| Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915) |
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| 01/22/2003 | EP1276972A1 Turbine |
| 01/22/2003 | EP1276971A1 Rotor for a gas turbine |
| 01/22/2003 | EP0954679B1 Coolable airfoil for a gas turbine engine |
| 01/22/2003 | CN1392917A Steam-type gas turbine subassembly and method for enhancing turbine performance |
| 01/22/2003 | CN1392822A Ultrasonic cross shot peening of vanes on rotor |
| 01/22/2003 | CN1392809A Device and method for producing blade for turbine and blade produced according to this method |
| 01/21/2003 | US6508630 Twisted stator vane |
| 01/21/2003 | US6508624 Turbomachine with double-faced rotor-shroud seal structure |
| 01/21/2003 | US6508620 Inner platform impingement cooling by supply air from outside |
| 01/21/2003 | US6508093 Method and apparatus for ultrasonic peening of annular recesses for the attachment of blades to a rotor |
| 01/21/2003 | US6508000 Transient liquid phase bonding repair for advanced turbine blades and vanes |
| 01/21/2003 | CA2218457C Process for manufacturing a hollow turbine engine blade |
| 01/16/2003 | WO2003004834A1 Securing system for the rotor blades of axial flow turbo engines |
| 01/16/2003 | WO2003004711A1 Sintered tin-containing cobalt-based and nickel-based alloys |
| 01/16/2003 | US20030012939 Fiber reinforced composite article, fiber member, and method for making |
| 01/16/2003 | US20030012655 Turbine rotor blades assembly and method for assembling the same |
| 01/16/2003 | US20030012654 Turbine blade arrangement |
| 01/16/2003 | US20030012651 Bladed rotor disc side-plate and corresponding arrangement |
| 01/16/2003 | US20030012647 Gas turbine stationary blade |
| 01/16/2003 | US20030012645 Inlet guide vane for axial compressor |
| 01/16/2003 | US20030012643 Turbine installation |
| 01/16/2003 | US20030010469 Device and method for casting a workpiece and workpiece |
| 01/15/2003 | EP1275819A2 Gas turbine stationary blade |
| 01/15/2003 | EP1275818A1 Base material with cooling hole |
| 01/15/2003 | EP1275747A1 Method and device for coating a high temperature resistant article with a thermal protection covering |
| 01/14/2003 | US6506022 Turbine blade having a cooled tip shroud |
| 01/14/2003 | US6506021 Cooling system for a gas turbine |
| 01/14/2003 | US6506020 Blade platform cooling |
| 01/14/2003 | US6506016 Angel wing seals for blades of a gas turbine and methods for determining angel wing seal profiles |
| 01/14/2003 | US6506013 Film cooling for a closed loop cooled airfoil |
| 01/14/2003 | US6505678 Ceramic core with locators and method |
| 01/14/2003 | US6505526 Fluid flow inspection apparatus and method for gas turbine buckets |
| 01/14/2003 | US6505489 Method and apparatus for ultrasonic peening of axial recesses for the attachment of blades to a rotor |
| 01/09/2003 | US20030008167 Comprises barrier layer, hot gas corrosion protection layer, heat barrier layer, and smoothing layer for turbine blades (stator or rotor blade) of an aircraft engine |
| 01/09/2003 | US20030008166 Bondcoat is formed by thermally co-spraying distinct alloy powders on the engine component forming an oxidation-resistant region, and spraying another alloy forming a bonding region |
| 01/09/2003 | US20030007870 Methods and apparatus for extending gas turbine engine airfoils useful life |
| 01/09/2003 | US20030007866 Shroud integral type moving blade and split ring of gas turbine |
| 01/09/2003 | US20030007864 System and method for airfoil film cooling |
| 01/09/2003 | US20030007827 Coupling arrangement |
| 01/08/2003 | EP1273815A2 Coupling arrangement |
| 01/08/2003 | EP1273759A1 Method and apparatus for extending gas turbine engine airfoils useful life |
| 01/08/2003 | EP1273758A2 System and method for airfoil film cooling |
| 01/08/2003 | EP1273757A1 Conically jointed turbocharger rotor |
| 01/08/2003 | CN2530041Y Self-crown wedge block damping loop-forming structure of turbine blade |
| 01/07/2003 | US6504127 Laser consolidation methodology and apparatus for manufacturing precise structures |
| 01/07/2003 | US6503574 Method for producing an enhanced thermal barrier coating system |
| 01/07/2003 | US6503349 Heating a repair alloy to a temperature that avoids recrystallization and repair zone incipient melting; rapid cooling and aging; stability of mechanical properties; joint strength; fatique; gas turbine high-pressurue vanes |
| 01/07/2003 | US6503059 Fourth-stage turbine bucket airfoil |
