Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
01/2002
01/02/2002EP1167693A2 Guide vane platforms
01/02/2002EP1167692A2 Fan blade configuration
01/02/2002EP1167691A2 Blade damper and method for making same
01/02/2002EP1167690A1 Cooling of the trailing edge of a gas turbine airfoil
01/02/2002EP1167689A1 Configuration of a coolable turbine blade
01/02/2002EP1167688A2 Fan blade platform
01/02/2002EP1167322A1 Article comprising a substrate containing silicon and a barrier layer which functions as a protective/thermal barrier coating
01/02/2002EP1165941A1 High temperature erosion resistant, abradable thermal barrier composite coating
01/02/2002EP1165940A1 Means for securing a bucket to a turbine wheel and methods of installation
01/02/2002EP1165939A1 Cast gas turbine blade that is flown through by a coolant and device and method for producing a distribution chamber for the gas turbine blade
01/02/2002EP1049562A4 Turbine blades made from multiple single crystal cast superalloy segments
01/02/2002EP1049561A4 Turbine components comprising thin skins bonded to superalloy substrates
01/02/2002CN2469184Y Blade self-capping damp piece structure of steam turbine
01/02/2002CN1329696A Rotor blade of wind driven generator
01/01/2002US6335105 For forming part for a gas turbine engine, heat resistance
01/01/2002US6334756 Turbine rotor, cooling method of turbine blades of the rotor and gas turbine with the rotor
01/01/2002US6334755 Turbomachine including a device for supplying pressurized gas
01/01/2002US6334753 Streamlined bodies with counter-flow fluid injection
01/01/2002US6334295 Rotating diffuser for pressure recovery in a steam cooling circuit of a gas turbine
01/01/2002CA2251198C Gas turbine stationary blade
12/2001
12/30/2001CA2351284A1 Corner tang fan blade
12/27/2001WO2001098654A1 A wind turbine rotor blade comprising one or more means secured to the blade for changing the profile thereof depending on the atmospheric temperature
12/27/2001WO2001098653A1 A wind turbine wing with noise reduction means
12/27/2001WO2001098634A1 Configuration of a coolable turbine blade
12/27/2001WO2001098561A2 Graded platinum diffusion aluminide coating
12/27/2001WO2001098232A1 Protective coating including porouos silicon nitride matrix and noble metal
12/27/2001US20010055653 Process for cleaning an article, process for coating an article, and device therefor
12/27/2001US20010055527 Blade locking device with hammer fastener on a disk
12/26/2001CN2467796Y Gas combustion turbine cooling blade
12/26/2001CN1076782C Vane for gas turbine
12/25/2001US6333488 Method for setting up and controlling confinement media flow in laser shock peening
12/25/2001US6333121 Low-sulfur article having a platinum-aluminide protective layer and its preparation
12/25/2001US6333069 Method for preventing harm from constrictions formed during coating with a protective coat in the cooling holes of gas-cooled parts
12/25/2001US6332754 Steam turbine
12/25/2001US6332617 Leaktight seal of a circular vane stage
12/25/2001US6332490 Apparatus for bonding a strip to an article surface
12/25/2001US6332272 Method of repairing a turbine blade
12/25/2001CA2245639C Recovery type steam-cooled gas turbine
12/20/2001WO2001096711A1 Device for locking hammer clamp blades on a disc
12/20/2001WO2001048424A3 Cold air refrigerating system and turboexpander turbine for this system
12/20/2001US20010053410 The MCrAlY-coating is repaired locally and the article is aluminised and/or chromised on the surface of the article on top of the MCrAlY-coating.
12/20/2001US20010052230 Fuel preheating in a gas turbine
12/20/2001DE10027842A1 Gas turbine layout cooling system bleeds portion of film cooling air through turbine blade via inlet or outlet edge borings for direct blade wall service.
