| 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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| 04/27/2000 | WO2000023634A1 Method and device for cleaning a product |
| 04/27/2000 | DE19852285C1 High temperature substrate, especially a nickel superalloy gas turbine component, blade or combustion chamber plate, has a heat insulating layer of ceramic, metal and-or metal alloy containing glass |
| 04/27/2000 | DE19847222A1 Component, e.g. turbine blade, is made of a metal part having a rigid structure with a surface layer having a partial finely ground structure |
| 04/26/2000 | EP0995880A2 Turbine blade |
| 04/25/2000 | US6054672 Laser welding superalloy articles |
| 04/25/2000 | US6053701 Gas turbine rotor for steam cooling |
| 04/25/2000 | US6053700 Ducted turbine |
| 04/25/2000 | US6053699 Steam turbine having a brush seal assembly |
| 04/25/2000 | US6053697 Trilobe mounting with anti-rotation apparatus for an air duct in a gas turbine rotor |
| 04/25/2000 | US6052897 Compressor-wheel arrangement for turbochargers |
| 04/25/2000 | CA2206980C Gas turbine blade retention |
| 04/20/2000 | WO2000022287A2 Gas turbine engine |
| 04/20/2000 | WO2000021746A1 Method for obtaining thin, light and rigid metal parts |
| 04/20/2000 | WO2000003124A3 High temperature airfoil |
| 04/20/2000 | DE19848104A1 Turbinenschaufel Turbine blade |
| 04/20/2000 | CA2345341A1 Gas turbine engine |
| 04/19/2000 | EP0994239A2 Truncated chamfer turbine blade |
| 04/19/2000 | EP0993939A1 Method of manufacturing thin, light and rigid metal pieces |
| 04/19/2000 | EP0725888B1 Mounting and sealing arrangement for a turbine shroud segment |
| 04/19/2000 | EP0670955B1 Coolable airfoil structure |
| 04/19/2000 | EP0636204B1 Rotors for gas turbine engines |
| 04/19/2000 | CN1251153A Steam turbine and blades thereof |
| 04/18/2000 | US6050777 Apparatus and method for cooling an airfoil for a gas turbine engine |
| 04/18/2000 | US6050776 Gas turbine stationary blade unit |
| 04/18/2000 | US6050079 Modulated turbine cooling system |
| 04/18/2000 | US6049979 Methods for shielding a welding gas turbine repair of a damaged turbine rotor wheel dovetail |
| 04/18/2000 | US6049978 Methods for repairing and reclassifying gas turbine engine airfoil parts |
| 04/18/2000 | CA2147448C Gas turbine rotor blade tip cooling device |
| 04/13/2000 | WO2000020740A2 Gas turbine engine |
| 04/13/2000 | WO2000020725A1 Sealing device for segmented stator ring |
| 04/13/2000 | DE19846332A1 Kühlkanal eines thermisch hochbelasteten Bauteils Cooling channel of a thermally highly stressed component |
| 04/13/2000 | CA2345293A1 Gas turbine engine |
| 04/12/2000 | EP0992656A1 Turbomachine to compress or expand a compressible medium |
| 04/12/2000 | EP0992655A2 Cooling channel for thermally highly stressed elements |
| 04/12/2000 | EP0992654A2 Coolant passages for gas turbine components |
| 04/12/2000 | EP0992653A1 Film-cooled components with triangular cross section cooling holes |
| 04/12/2000 | EP0992603A1 Thermal barrier coating systems and materials |
| 04/12/2000 | EP0992315A2 Method for reducing void volumes in cavities for laser drilling |
| 04/12/2000 | EP0992310A2 Step milling process |
| 04/12/2000 | EP0991866A1 Compressor blade and use of the same |
| 04/12/2000 | EP0991850A1 Internally cooled steam turbine shaft and method for cooling the same |
| 04/12/2000 | CN1250487A Method of forming internal passages within articles and articles formed by same |
| 04/11/2000 | US6048174 Impact resistant hollow airfoils |
| 04/11/2000 | US6048169 Turbine shaft and method for cooling a turbine shaft |
| 04/11/2000 | US6047540 Small gas turbine engine having enhanced fuel economy |
| 04/11/2000 | US6047474 Method of manufacturing a bimetallic turbine blade and use thereof |
| 04/11/2000 | CA2148581C Heat treatment to reduce embrittlement of titanium alloys |
| 04/06/2000 | WO2000019065A1 Gas turbine moving blade and a method for producing a gas turbine moving blade |
| 04/06/2000 | DE19845147A1 Vorrichtung und Verfahren zur Kühlung einer einseitug von Heißgas umgebenen Wand Apparatus and method for cooling a hot gas einseitug surrounding wall |
