| 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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| 09/11/2002 | EP1239116A2 Fluted blisk |
| 09/11/2002 | EP1239059A2 Chemical milling of the blades of a gas turbine engine |
| 09/11/2002 | EP1239058A2 Coating for gas turbine blades |
| 09/11/2002 | EP1238742A1 Method of applying braze materials to a substrate requiring repair |
| 09/11/2002 | EP1238185A1 A single or multi-bladed rotor |
| 09/11/2002 | EP1238184A1 Machine set |
| 09/11/2002 | EP1169495A4 Electrochemical stripping of turbine blades |
| 09/11/2002 | EP0891483B1 Closed-loop air cooling system for a turbine engine |
| 09/11/2002 | CN1368923A Rotor with split rotor blade |
| 09/10/2002 | US6447624 Manufacturing process of nickel-based alloy having improved hot sulfidation-corrosion resistance |
| 09/10/2002 | US6447255 Gas turbine nose cone assembly |
| 09/10/2002 | US6447254 Silicon oxynitride ceramic and alumina or lutetium oxide sintering aid; ball milling, decantation, drying, and granulation; wear resistance; rotor and turbine blades |
| 09/10/2002 | US6447253 Turbine rotor disk fitted with blades having christmastree-shaped roots, and a method of mounting a blade on a disk |
| 09/10/2002 | US6447252 Rotor-shaft connector |
| 09/10/2002 | US6447250 Non-integral fan platform |
| 09/06/2002 | WO2002068800A1 Turbine blade with pre-segmented squealer tip |
| 09/06/2002 | WO2002050323A3 Nickel diffusion braze alloy and method for repair of superalloys |
| 09/06/2002 | WO2002048508A3 Turbine bucket cover and brush seal |
| 09/05/2002 | US20020123827 System and method for performing electronic triage of a turbine part |
| 09/05/2002 | US20020122738 Article having imbedded cavity |
| 09/05/2002 | US20020122725 Article having dampening member installed into an imbedded cavity |
| 09/05/2002 | US20020122723 Electrical machine |
| 09/05/2002 | US20020122721 Tip treatment assembly for a gas turbine engine |
| 09/05/2002 | US20020122718 Tip treatment bars for gas turbine engines |
| 09/05/2002 | US20020122716 Methods and apparatus for cooling gas turbine engine blade tips |
| 09/04/2002 | EP1236864A2 System and method for perfoming electronic triage of a turbine part and for carrying out a turbine part repair |
| 09/04/2002 | CN1090283C Turbocharging system with internally-fitted assisting electric motor and cooling system thereof |
| 09/04/2002 | CN1090282C Inner cylinder jet type internal combustion engine control device |
| 09/03/2002 | US6444335 Gas turbine engines |
| 09/03/2002 | US6444271 Durable refractory ceramic coating |
| 09/03/2002 | US6444060 Enhancement of an unused protective coating |
| 09/03/2002 | US6443700 Transpiration-cooled structure and method for its preparation |
| 09/03/2002 | US6443699 Bushing retention system for thermal medium cooling delivery tubes in a gas turbine rotor |
| 09/03/2002 | US6443697 Turbine wheel and pelton turbine equipped with same |
| 09/03/2002 | US6443695 Steam turbine |
| 09/03/2002 | CA2264682C Gas turbine cooled blade tip shroud |
| 09/03/2002 | CA2262064C Gas turbine moving blade platform |
| 08/29/2002 | WO2002066706A2 High temperature coatings for gas turbines |
| 08/29/2002 | WO2002018674A3 Thermal barrier coating system for turbine components |
| 08/29/2002 | US20020119730 Method of forming a trailing edge cutback for a turbine bucket |
| 08/29/2002 | US20020119340 Turbines; heat resistance |
| 08/29/2002 | US20020119338 Tubine engine component having wear coating and method for coating a turbine engine component |
| 08/29/2002 | US20020119047 Turbine airfoil with single aft flowing three pass serpentine cooling circuit |
| 08/29/2002 | US20020119046 Attachment air inlet configuration for highly loaded single crystal turbine blades |
| 08/29/2002 | US20020119045 Turbine airfoil with metering plates for refresher holes |
| 08/29/2002 | US20020119043 Article having corrosion resistant coating |
| 08/29/2002 | US20020117485 Method and apparatus for increasing welding rates for high aspect ratio welds |
| 08/29/2002 | DE10122524A1 Strömungsmaschinenlaufrad und Strömungsmaschine Fluid Machinery impeller and flow machine |
| 08/29/2002 | CA2418101A1 High temperature coatings for gas turbines |
| 08/28/2002 | EP1234949A2 Cooling air inlet configuration for a blade root |
