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)
12/2000
12/26/2000US6164908 Sealing structure for first stage stator blade of gas turbine
12/26/2000US6164075 Steam cooling type gas turbine combustor
12/26/2000US6164058 Arrangement for damping combustion-chamber oscillations
12/26/2000US6164057 Gas turbine generator having reserve capacity controller
12/21/2000WO2000077363A1 Method for operating a turbomachine and corresponding turbomachine
12/21/2000WO2000077348A1 Apparatus for reducing combustor exit duct cooling
12/21/2000WO2000076695A1 Directional solidification method and apparatus
12/21/2000WO2000055485A3 Control of the inlet of an auxiliary power unit
12/21/2000DE19926949A1 Cooling arrangement for blades of gas turbine etc. has blades combined into groups with connected flow channels to form continuous coolant channel for cooling steam
12/21/2000DE19926891A1 Verfahren zum Betreiben einer Turbomaschine und Turbomaschine A method of operating a turbomachine, the turbomachine and
12/20/2000EP1061243A2 An apparatus for and a method of filtering a fluid
12/20/2000EP1061237A1 Seal ring for steam turbine
12/20/2000EP1061235A2 Axial seal system for a gas turbine steam-cooled rotor
12/20/2000EP1061234A2 Axial Thermal medium delivery tubes and retention plates for a gas turbine rotor
12/20/2000EP1032811A4 Velocity adaptive control test system
12/19/2000US6162347 Hollow turbine
12/19/2000US6162014 Turbine spline seal and turbine assembly containing such spline seal
12/19/2000US6162011 Method and apparatus for stabilizing an intake air flow of a ground-based turbine engine
12/19/2000US6161385 Turbomachine and method of use
12/14/2000WO2000075499A1 Modified fuel gas turbo-expander for oxygen blown gasifiers and related method
12/14/2000WO2000075492A1 Concentricity ring
12/14/2000WO2000075491A1 Turbomachine and sealing element for a rotor thereof
12/14/2000CA2371131A1 Turbomachine and sealing element for a rotor of a turbomachine
12/13/2000EP1059422A1 Protection device for the nozzle vane actuator of a turboreactor
12/13/2000EP1059418A2 Gas turbine airfoil internal air system
12/12/2000US6159314 Nickel-base single-crystal superalloys, method for manufacturing the same, and gas turbine parts prepared therefrom
12/12/2000US6158961 Truncated chamfer turbine blade
12/12/2000US6158957 Thermal barrier removal process
12/12/2000US6158955 Welding method and assembly therefor
12/07/2000WO2000073762A1 Inspection device for an annular combustion chamber of a gas turbine and method of inspecting an annular combustion chamber of a gas turbine
12/07/2000DE19961540A1 Air feed channel for steam generator with heat recovery, is coupled to left and right sides of inlet channel for steam generator supplied with gas turbine exhaust gas
12/07/2000DE19925328A1 Einrichtung zum Zünden der Verbrennung in einer Brennkammer einer Gasturbine Means for igniting the combustion in a combustor of a gas turbine
12/06/2000EP1057987A2 Ignition device for a gas turbine combustor
12/06/2000EP1057986A1 Heat engine
12/06/2000EP1057972A2 Turbine blade tip with offset squealer
12/06/2000EP1057568A2 Welding method and assembly therefor
12/05/2000US6156269 Method of protecting high-energy machinery from corrosion damage
12/05/2000US6155819 Dry, low NOx catalytic pilot
12/05/2000US6155777 Removal of cooling air on the housing side of a diffuser of a compressor stage of gas turbines
12/05/2000US6155056 Cooling louver for annular gas turbine engine combustion chamber
12/05/2000US6155055 Separator for a two-head combustor chamber
12/05/2000US6155040 Gas turbine
12/05/2000US6155038 Method and apparatus for use in control and compensation of clearances in a gas turbine
12/05/2000US6154959 Laser cladding a turbine engine vane platform
11/2000
11/30/2000WO2000071855A1 Device for controlling air flow in a turbine blade
11/30/2000WO2000071854A1 Cast on-board injection nozzle with adjustable flow area
11/30/2000WO2000071781A2 Bond coats for turbine components and method of applying the same
11/30/2000WO2000071228A1 Concentric fuel/oil filters and heat exchanger package
11/30/2000DE19924607A1 Inspektionsvorrichtung für eine Ringbrennkammer einer Gasturbine und Verfahren zur Inspektion einer Ringbrennkammer einer Gasturbine An inspection apparatus for an annular combustion chamber of a gas turbine and method for inspection of an annular combustor of a gas turbine