| 04/05/2000 | EP0990772A2 Device and method to cool a wall whose outer surface is in contact with a hot gas flow |
| 04/05/2000 | EP0990771A1 Trapped insert turbine airfoil |
| 04/05/2000 | EP0990770A1 Blading for highly loaded turbines |
| 04/05/2000 | EP0990481A1 Co-machined bonded airfoil |
| 04/05/2000 | EP0990090A1 Rotor blade of an axial-flow engine |
| 04/05/2000 | EP0731874B1 Hollow fan blade dovetail |
| 04/05/2000 | CN1249393A Turbine blade capable of bearing high load |
| 04/04/2000 | US6045325 Apparatus for minimizing inlet airflow turbulence in a gas turbine engine |
| 04/04/2000 | US6044830 Combustion engine |
| 04/04/2000 | CA2041130C Automatic tacking device |
| 03/30/2000 | WO2000017504A1 Fuel preheating in a gas turbine |
| 03/30/2000 | WO2000017491A1 High temperature gas turbine, preferably of a gas turbine engine |
| 03/30/2000 | WO2000017490A2 Methods for repairing and reclassifying airfoil parts |
| 03/30/2000 | WO2000017417A1 Method for processing the interior of a hollow part |
| 03/29/2000 | EP0775249B1 Flow directing assembly for the compression section of a rotary machine |
| 03/29/2000 | CN2371342Y Corrosion- and fatigue-resisting steam turbine vane |
| 03/28/2000 | US6042951 Ceramic-coated blade of gas turbine and method of producing same |
| 03/28/2000 | US6042880 Exposing bond coat substrate by removing ceramic protective coating, diffusing alloying metals into thermally degraded bond coat areas, overcoating with an aluminum alloy or aluminide, overcoating with final ceramic protective coating |
| 03/28/2000 | US6042338 Detuned fan blade apparatus and method |
| 03/28/2000 | US6042336 Offset center of gravity radial damper |
| 03/28/2000 | US6041514 Impeller for a hair dryer |
| 03/23/2000 | WO2000015382A1 Laser welding superalloy articles |
| 03/22/2000 | EP0987347A1 Thermal barrier coating system and method therefor |
| 03/21/2000 | US6039810 High temperature vapor coating container |
| 03/21/2000 | US6039542 Panel damped hybrid blade |
| 03/21/2000 | US6039537 Turbine blade which can be subjected to a hot gas flow |
| 03/21/2000 | US6039533 Fan blade, structures and methods |
| 03/21/2000 | US6039531 Gas turbine blade |
| 03/16/2000 | DE19932479A1 Gas turbine rotor cooling system uses cooled space outlets linked to flowed turbine space and arranged in blade flange parts in flowed nozzle area. |
| 03/15/2000 | EP0985802A1 Film cooling orifice and it's method of manufacture |
| 03/15/2000 | EP0985801A2 Blade configuration for steam turbine |
| 03/14/2000 | US6037687 Double diaphragm compound shaft |
| 03/14/2000 | US6037004 Shield has plurality of interdigitated tabs which urge the shield against the airfoil surfaces; protect airfoil from impact by particles directed at the tip of such airfoils |
| 03/14/2000 | US6036441 Series impingement cooled airfoil |
| 03/14/2000 | US6036440 Gas turbine cooled moving blade |
| 03/14/2000 | US6036438 Turbine nozzle |
| 03/14/2000 | US6036437 Bucket cover geometry for brush seal applications |
| 03/14/2000 | US6036436 Gas turbine cooling stationary vane |
| 03/14/2000 | CA2008744C F.o.d. - resistant blade |
| 03/14/2000 | CA2007633C Clearance control for the turbine of a gas turbine engine |
| 03/14/2000 | CA2007632C Cooled blades for a gas turbine engine |
| 03/14/2000 | CA2007631C Cooled blades for a gas turbine engine |
| 03/09/2000 | WO2000012869A1 Turbine guide blade |
| 03/09/2000 | WO2000012868A1 Turbine bucket |
| 03/09/2000 | WO1999064726A3 Compliant sleeve for ceramic turbine blades |
| 03/09/2000 | DE19838754C1 Abgasturbolader für eine Brennkraftmaschine Exhaust gas turbocharger for an internal combustion engine |
| 03/08/2000 | EP0984138A2 Turbomachine with shaft cooling |
| 03/08/2000 | EP0797724B1 Gas turbine blade retention |
| 03/08/2000 | EP0791127B1 Gas turbine vane with a cooled inner shroud |
| 03/08/2000 | CN1246579A Deformed material welding rotor of steam turbine |
| 03/07/2000 | US6034344 Method for applying material to a face of a flow directing assembly for a gas turbine engine |