12/19/2001EP1164273A2 Turbo jet engine with heat exchanger
12/19/2001EP1164253A1 Cooling system for the shroud of paired rotor blades
12/19/2001EP1164252A2 Support pedestals for a wall cover in a gas turbine nozzle segment
12/19/2001EP1164251A1 Rotor blade locking means
12/19/2001EP1164250A2 Floating connector for an impingement insert
12/19/2001EP1163970A1 Method of forming cooling holes in ceramic matrix composite turbine components
12/19/2001EP1163429A1 Sealing device for segmented stator ring
12/19/2001EP1163428A1 Guide blade and guide blade rim for a fluid-flow machine and component for delimiting a flow channel
12/19/2001EP1163427A1 Gas turbine rotor with internally-cooled gas turbine blade
12/19/2001EP1163426A1 Turbomachine blade
12/19/2001EP1163425A1 Turbine blade
12/19/2001CN1076430C Heat recovery gas turbine rotor
12/18/2001US6331361 Methods for manufacture and repair and resulting components with directionally solidified or single crystal materials
12/18/2001US6331217 Turbine blades made from multiple single crystal cast superalloy segments
12/18/2001US6331100 Doubled bowed compressor airfoil
12/18/2001US6331098 Coriolis turbulator blade
12/18/2001US6331097 Method and apparatus for purging turbine wheel cavities
12/18/2001CA2076100C Low noise fan assembly
12/13/2001US20010051218 Heat resistant coating a refractory metal silicide that is at least partially diffused into the base structure on at least one surface; for high temperature environments such as jets and rockets
12/13/2001DE10028732A1 Exhaust gas turbine comprises a running wheel which rotates in a turbine housing having a spiral-like inlet channel connected to an annular chamber into which a guiding mesh can be pushed
12/12/2001EP1162286A1 A method for removing a coating from a substrate
12/12/2001EP1162284A1 Process of repairing a coated component
12/11/2001US6329633 Method and material for processing a component for laser machining
12/11/2001US6329632 Method and device for machining holes or shapes of varying profile using an excimer laser
12/11/2001US6328810 Removing loose contamination from hardware surfaces; selectively applying reactive metal and filler to preselected portion of hardware surfaces; heating to cause reaction between combustion products and reactive metal; cooling
12/11/2001US6328533 Swept barrel airfoil
12/11/2001US6328532 Blade cooling
12/11/2001US6328531 Cooled turbine blade
12/11/2001CA2256597C Steam cooled type gas turbine
12/06/2001WO2001092688A2 Improvements to disc-type airborne vehicle and radial flow gas turbine engine used therein
12/06/2001US20010048972 Galvanizing; controlling tolerances
12/06/2001US20010048878 Cooling circuit for a gas turbine bucket and tip shroud
12/06/2001US20010047763 Masking fixture and method
12/05/2001EP1160418A2 Steam exit flow design for aft cavities of an airfoil
12/05/2001EP1160352A1 Method of adjusting the size of cooling holes of a gas turbine component
12/05/2001EP1159533A1 Centrifugal air flow control
12/05/2001EP0960308B1 Gas turbine installation with a ceramic-covered combustion chamber housing
12/04/2001US6326585 Apparatus for laser twist weld of compressor blisks airfoils
12/04/2001US6325871 Method of bonding cast superalloys
12/04/2001US6325593 Ceramic turbine airfoils with cooled trailing edge blocks
12/04/2001US6324831 Monorotor for a gas turbine engine
11/2001
11/29/2001US20010046441 Axial thermal medium delivery tubes and retention plates for a gas turbine rotor
11/29/2001US20010045426 Apparatus and method for heating a workpiece of metal
11/28/2001EP1158140A2 Exit joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles
11/28/2001CN1324433A Gas turbine engine
11/28/2001CN1075564C Low heat expansion alloy
11/27/2001US6322323 Turbine movable blade
11/27/2001US6322322 High temperature airfoil
11/27/2001US6321449 Method of forming hollow channels within a component
11/22/2001WO2001088214A1 Η-tial alloy-based component comprising areas having a graduated structure
11/22/2001US20010042607 Process for producing a thermally loaded casting
11/22/2001DE10102991A1 Device, for heating metal workpiece, has induction coil with variable frequency AC current, first frequency for heating predetermined workpiece region, second for heating separate object
11/22/2001DE10024343A1 One-piece component used e.g. for valves in combustion engines has a lamella cast structure
11/22/2001DE10024302A1 Verfahren zur Herstellung eines thermisch belasteten Gussteils A process for producing a thermally loaded casting
11/21/2001EP1156189A1 Turbine blade, turbine and operating method of a turbine
11/21/2001EP1156187A2 Nozzle cavity insert having impingement and convection cooling regions
11/21/2001EP1156186A2 Film cooling air pocket in a closed loop cooled airfoil