade, is produced by plastic shaping and then diffusion welding of an assembly of loose metal-coated silicon carbide fibers between metal pieces
08/09/2000EP1025398A1 Combustor with independently controllable fuel flow to different stages
08/09/2000EP1025350A1 Device, method and application in connection with a turbomachine and pumping and lubricating arrangement in connection with such a machine
08/09/2000EP1025053A1 Performance-based control system
08/08/2000US6099253 Gas turbine rotor blade
08/08/2000US6099244 Cooled stationary blade for a gas turbine
08/08/2000US6098398 Low temperature hydrogen combustion turbine
08/08/2000US6098397 Combustor for a low-emissions gas turbine engine
08/08/2000US6098396 Internal combustion engine having a catalytic reactor
08/08/2000US6098395 Closed-loop air cooling system for a turbine engine
08/03/2000WO2000050748A1 Combustion unit for combusting a liquid fuel and a power generating system comprising such combustion unit
08/03/2000WO2000044525A1 Repair of turbine exhaust case
08/03/2000WO2000020740B1 Gas turbine engine
08/03/2000CA2358941A1 Repair of turbine exhaust case
08/02/2000EP1024250A2 Rotating diffuser for pressure recovery in a steam cooling circuit of a gas turbine
08/02/2000EP1023526A1 Gas and steam turbine installation and method for operating an installation of this type
08/01/2000US6095793 Dynamic control system and method for catalytic combustion process and gas turbine engine utilizing same
08/01/2000US6095791 Fuel injector arrangement; method of operating a fuel injector arrangement
08/01/2000US6095756 High-CR precision casting materials and turbine blades
08/01/2000US6095751 Seal device between fastening bolt and bolthole in gas turbine disc
08/01/2000US6094907 Jet engine and method for reducing jet engine noise by reducing nacelle boundary layer thickness
08/01/2000US6094905 Cooling apparatus for gas turbine moving blade and gas turbine equipped with same
08/01/2000CA2215625C Spring seal device for combustor
08/01/2000CA2206983C Burner replacing system
07/2000
07/27/2000WO2000043658A1 Gas turbine generating method and generator
07/27/2000WO2000043642A1 Improved bushing for a jet engine vane
07/27/2000WO2000028189A8 Individually replaceable and reversible insertable steam turbine nozzle
07/27/2000WO2000020748A3 Fan noise reduction from turbofan engines using adaptive herschel-quincke tubes
07/27/2000WO2000009875A9 Nozzles for water injection in a turbine engine
07/27/2000DE19924067A1 Entrance or feed air-treatment esp. for gas-and-steam turbine plant
07/27/2000DE19902437A1 Rapid running-up and load raising process for gas turbine plant, involving raising fuel mass flow supplied to plant and at same time supplying auxiliary working medium to turbine
07/27/2000CA2652851A1 Improved bushing for a jet engine vane
07/26/2000EP1022436A2 Gas turbine engine seals
07/26/2000EP1022435A2 Internal cooling circuit for gas turbine bucket
07/26/2000EP1022434A2 Gas turbine blade cooling configuration
07/26/2000EP1022433A2 Debris trap in a turbine cooling system
07/26/2000EP0654163B1 Process and device for monitoring vibrational excitation of an axial compressor
07/25/2000US6092621 Methods and apparatus for suppressing engine test cell howl
07/25/2000US6092590 Method and evaporator device for evaporating a low temperature liquid medium
07/25/2000US6092546 Fuel flow divider and pressurizing valve for gas turbine
07/25/2000US6092361 Recuperator for gas turbine engine
07/25/2000US6092360 Auxiliary power unit passive cooling system
07/20/2000WO2000042242A1 Electrochemical stripping of turbine blades
07/20/2000DE19941685C1 Method of increasing pressure of gas supplied from compressor in power station with booster pump
07/19/2000EP1020637A1 Fuel circuit with protected main stream filter
07/19/2000EP1019658A1 Combustor cooling method
07/18/2000US6089826 Turbulator for gas turbine cooling blades
07/18/2000US6089825 Abradable seal having improved properties and method of producing seal
07/18/2000US6089824 Introduced in protection element against bird ingestion into aircraft turbines
07/18/2000US6089822 Gas turbine stationary blade