| 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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| 09/13/1995 | EP0670954A1 Airfoil casting core reinforced at trailing edge |
| 09/13/1995 | EP0670953A1 Coolable airfoil structure |
| 09/12/1995 | US5449273 Composite airfoil leading edge protection |
| 09/12/1995 | US5448828 Hot isostatic pressing of intermetallic powder for diffusion binding to base material of chromium steel or titanium alloy |
| 09/06/1995 | CN1107934A 燃气轮机轮叶 Gas turbine vane |
| 09/05/1995 | US5447413 Stator endwall for an elastic-fluid turbine |
| 08/30/1995 | EP0669450A1 Component support structure |
| 08/30/1995 | EP0669403A2 Gas turbine blade alloy |
| 08/30/1995 | EP0669183A1 Welding method of two parts of a blade |
| 08/29/1995 | US5445499 Retaining and sealing system for rotor blades |
| 08/29/1995 | US5445498 Bucket for next-to-the-last stage of a turbine |
| 08/24/1995 | WO1995022850A1 Laminated rotor assembly |
| 08/24/1995 | WO1995022685A1 Hollow fan blade dovetail |
| 08/23/1995 | EP0668368A1 Gas turbine blade and a process for manufacturing the same |
| 08/22/1995 | US5443590 Rotatable turbine frame |
| 08/22/1995 | US5443367 Hollow fan blade dovetail |
| 08/22/1995 | US5443366 Gas turbine engine fan blade assembly |
| 08/22/1995 | US5443365 Fan blade for blade-out protection |
| 08/17/1995 | DE4411680C1 Repairing defects in protecting coatings of machinery |
| 08/16/1995 | EP0667207A1 Procedure for the preparation of a circular fibre reinforced metallic piece |
| 08/15/1995 | US5440874 Turbo-engine provided with a device for blowing air onto a rotor element |
| 08/10/1995 | WO1995021042A2 Repair coating for superalloy articles, such as gas turbine engine components |
| 08/09/1995 | EP0666407A2 Integrally bladed discs or drums |
| 08/09/1995 | EP0666406A1 Cooled turbine blade |
| 08/09/1995 | EP0666142A1 Method and device for the surface treatment and for the pre-stressing of the inner wall of a cavity |
| 08/08/1995 | US5439750 Titanium metal matrix composite inserts for stiffening turbine engine components |
| 08/08/1995 | US5439354 Hollow airfoil impact resistance improvement |
| 08/08/1995 | US5439353 Composite blade with reinforced leading edge |
| 08/08/1995 | US5439351 Heat pipes |
| 08/01/1995 | US5437737 A filler mixture consisting of at least two particle alloy powder having a melting point depressant |
| 07/26/1995 | EP0663964A1 PROTECTION OF CHROMIUM-STEEL SUBSTRATES AGAINST CORROSIVE AND EROSIVE ATTACK AT TEMPERATURES UP TO ABOUT 500 oC. |
| 07/25/1995 | US5435694 Stress relieving mount for an axial blade |
| 07/25/1995 | US5435693 Pin and roller attachment system for ceramic blades |
| 07/25/1995 | US5435138 Reduction in turbine/boiler thermal stress during bypass operation |
| 07/19/1995 | EP0547219B1 A titanium compressor blade having a wear-resistant portion |
| 07/13/1995 | WO1995018916A1 Gas turbine airfoil |
| 07/11/1995 | US5432905 Advanced asyncronous video architecture |
| 07/11/1995 | US5431752 Friction welding of γ titanium aluminide to steel body with nickel alloy connecting piece there between |
| 07/11/1995 | US5431543 Turbine blade locking assembly |
| 07/11/1995 | US5431542 Ramped dovetail rails for rotor blade assembly |
| 07/11/1995 | US5431541 Ceramic blade attachment system |
| 07/11/1995 | US5431537 Cooled gas turbine blade |
| 07/11/1995 | US5431533 For a rotor supported for rotary motion |
| 07/11/1995 | US5430936 Method for making gas turbine engine blade attachment slots |
| 07/06/1995 | WO1995017990A1 Method for making gas turbine engine blade attachment slots |
| 07/05/1995 | EP0661415A1 Sealing means between a housing and a rotating body |
| 07/05/1995 | EP0661414A1 A cooled turbine blade for a gas turbine |
| 07/05/1995 | EP0661413A1 Axial blade cascade with blades of arrowed leading edge |
| 07/04/1995 | US5429877 Internally reinforced hollow titanium alloy components |
