| 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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| 10/08/2002 | US6461109 Third-stage turbine nozzle airfoil |
| 10/08/2002 | US6461108 Cooled thermal barrier coating on a turbine blade tip |
| 10/08/2002 | US6461107 Turbine blade tip having thermal barrier coating-formed micro cooling channels |
| 10/08/2002 | US6461105 Variable vane for use in turbo machines |
| 10/08/2002 | US6460343 Gas turbine engine |
| 10/03/2002 | WO2002077418A1 Environmental and thermal barrier coating for ceramic components |
| 10/03/2002 | WO2002050411A3 Tangential on board injector with auxiliary supply of cooled air |
| 10/03/2002 | US20020141872 Process for forming micro cooling channels inside a thermal barrier coating system without masking material |
| 10/03/2002 | US20020141870 Turbine airfoil trailing edge with micro cooling channels |
| 10/03/2002 | US20020141869 Turbine blade tip having thermal barrier coating-formed micro cooling channels |
| 10/03/2002 | US20020141868 Cooled thermal barrier coating on a turbine blade tip |
| 10/03/2002 | US20020141863 Twisted stator vane |
| 10/02/2002 | EP1245806A1 Cooled gas turbine balde |
| 10/02/2002 | EP1245787A2 Cooling a coated turbine blade tip |
| 10/02/2002 | EP1245786A2 Turbine airfoil training edge with micro cooling channels |
| 10/02/2002 | EP1245785A1 Turbine airfoil and manufacturing method therefor |
| 10/02/2002 | EP1245784A2 Variable guide vane |
| 10/02/2002 | EP1245691A2 Mask material |
| 10/02/2002 | EP1245689A2 Low-alloy heat-resistant steel, heat treatment method therefor, and turbine rotor comprising the same |
| 10/02/2002 | EP1245327A1 Filler powder for diffusion-brazing of nickel-, cobalt- or iron-based workpieces |
| 10/02/2002 | EP1244605A1 High temperature erosion resistant coating and material containing compacted hollow geometric shapes |
| 10/02/2002 | EP1144727B1 Antiabrasion coating |
| 10/02/2002 | EP1012445B1 Blade for a turbo-machine and steam turbine |
| 10/02/2002 | EP1000224B1 Distribution of cooling air in a turbine stage of a gas turbine |
| 10/02/2002 | EP0998361B1 Turbine blade and use of a known method for producing such a turbine blade |
| 10/02/2002 | EP0938624B1 Turbofan aircraft engine |
| 10/02/2002 | DE10115350A1 Bypass jet engine for aircraft is constructed such that at least a part of bypass or cold flow is located between inside diameter of base engine and surface or limits of central shaft housing |
| 10/02/2002 | DE10101070C1 Verfahren zum Gasphasendiffusionsbeschichten von metallischen Bauteilen Method for gas phase diffusion coating of metal components |
| 10/02/2002 | CN1372502A Method and device for treating the surface of part |
| 10/02/2002 | CN1372069A Propeller regulating mechanism for power changeable turbine and assembling method thereof |
| 10/02/2002 | CN1091675C Metal products and method for working hard metal products by lasre vibration peening |
| 10/01/2002 | US6457942 Fan blade retainer |
| 10/01/2002 | US6457938 Wide angle guide vane |
| 10/01/2002 | US6457935 System for ventilating a pair of juxtaposed vane platforms |
| 10/01/2002 | US6457934 Connector tube for a turbine rotor cooling circuit |
| 10/01/2002 | US6457654 Micromachined synthetic jet actuators and applications thereof |
| 10/01/2002 | US6457450 Ju. M. Luzhkov rotary-turbine internal combustion engine |
| 09/29/2002 | CA2378632A1 Powder used in diffusion brazing of nickel, cobalt or iron alloys |
| 09/26/2002 | WO2002074482A1 Apparatus and method for focal point control for laser machining |
| 09/26/2002 | WO2001075276A1 Gas turbine engine |
| 09/26/2002 | US20020136884 Thermal barrier coating having subsurface inclusions for improved thermal shock resistance |
| 09/26/2002 | US20020136835 Environmental and thermal barrier coating for ceramic components |
| 09/26/2002 | US20020136659 Rotor for a turbomachine, and process for producing a rotor of this type |
| 09/26/2002 | US20020136640 Torque pin |
| 09/26/2002 | US20020136639 Gas turbine engine aerofoils |
| 09/26/2002 | US20020136638 Pre-segmented squealer tip for turbine blades |
| 09/26/2002 | US20020136635 Device for cooling a shroud of a gas turbine blade |
| 09/26/2002 | DE10114612A1 Rotor für eine Turbomaschine sowie Verfahren zur Herstellung eines solchen Rotors Rotor for a turbomachine, as well as method for the production of such a rotor |
| 09/25/2002 | EP1243878A2 Cold air refrigerating system and turboexpander turbine for this system |
| 09/25/2002 | EP1243754A2 Turbomachine rotor and method of manufacture therefor |
| 09/25/2002 | EP1243630A2 Carbon resistant surface coating |
