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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06/25/2002 | US6408610 Method of adjusting gas turbine component cooling air flow |
06/25/2002 | US6408609 Method and apparatus for enhancing power output and efficiency of combustion turbines |
06/25/2002 | CA2278034C Gas turbine installation |
06/25/2002 | CA2257162C Gas turbine cooled moving blade |
06/22/2002 | CA2329555A1 Main propulsion engine system integrated with secondary power unit |
06/20/2002 | WO2002048527A1 Combustor turbine successive dual cooling |
06/20/2002 | WO2002048525A2 System to feed cooling air into a gas turbine rotor |
06/20/2002 | WO2002048509A1 A turbine arrangement and a method of operating a turbine arrangement |
06/20/2002 | WO2002048508A2 Turbine bucket cover and brush seal |
06/20/2002 | WO2002034391A3 Method of preparing a catalyst layer over a metallic surface of a recuperator |
06/20/2002 | WO2002021027A8 Heat-resistance magnetic silicone rubber body for brush seals in turbomachinery and methods of application |
06/20/2002 | US20020076573 Vapor deposition repair of superalloy articles |
06/20/2002 | US20020076541 Process for making ceramic matrix composite parts with cooling channels |
06/20/2002 | US20020076319 Gas turbine steam passage seal structure between blade ring and stationary blade |
06/20/2002 | US20020074965 Apparatus for robotically inspecting gas turbine combustion components |
06/20/2002 | US20020074804 Automatic turbogenerator restarting method and system |
06/20/2002 | US20020074240 Feedback controlled airfoil stripping system with integrated water management and acid recycling system |
06/20/2002 | US20020074017 Cleaning of oxides and dirt from internal cooling air passages of airfoils by immersion in an inorganic hydroxide stripping solution for a short time |
06/20/2002 | US20020073850 Filter arrangement and methods |
06/20/2002 | US20020073788 Methods for robotically inspecting gas turbine combustion components |
06/20/2002 | US20020073714 Gas turbine engine with offset shroud |
06/20/2002 | US20020073713 Method and apparatus for compressing gaseous fuel in a turbine engine |
06/20/2002 | US20020073712 Subatmospheric gas-turbine engine |
06/20/2002 | US20020073711 Combustor rear facing step hot side contour method |
06/20/2002 | US20020073710 Method of cooling gas only nozzle fuel tip |
06/20/2002 | US20020073709 Gas only nozzle |
06/20/2002 | US20020073688 Annular recuperator |
06/20/2002 | US20020073687 Liquid fuel reverse purge |
06/19/2002 | EP1215421A2 Turbine rotor-stator leaf seal and related method |
06/19/2002 | EP1215306A1 Coating removal system |
06/19/2002 | EP1215183A1 Ceramic matrix composite parts with channels and process of making the same |
06/19/2002 | EP1215005A2 Electrochemical machining process for forming surface roughness elements on a gas turbine shroud |
06/19/2002 | EP1214172A1 Laser cladding a turbine engine vane platform |
06/19/2002 | EP0898639B1 Turbomachine rotor cooling |
06/19/2002 | EP0894186B1 Fuel heating system used in conjunction with steam cooled combustors and transitions |
06/19/2002 | CN1354820A Turbo-machine comprising sealing system for rotor |
06/19/2002 | CN1354819A Gas turbine engine |
06/19/2002 | CN1354066A Method for repairing curved section of nozzle guide device |
06/19/2002 | CA2364593A1 Cleaning of internal passages of airfoils |
06/18/2002 | US6406561 One-step noble metal-aluminide coatings |
06/18/2002 | US6406254 Cooling circuit for steam and air-cooled turbine nozzle stage |
06/18/2002 | US6405977 Modular air intake duct for aircraft |
06/18/2002 | US6405538 Gas turbine, gas turbine apparatus, and refrigerant collection method for gas turbine moving blades |
06/18/2002 | US6405524 Apparatus for decreasing gas turbine combustor emissions |
06/18/2002 | US6405520 Gas and steam turbine plant and method for cooling a coolant of a gas turbine of such a plant |
06/13/2002 | WO2002046739A1 A novel method for chromatographic finger printing and standardization of single medicines and formulations |
06/13/2002 | WO2002046589A1 Turbine equipment |
06/13/2002 | WO2002046498A2 Method of removing ceramic coatings |
06/13/2002 | US20020071764 Turbine bucket cover and brush seal |
