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