| 08/28/2002 | EP1234104A1 Shear pin with locking cam |
| 08/28/2002 | CA2372353A1 Torque pin |
| 08/27/2002 | US6441341 Method of forming cooling holes in a ceramic matrix composite turbine components |
| 08/27/2002 | US6440575 Ceramic thermal barrier layer for gas turbine engine component |
| 08/27/2002 | US6439851 Reduced stress rotor blade and disk assembly |
| 08/27/2002 | US6439848 Drilled cooling air openings in gas turbine components |
| 08/27/2002 | US6439847 Air-cooled turbine blade |
| 08/27/2002 | US6439846 Turbine blade wall section cooled by an impact flow |
| 08/27/2002 | US6439844 Turbine bucket cover and brush seal |
| 08/27/2002 | US6439838 Periodic stator airfoils |
| 08/27/2002 | US6439837 Nozzle braze backside cooling |
| 08/27/2002 | US6438838 Method for repairing and producing integrally bladed rotors for a turbine or turbo engine |
| 08/27/2002 | US6438837 Methods for aligning holes through wheels and spacers and stacking the wheels and spacers to form a turbine rotor |
| 08/22/2002 | WO2002064959A1 Connection method for turbo charger turbine shaft |
| 08/22/2002 | US20020114701 Method of investment casting with casting identification |
| 08/22/2002 | US20020114700 Airfoil configured for moisture removal from steam turbine flow path |
| 08/22/2002 | US20020114696 Gas turbine nozzle vane insert and methods of installation |
| 08/22/2002 | DE10108005A1 Bindung der Beschaufelung einer Strömungsmaschine Binding of the blading of a turbomachine |
| 08/22/2002 | DE10104662A1 Verfahren zur Reduzierung der Geräuschabstrahlung von Propellern A method of reducing noise radiation of propellers |
| 08/22/2002 | CA2364910A1 Method of applying braze materials to a substrate |
| 08/21/2002 | EP1233147A2 Gas turbine with cooling arrangement |
| 08/21/2002 | EP1233146A2 Gas turbine nozzle vane insert and methods of installation |
| 08/21/2002 | EP1233081A1 Process and apparatus for plasma coating a turbine blade |
| 08/21/2002 | EP1232331A1 Lightweight structural component having a sandwich structure |
| 08/21/2002 | CN1364975A Method and device for reducing the temperature of turbine leaf opex |
| 08/20/2002 | US6438645 Apparatus and structure for rapid enablement |
| 08/20/2002 | US6435835 Article having corrosion resistant coating |
| 08/20/2002 | US6435834 Bucket and wheel dovetail connection for turbine rotors |
| 08/20/2002 | US6435833 Bucket and wheel dovetail connection for turbine rotors |
| 08/20/2002 | US6435831 Gas-turbine rotor |
| 08/20/2002 | US6435830 Article having corrosion resistant coating |
| 08/20/2002 | US6435826 Article having corrosion resistant coating |
| 08/20/2002 | US6435825 Hollow nozzle partition with optimized wall thickness and method of forming |
| 08/20/2002 | US6435821 Variable vane for use in turbo machines |
| 08/20/2002 | US6435819 Turbo machines |
| 08/20/2002 | US6435816 Gas injector system and its fabrication |
| 08/20/2002 | US6435815 Aerofoil for an axial flow turbo machine |
| 08/20/2002 | US6435814 Film cooling air pocket in a closed loop cooled airfoil |
| 08/20/2002 | US6435813 Impigement cooled airfoil |
| 08/20/2002 | US6435812 Bore tube assembly for steam cooling a turbine rotor |
| 08/20/2002 | CA2263642C Seal structure for gas turbines |
| 08/15/2002 | WO2001040548A9 Chemical cleaning solution for gas turbine blades |
| 08/15/2002 | US20020110454 Gas turbine blade and method for producing a gas turbine blade |
| 08/15/2002 | US20020110451 Methods and apparatus for reducing seal teeth wear |
| 08/15/2002 | US20020110450 Air bearing articulated shaft and floating module configuration for a small rotary compressor |
| 08/15/2002 | US20020108734 Process for the rapid production of hollow components of flow machines for manufacturing development |
| 08/15/2002 | US20020108681 Heat treatment comprising the steps of normalizing the heat resistant steel, and oil-cooling the normalized heat-resisting steel to a temperature of <300 degrees C.; high heat resistance and mechanical strength; steam turbine rotors |
| 08/15/2002 | US20020108379 Gas turbine |
| 08/14/2002 | EP1231420A2 Methods and apparatus for reducing seal teeth wear |
| 08/14/2002 | EP1231359A2 Method and apparatus for reducing turbine blade tip region temperatures |