| 09/25/2002 | EP1242729A1 Method for operating a steam turbine, and a turbine system provided with a steam turbine that functions according to said method |
| 09/25/2002 | EP1242719A1 Viscous drag impeller components incorporated into pumps, turbines and transmissions |
| 09/24/2002 | US6455122 Heat-resisting fiber-reinforced composite material and manufacturing method thereof |
| 09/24/2002 | US6454885 Nickel diffusion braze alloy and method for repair of superalloys |
| 09/24/2002 | US6454536 Adhesion enhancers to promote bonds of improved strength between elastomers metals in lightweight aircraft fan blades |
| 09/24/2002 | US6454535 Blisk |
| 09/24/2002 | US6454534 Flush bucket cover |
| 09/24/2002 | US6454531 Fabricating turbine rotors composed of separate components |
| 09/24/2002 | US6454528 Intake and exhaust damper with movable motor fan assembly |
| 09/24/2002 | US6454526 Cooled turbine vane with endcaps |
| 09/24/2002 | US6454156 Method for closing core printout holes in superalloy gas turbine blades |
| 09/24/2002 | US6453674 Method of operation of gas turbine engine |
| 09/24/2002 | US6453557 Method of joining a vane cavity insert to a nozzle segment of a gas turbine |
| 09/23/2002 | CA2376832A1 Carbon resistant surface coating |
| 09/19/2002 | WO2001059263A3 Turbine blade arrangement |
| 09/19/2002 | US20020132131 Protective coating for a thermally stressed component, particularly a turbine component |
| 09/19/2002 | US20020130047 Methods of providing article with corrosion resistant coating and coated article |
| 09/19/2002 | US20020129878 For stationary or moving blades of a gas turbine; high temperature strength and room temperature ductility |
| 09/19/2002 | DE10112062A1 Method of welding together two thermally differently loaded parts e.g. for turbo-machine, requires initially positioning inter-layer on connection surface of second part |
| 09/18/2002 | EP1240410A1 Axial flow turbine type rotor machine for elastic fluid operation |
| 09/18/2002 | EP0968317B1 Method of forming internal passages within articles and articles formed by same |
| 09/18/2002 | CN1091220C Runner for turbo-machine, esp. for water turbine |
| 09/17/2002 | US6451454 Turbine engine component having wear coating and method for coating a turbine engine component |
| 09/17/2002 | US6451416 Hybrid monolithic ceramic and ceramic matrix composite airfoil and method for making the same |
| 09/17/2002 | US6450770 Second-stage turbine bucket airfoil |
| 09/17/2002 | US6450769 Blade assembly with damping elements |
| 09/17/2002 | US6450768 Axial thermal medium delivery tubes and retention plates for a gas turbine rotor |
| 09/17/2002 | US6450766 Stator vane blank and method of forming the vane blank |
| 09/17/2002 | US6450759 Gas turbine nozzle vane insert and methods of installation |
| 09/17/2002 | US6450758 Cooling system for a bearing of a turbine rotor |
| 09/17/2002 | CA2263012C Gas turbine moving blade platform |
| 09/12/2002 | WO2002070867A1 Methods and apparatus for cooling gas turbine engine blade tips |
| 09/12/2002 | WO2002070772A1 Method for plasma coating a turbine blade and coating device |
| 09/12/2002 | US20020128076 Method and apparatus to permit maintenance of tie bolt clamp load for extended temperature ranges |
| 09/12/2002 | US20020127112 Enhanced coating system for turbine airfoil applications |
| 09/12/2002 | US20020127111 Turbine moving blade, turbine stationary blade, turbine split ring, and gas turbine |
| 09/12/2002 | US20020127108 Fluted blisk |
| 09/12/2002 | US20020127105 Fixation device for blading of a turbo-machine |
| 09/12/2002 | US20020127104 Method for providing a curved cooling channel in a gas turbine component as well as coolable blade for a gas turbine component |
| 09/12/2002 | US20020127103 Cooled gas turbine blade |
| 09/12/2002 | US20020127097 Turbine vane assembly including a low ductility vane |
| 09/12/2002 | US20020127095 Gas turbine engine guide vane |
| 09/12/2002 | US20020125215 Chemical milling of gas turbine engine blisks |
| 09/12/2002 | US20020124615 Method for reducing variance in the coolant consumption of components of a turbo-machine |
| 09/12/2002 | US20020124570 Gas turbine, gas turbine apparatus, and refrigerant collection method for gas turbine moving blades |
| 09/12/2002 | US20020124402 Method for extending the life of attachments that attach blades to a rotor |
| 09/12/2002 | CA2438156A1 Method for the plasma coating of a turbine blade or vane, and coating device |
| 09/11/2002 | EP1239120A2 Gas turbine engine guide vane |
| 09/11/2002 | EP1239119A1 Turbine vane assembly including a low ductility vane |