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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07/27/1999 | US5927644 Double failsafe engine mount |
07/27/1999 | US5927067 Self-cleaning augmentor fuel manifold |
07/27/1999 | CA2189743C Annular bearing compartment |
07/27/1999 | CA2189641C Bearing support housing |
07/21/1999 | EP0930418A2 Gas turbine rotor blade |
07/21/1999 | EP0929734A1 Gas turbine airfoil cooling |
07/20/1999 | US5924279 Engine intake design |
07/20/1999 | US5924275 Center burner in a multi-burner combustor |
07/14/1999 | EP0928881A1 Turbomachine with concentric shafts which in case of a shaft rupture have a braking action on each other |
07/14/1999 | EP0928880A1 Tip shroud for moving blades of gas turbine |
07/14/1999 | EP0928396A1 Thermal shield component with cooling fluid recirculation and heat shield arrangement for a component circulating hot gas |
07/14/1999 | EP0928367A1 Method of mixing two fluid flows at a compressor |
07/14/1999 | EP0928364A1 Method of compensating pressure loss in a cooling air guide system in a gas turbine plant |
07/14/1999 | EP0928326A1 DIMETHYL ETHER FUEL AND METHOD OF GENERATING POWER IN A DRY LOW NOx COMBUSTION SYSTEM |
07/13/1999 | US5923003 Extended reaction acoustic liner for jet engines and the like |
07/13/1999 | US5921751 Coating scheme to contain molten material during gas turbine engine fires |
07/08/1999 | WO1999033701A2 Self-adjusting air intake |
07/07/1999 | EP0927815A2 Fan case liner |
07/07/1999 | EP0927814A1 Tip shroud for cooled blade of gas turbine |
07/07/1999 | EP0826076B1 Metal component with a high-temperature protection coating system and a method of coating the component |
07/06/1999 | US5919031 Coolable blade |
07/06/1999 | US5918679 Fire safety system |
07/06/1999 | US5918628 Multi-stage check valve |
07/06/1999 | US5918466 Coal fuel gas turbine system |
07/06/1999 | US5918458 System and method of providing clean filtered cooling air to a hot portion of a gas turbine engine |
07/01/1999 | WO1999032771A1 Pulse width modulated low pressure fuel control |
07/01/1999 | WO1999032770A1 Peak compressor bleed pressure storage for extended fuel nozzle purging of a microturbine power generating system |
07/01/1999 | WO1999032768A1 Microturbine power generating system including auxiliary compressor |
07/01/1999 | WO1999032763A1 A LOW NOx CONDITIONER SYSTEM AND PROCESS FOR A MICROTURBINE POWER GENERATING SYSTEM |
07/01/1999 | WO1999032761A1 Cooling arrangement for turbine rotor |
07/01/1999 | WO1999032357A1 Turbomachine-driven environmental control system |
07/01/1999 | DE19758160A1 Divided housing connection for apparatus and machines e.g. gas or steam turbines |
06/30/1999 | EP0926324A1 Cooling structure for combustor tail pipes |
06/30/1999 | EP0926323A2 Steam cooled gas turbine |
06/30/1999 | EP0926315A2 Turbine seal |
06/30/1999 | EP0926314A1 Seal structure for gas turbines |
06/30/1999 | EP0926313A1 Structure and method for holding inserts for stationary blades of gas turbine |
06/30/1999 | EP0926261A2 Coatings for gas turbine compressor components |
06/30/1999 | EP0926255A1 Thermal spray coating process for rotor blade tips |
06/30/1999 | EP0926254A2 Thermal coating composition |
06/30/1999 | EP0925844A2 Method for applying a coating to the tip of a flow directing assembly |
06/30/1999 | EP0925444A1 Gas turbine engine starting system and method |
06/30/1999 | EP0830501A4 Torch assembly |
06/30/1999 | CN1221069A Gas-turbine installation |
06/30/1999 | CN1221067A Columnar zirconium oxide abrasive coating for gas turbine engine seal system |
06/29/1999 | US5916638 Method for applying a coating to the tip of a flow directing assembly |
06/29/1999 | US5916126 Starting fuel control system for a staged combustor |
06/29/1999 | US5915917 Compressor stall and surge control using airflow asymmetry measurement |
06/29/1999 | US5915697 Flexible cloth seal assembly |
06/29/1999 | US5915651 Reverse thrust inlet vortex inhibitor |
06/29/1999 | US5915403 For channeling airflow to a turbofan engine of a subsonic aircraft |
06/24/1999 | WO1999031415A1 Noise attenuating device for butterfly valves |