11/30/2000DE10021327A1 Automatic method to manufacture cell of recovery device; involves using workstations controlled by individual and main control systems to assemble and shape elements to form cells
11/29/2000EP1055809A2 A gas turbine engine and a method of controlling a gas turbine engine
11/29/2000EP1055480A2 Repair of a recess in an article surface
11/28/2000US6152694 Tip shroud for moving blades of gas turbine
11/28/2000US6152690 Sealing apparatus for gas turbine
11/28/2000US6152685 Seal active clearance control system for gas turbine stationary blade
11/28/2000CA2019802C An acoustic liner
11/23/2000WO2000070193A1 Turbo-machine comprising a sealing system for a rotor
11/23/2000WO2000070192A1 Seal for sealing a gap, in particular in a turbine, and a turbine
11/23/2000WO2000070191A1 Sealing system for a rotor of a turbo engine
11/23/2000WO2000069996A1 Turbine fuel composition
11/23/2000DE19919293C1 Hochtemperatur-Gaserhitzer High-temperature gas heater
11/23/2000CA2372875A1 Turbomachine with a sealing system for a rotor
11/23/2000CA2372740A1 Turbomachine, in particular a gas turbine, with a sealing system for a rotor
11/22/2000EP1054137A2 Mounting an inner shell within an outer turbine casing
11/22/2000EP1053434A2 Fuel air mixer for a radial dome in a gas turbine engine combustor
11/22/2000CN1273895A Surface processing method for matchable, conforming to fluid tech.
11/21/2000US6149387 Seal structure for gas turbine flange contact surfaces
11/21/2000US6148605 Method and device for reversing the thrust of very high bypass ratio turbojet engines
11/21/2000US6148518 Method of assembling a rotary machine
11/21/2000US6148517 Repair of turbine exhaust case
11/16/2000WO2000068616A1 Catalytic converter arrangement
11/16/2000WO2000068461A2 Thermal barrier coating
11/15/2000EP1052424A2 Apparatus and methods for balancing turbine rotors
11/15/2000EP1052376A2 Tip sealing method for compressors
11/15/2000EP1052375A2 Apparatus and method for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages
11/15/2000EP1052374A2 Cooling circuit for steam and air-cooled turbine nozzle stage
11/15/2000EP1052372A2 Trailing edge cooling passages for gas turbine nozzles with turbulators
11/15/2000EP1052371A2 Retention sleeve for a transfer tube of a thermal medium in a gas turbine
11/15/2000EP1052370A2 Method of manufacturing streamlined aerodynamics surfaces
11/15/2000CN1058551C New power process
11/14/2000US6146099 Frangible fan blade
11/14/2000US6146098 Tip shroud for cooled blade of gas turbine
11/14/2000US6146090 Cooling/heating augmentation during turbine startup/shutdown using a seal positioned by thermal response of turbine parts and consequent relative movement thereof
11/14/2000US6145616 Acoustic chamber
11/14/2000US6145319 Transitional multihole combustion liner
11/14/2000US6145318 Dual orifice bypass system for dual-fuel gas turbine
11/14/2000US6145296 Gas turbine engine having counter rotating turbines and a controller for controlling the load driven by one of the turbines
11/14/2000US6145294 Liquid fuel and water injection purge system for a gas turbine
11/09/2000WO2000066887A1 Thermodynamic process and system for generating work
11/09/2000DE19920655A1 High temperature insulation used for lining combustion chambers and inner components of gas turbines has a multilayer structure whose first layer is in contact with a hot medium
11/08/2000EP1050672A2 Electrical generator for an aero-engine
11/08/2000EP1050665A2 Bushing retention system for cooling tubes in a gas turbine rotor
11/08/2000EP1050663A2 Article having protuberances for creating turbulent flow and method for providing protuberances on an article
11/08/2000CN1272593A Method for improving cooling effect of gaseous coolant flow and its related product
11/07/2000US6143107 Hard-faced insulating refractory fiber linings
11/07/2000US6142731 Low thermal expansion seal ring support
11/07/2000US6142730 Gas turbine cooling stationary blade
11/07/2000US6142477 Active seal
11/07/2000US6142418 Multi-path secondary power system for an aircraft
11/07/2000US6141968 Fuel nozzle for gas turbine engine with slotted fuel conduits and cover