06/13/2002 | US20020071760 Variable stator vane bushing |
06/13/2002 | US20020070716 Electrical system for turbine/alternator on common shaft |
06/13/2002 | US20020070075 Silencing apparatus, notably for a turbo engine |
06/13/2002 | US20020069647 Turbine engine fuel supply system |
06/13/2002 | US20020069644 Combustor turbine successive dual cooling |
06/13/2002 | US20020069637 Speed-reducing gear unit to absorb the axial loads generated by a turbojet fan |
06/13/2002 | CA2424363A1 A novel method for chromatographic finger printing and standardization of single medicines and formulations |
06/12/2002 | EP1213539A1 Gas turbine combustor, gas turbine, and jet engine |
06/12/2002 | EP1213446A2 Variable stator vane bushing |
06/12/2002 | EP1213445A1 Reducing gear balancing the forces generated by the fan of a turbo machine |
06/11/2002 | US6403157 Masking fixture and method |
06/11/2002 | US6403020 Method for firing ceramic cores |
06/11/2002 | US6402469 Fan decoupling fuse |
06/11/2002 | US6402466 Leaf seal for gas turbine stator shrouds and a nozzle band |
06/11/2002 | US6402458 Clock turbine airfoil cooling |
06/11/2002 | US6401448 System for mounting aircraft engines |
06/11/2002 | US6401446 Valve apparatus for providing shutoff and overspeed protection in a gas turbine fuel system |
06/11/2002 | CA2230347C Steam cooled gas turbine system |
06/06/2002 | WO2002044539A1 Bypass duct fan noise reduction assembly |
06/06/2002 | WO2002044538A2 Device for centring a tube in a turbine shaft |
06/06/2002 | WO2002044526A1 Bladed rotor disc side-plate and corresponding arrangement |
06/06/2002 | US20020066275 Process and device for preheating suction air by waste heat in power engines |
06/06/2002 | US20020066272 Gas turbine combustor, gas turbine, and jet engine |
06/06/2002 | US20020066267 Process and device for collecting air, and engine associated therewith |
06/06/2002 | US20020066265 Intake-air cooling type gas turbine power equipment and combined power plant using same |
06/05/2002 | EP1211406A1 Methods and apparatus for sealing gas turbine engine variable nozzles |
06/05/2002 | EP1211401A1 Fuel gas moisturization system control |
06/05/2002 | EP1211387A1 Internal stator shroud |
06/05/2002 | EP1211385A2 Making cooling channels in turbine components |
06/05/2002 | EP1211381A1 Cover plate for a bladed rotor disk |
06/05/2002 | EP0910731B1 Method and device for generation of mechanical work and, if desired, heat in an evaporative gas turbine process |
06/04/2002 | US6399217 Article surface with metal wires and method for making |
06/04/2002 | US6398518 Method and apparatus for increasing the efficiency of a multi-stage compressor |
06/04/2002 | US6398503 High temperature component, gas turbine high temperature component and manufacturing method thereof |
06/04/2002 | US6398487 Methods and apparatus for supplying cooling airflow in turbine engines |
06/04/2002 | US6398486 Steam exit flow design for aft cavities of an airfoil |
06/04/2002 | US6398483 Protection device for protecting control mechanism of inlet guide-vanes of turbojet engine |
06/04/2002 | US6397604 Cooling supply system for stage 3 bucket of a gas turbine |
06/04/2002 | US6397603 Conbustor having a ceramic matrix composite liner |
06/04/2002 | US6397602 Fuel system configuration for staging fuel for gas turbines utilizing both gaseous and liquid fuels |
06/04/2002 | US6397578 Gas turbine power plant |
06/04/2002 | US6397575 Apparatus and methods of reheating gas turbine cooling steam and high pressure steam turbine exhaust in a combined cycle power generating system |
05/30/2002 | WO2002042623A2 Fan-stator interaction tone reduction |
05/30/2002 | WO2002042611A1 Transient turbine exhaust temperature control for a turbogenerator |
05/30/2002 | WO2002042610A2 Metallic honeycomb cellular seal-structure for a turbomachine |
05/30/2002 | WO2002042150A1 Aircraft deicer |
05/30/2002 | US20020064459 Retention sleeve for a thermal medium carrying tube in a gas turbine |
05/30/2002 | US20020064455 Methods and apparatus for sealing gas turbine engine variable nozzles |
05/30/2002 | US20020064453 Bypass duct fan noise reduction assembly |
05/30/2002 | US20020063479 Active turbine combustion parameter control system and method |
05/30/2002 | US20020063114 Device for cleaning an article |