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