06/24/1999 | DE19756097A1 Turbocharger with vertical shaft |
06/23/1999 | EP0924412A1 Method of operating a gas turbo group |
06/23/1999 | EP0924411A2 Fluid manifold |
06/23/1999 | EP0924410A1 Gas/steam power plant |
06/23/1999 | EP0924409A2 Heat exchanger system for a gas turbine engine |
06/23/1999 | EP0924408A2 Method for cooling a component of a gas turbine engine |
06/23/1999 | EP0924407A2 Inlet and outlet module for a gas turbine engine heat exchanger |
06/23/1999 | EP0924406A1 Gas turbine with steam generator and recuperator arranged in parallel in the exhaust gas flow |
06/23/1999 | EP0924389A2 Variable inlet guide vane for a gas turbine engine |
06/23/1999 | CN1220341A Gas/steam generating equipment |
06/22/1999 | US5914059 Method of repairing metallic articles by energy beam deposition with reduced power density |
06/22/1999 | US5913808 Turbine engine intake with gas mixer |
06/22/1999 | US5913807 Turbojet engine start system |
06/22/1999 | US5913658 Removable inner turbine shell with bucket tip clearance control |
06/19/1999 | CA2225263A1 Fluid manifold |
06/17/1999 | WO1999030019A1 Flow divider programmed by pressurizing valve |
06/17/1999 | DE19753264C1 Gasturbinenanlage und Verfahren zum Betreiben einer Gasturbinenanlage sowie Gas- und Dampfturbinenanlage Gas turbine system and method of operating a gas turbine plant and gas and steam turbine plant |
06/16/1999 | EP0922842A1 Hot air diffuser for jet engine intake fairing with de-icing circuit |
06/16/1999 | EP0654162B1 Process for detecting fouling of an axial compressor |
06/16/1999 | EP0654161B1 Process and device for monitoring and for controlling of a compressor |
06/15/1999 | US5911680 Mounting/demounting device for combustor for use in gas turbine |
06/15/1999 | US5911679 Variable pitch rotor assembly for a gas turbine engine inlet |
06/10/1999 | WO1999028608A1 Preheating of intake air for gas turbine plants |
06/10/1999 | WO1999015402A3 Starter system and method for aircraft gas turbine engine |
06/10/1999 | DE19807940A1 Pressurised, pulverised coal fired gas-turbine plant |
06/09/1999 | EP0921335A2 Gas turbine spindle bolt seal device |
06/09/1999 | EP0921293A1 Hot air exhaust device for a jet engine air intake fairing with de-icing circuit |
06/09/1999 | EP0921278A1 Sealing structure for first stage stator blade of gas turbine |
06/09/1999 | EP0921071A2 Noise suppression system for a jet engine |
06/09/1999 | EP0819209B1 Method of operating a waste-heat steam generator, and a waste-heat steam generator operated by this method |
06/09/1999 | CN1219218A Closed-loop air cooling system for a turbine engine |
06/09/1999 | CN1219217A Process and apparatus for achieving power augementation in gas turbines via wet compression |
06/08/1999 | US5910094 For discouraging the passage of flame between two regions |
06/03/1999 | WO1999027304A1 Combustion chamber and method for cooling a combustion chamber with vapour |
06/02/1999 | EP0919845A1 Inspection system of internal zones of a machine by optical fiber endoscopy |
06/02/1999 | EP0919773A1 Flame detector for combustor |
06/02/1999 | EP0919707A1 Cooling-air cooling unit for gas turbines |
06/02/1999 | EP0919706A2 Recovery type steam cooled gas turbine |
06/02/1999 | EP0919701A1 Sealing structure for joint surfaces of flanges of gas turbine |
06/02/1999 | EP0919700A1 Device for sealing gas turbine stator blades |
06/02/1999 | EP0919699A2 Columnar zirconium oxide abrasive coating for a gas turbine engine seal system |
06/02/1999 | DE19751299A1 Brennkammer sowie Verfahren zur Dampfkühlung einer Brennkammer Combustion chamber and method for cooling a steam chamber |
06/01/1999 | USRE36215 Swirl anti-ice system |
06/01/1999 | US5907949 Starting fuel control method for a turbine engine |
05/26/1999 | EP0918151A1 Device and method to preheat fuel for a combustor |
05/26/1999 | EP0918150A1 Deicing device for the air inlet fairing of a jet engine |
05/26/1999 | EP0918149A1 Protection device for the air inlet of a jet engine which is provided with an anti-icing system |
05/26/1999 | EP0799366B1 A system for repairing damaged gas turbine engine airfoils |