| 01/07/2003 | US6503054 Second-stage turbine nozzle airfoil |
| 01/07/2003 | US6503053 Blade with optimized vibration behavior |
| 01/07/2003 | US6502304 Turbine airfoil process sequencing for optimized tip performance |
| 01/07/2003 | US6502303 Method of repairing a turbine blade tip |
| 01/05/2003 | CA2352673A1 Inline-pipeline electric motor-generator propeller module |
| 01/03/2003 | WO2003001042A1 Means for wear reduction in a gas turbine combustor |
| 01/03/2003 | CA2451481A1 Means for wear reduction in a gas turbine combustor |
| 01/02/2003 | US20030002988 Bonded niobium silicide and molybdenum silicide composite articles using semi-solid brazes |
| 01/02/2003 | US20030002987 Compressor rotor blade spacer apparatus |
| 01/02/2003 | US20030002979 Hybrid turbine nozzle |
| 01/02/2003 | US20030002975 Combustor hot streak alignment for gas turbine engine |
| 01/02/2003 | US20030000602 Integrally bladed rotor airfoil fabrication and repair techniques |
| 01/02/2003 | EP1270873A2 Gas turbine blade |
| 01/02/2003 | EP1270872A1 Gas turbine engine |
| 01/02/2003 | EP1270141A2 Method for repairing cracks in a turbine blade root trailing edge |
| 01/02/2003 | EP1268981A1 Turbine installation |
| 01/01/2003 | CN1388306A Combustion gas turbine nited equipment |
| 12/31/2002 | US6500283 Casting alloy with sulfide forming compound such as yttria on surface; solidifying; reheating to cause migration of sulfur to the surface forming yttrium oxysulfide |
| 12/31/2002 | US6499969 Conically jointed turbocharger rotor |
| 12/31/2002 | US6499959 Steam turbine high strength tangential entry closure bucket and retrofitting methods therefor |
| 12/31/2002 | US6499957 Rotor for a turbomachine |
| 12/31/2002 | US6499953 Dual flow impeller |
| 12/31/2002 | US6499950 Cooling circuit for a gas turbine bucket and tip shroud |
| 12/31/2002 | US6499949 Turbine airfoil trailing edge with micro cooling channels |
| 12/31/2002 | US6499946 Steam turbine rotor and manufacturing method thereof |
| 12/31/2002 | US6499945 Wheelspace windage cover plate for turbine |
| 12/31/2002 | US6499943 Friction-susceptible component of a thermal turbo machine |
| 12/31/2002 | US6499938 Method for enhancing part life in a gas stream |
| 12/31/2002 | CA2280751C Gas turbine blade |
| 12/31/2002 | CA2266140C Gas turbine cooled blade |
| 12/31/2002 | CA2206160C Process for manufacturing a turbomachine hollow vane and multiple-effect press-kiln used in process operation |
| 12/27/2002 | WO2002103166A1 Fastening of blades |
| 12/27/2002 | WO2002103165A1 Method for forming abrasion-resistant layer for moving blade, abrasion-resistant layer and method for regeneration thereof, and gas turbine |
| 12/27/2002 | WO2002103164A1 Multi-stage turbo-machines with specific blade aspect ratios |
| 12/27/2002 | WO2002103075A1 Method for repairing ni base alloy component |
| 12/27/2002 | WO2002103074A1 Thermal barrier coating material and method for production thereof, gas turbine member using the thermal barrier coating material, and gas turbine |
| 12/27/2002 | CA2450654A1 Method of forming abrasion-resistant layer on rotor blade, an abrasion-resistant layer and a method of regenerating the same, and a gas turbine |
| 12/26/2002 | US20020197507 Ceramic turbine blade attachment having high temperature, high stress compliant layers and method of fabrication thereof |
| 12/26/2002 | US20020197163 Steam turbine blade, and steam turbine and steam turbine power plant using the same |
| 12/26/2002 | US20020197161 Gas turbine airfoill |
| 12/26/2002 | US20020197160 Airfoil tip squealer cooling construction |
| 12/26/2002 | US20020197159 Turbine blade with rub tolerant cooling construction |
| 12/26/2002 | US20020197157 Tandem guide vanes |
| 12/26/2002 | US20020197156 Aerofoil for an axial flow turbomachine |
| 12/26/2002 | US20020197155 Abradeable seal system |
| 12/26/2002 | US20020197152 Airfoils with improved oxidation resistance and manufacture and repair thereof |
| 12/26/2002 | US20020195176 Integrally bladed rotor airfoil fabrication and repair techniques |
| 12/26/2002 | US20020194733 Method for repairing cracks in a turbine blade root trailing edge |
| 12/25/2002 | CN1386958A Blade of turbine and turbine |
| 12/25/2002 | CN1097140C Blades of fluid machine affected by hot loading |
| 12/25/2002 | CN1097139C Cooling structure for airfoil leading edge |
| 12/24/2002 | US6497968 Turbines; heat resistance |