| 07/04/1995 | US5429479 Stage of vanes free at one extremity |
| 07/04/1995 | US5428953 Combined cycle gas turbine with high temperature alloy, monolithic compressor rotor |
| 06/29/1995 | WO1995017535A1 Rotor blades |
| 06/29/1995 | DE4343904A1 Bauteil aus faserverstärktem Verbundwerkstoff mit einer Schutzschicht gegen Erosion Component of fiber-reinforced composite material with a protective layer against erosion |
| 06/28/1995 | EP0659979A1 Variable camber turbine blade |
| 06/28/1995 | EP0659978A1 Aerodynamic tip sealing for rotor blades |
| 06/28/1995 | EP0470155B1 Wear-resistant laminated articles |
| 06/21/1995 | CA2138462A1 Increased output on full arc admission impulse turbines |
| 06/20/1995 | US5425622 Turbine blade attachment means |
| 06/20/1995 | US5425621 Device for axially securing moving blades and for eliminating rotor unbalances for axial-flow compressors or turbines |
| 06/20/1995 | US5425617 Constant static pressure runner in an axial flow turbine |
| 06/20/1995 | US5425174 Method for preparing a ceramic gas-turbine nozzle with cooling fine holes |
| 06/20/1995 | CA2020965C Turbomachine with seal fluid recovery channel |
| 06/14/1995 | EP0657623A1 Anti-contamination thrust balancing system for gas turbine engines |
| 06/08/1995 | WO1995015430A1 Airfoil having coolable leading edge region |
| 06/08/1995 | WO1995015240A1 Turbine blade repair |
| 06/08/1995 | DE4341216A1 Sealing component for diaphragm or labyrinth glands |
| 06/08/1995 | CA2178006A1 Turbine blade repair |
| 06/07/1995 | EP0464158B1 Lightweight airfoil |
| 06/06/1995 | US5421704 Inter-blade platform for a bladed disc of a turbomachine rotor |
| 06/04/1995 | CA2137180A1 Gas turbine blade alloy |
| 06/01/1995 | WO1995014849A1 Ceramic blade attachment system |
| 06/01/1995 | WO1995014848A1 Cooled turbine airfoil |
| 06/01/1995 | DE2841827C1 Metallic object having a thermal insulation coating |
| 06/01/1995 | DE2826998C1 Nozzle guide blade for a gas-turbine power plant |
| 05/31/1995 | EP0655511A1 Heat-resistant, ferritic cast steel having high castability and exhaust equipment member made thereof |
| 05/30/1995 | US5419971 Enhanced thermal barrier coating system |
| 05/30/1995 | US5419681 Film cooled wall |
| 05/30/1995 | US5419040 Hollow fan blade fabrication |
| 05/30/1995 | US5419039 For a gas turbine engine |
| 05/26/1995 | WO1995014157A1 Coolable rotor assembly |
| 05/24/1995 | EP0654586A1 Stator vane assembly |
| 05/24/1995 | EP0654585A1 Turbine blade geometry |
| 05/24/1995 | EP0654529A1 $g(a)-2,8-SIALYLTRANSFERASE |
| 05/24/1995 | DE4441507A1 Cooling structure for gas turbine blade |
| 05/23/1995 | US5418060 India-stabilized zirconia coating for composites |
| 05/23/1995 | US5417545 Cooled turbine nozzle assembly and a method of calculating the diameters of cooling holes for use in such an assembly |
| 05/18/1995 | DE4338745A1 Heat shield to gas turbine rotor |
| 05/17/1995 | CN1102632A Fibre reinforcement composite, making of same and unit made of same |
| 05/16/1995 | US5415526 Coolable rotor assembly |
| 05/16/1995 | US5414929 Method of producing a turbine rotor |
| 05/11/1995 | DE4338475A1 Shaft/hub connection with a light-alloy hub |
| 05/09/1995 | US5413463 Turbulated cooling passages in gas turbine buckets |
| 05/09/1995 | US5413458 Turbine vane with a platform cavity having a double feed for cooling fluid |
| 05/04/1995 | WO1995012056A1 Mounting and sealing arrangement for a turbine shroud segment |
| 05/03/1995 | EP0651137A1 Turbomachine with heating of the rotor discs during engine acceleration |
| 05/02/1995 | CA1335439C Alloy heat engine parts covered with a metal-ceramic protective coating |
| 04/28/1995 | CA2134420A1 Gas turbine vane |
| 04/27/1995 | WO1995011388A1 Surface of a body immersed in a fluid flow |
| 04/27/1995 | DE4336386A1 Turbine wheel and/or pump wheel (impeller) |
| 04/26/1995 | EP0649975A1 Metering of cooling air in turbine blades |