| 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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| 02/26/2002 | US6350103 Jet engine booster structure |
| 02/26/2002 | US6350102 Shroud leakage flow discouragers |
| 02/26/2002 | CA2170875C Interactive laser welding at elevated temperatures of superalloy articles |
| 02/21/2002 | WO2002014654A1 Turbine vane system |
| 02/21/2002 | US20020021966 Method and apparatus for cooling a wall within a gas turbine engine |
| 02/21/2002 | US20020020168 Turbojet power plant with heat exchanger |
| 02/21/2002 | DE10124393A1 Hitzebeständiger Stahl, Verfahren zur thermischen Behandlung von hitzebeständigem Stahl, und Kompenten aus hitzebeständigem Stahl A heat-resistant steel, process for the thermal treatment of heat-resistant steel, heat-resistant steel and Kompenten from |
| 02/20/2002 | EP1180580A1 Device for mounting an annular flask at a radial side of a bladed rotor |
| 02/20/2002 | EP1180579A2 Finger damper for turbine disk |
| 02/20/2002 | EP1180578A1 Statoric blades for a turbomachine |
| 02/20/2002 | EP1180577A2 Cooling method for a turbine rotor |
| 02/20/2002 | EP1180196A1 Turbo-machine comprising a sealing system for a rotor |
| 02/20/2002 | CN1336265A Metal object having under-pressure and single-end belt, and its mfg. method |
| 02/20/2002 | CN1079491C Turbine shaft and process for cooling same |
| 02/19/2002 | US6347923 Coolable blade for a gas turbine |
| 02/19/2002 | US6347660 Multipiece core assembly for cast airfoil |
| 02/14/2002 | US20020018719 Rotor blade retaining apparatus |
| 02/14/2002 | US20020018718 Enhanced fan and fan drive assembly |
| 02/14/2002 | US20020018717 Cooled gas turbine aerofoil |
| 02/14/2002 | US20020018715 Turbine blade support assembly and a turbine assembly |
| 02/14/2002 | US20020018711 Cooled flow deflection apparatus for a fluid-flow machine which operates at high temperatures |
| 02/13/2002 | EP0991850B1 Internally cooled steam turbine shaft and method for cooling the same |
| 02/12/2002 | US6345955 Bowed nozzle vane with selective TBC |
| 02/12/2002 | US6345952 Steam turbine |
| 02/12/2002 | CA2246856C Seal device between fastening bolt and bolthole in gas turbine disc |
| 02/12/2002 | CA2229883C Gas turbine shroud and platform seal system |
| 02/07/2002 | WO2002009905A1 Method and device for hardening a metal component by plasma pulse technology |
| 02/07/2002 | US20020015642 Turbine disc |
| 02/07/2002 | US20020014006 Process and blank for preparing rhomboidal blades for axial turbo engines |
| 02/06/2002 | EP1178231A2 Mechanical coupling for cooperating rotatable members |
| 02/06/2002 | EP1178181A2 Turbine blade tandem cooling |
| 02/06/2002 | EP1177330A2 Thermal barrier coating |
| 02/06/2002 | EP0954680B1 Turbine blade and its use in a gas turbine system |
| 02/05/2002 | US6344098 Heat treatment process is provided that produces a monoblock, low alloy steel rotor for use in low pressure steam turbines. |
| 02/05/2002 | US6343914 Fluid-flow machine component |
| 02/05/2002 | US6343911 Side wall cooling for nozzle segments for a gas turbine |
| 02/05/2002 | US6343641 Controlling casting grain spacing |
| 02/05/2002 | US6343474 Cooling passage of a component subjected to high thermal loading |
| 02/05/2002 | CA2254230C Gas turbine rotor blade |
| 02/05/2002 | CA2253741C Gas turbine cooled blade turbulators |
| 02/05/2002 | CA2052436C Composite material turbine wheel |
| 02/05/2002 | CA2049091C Steam turbine rotor having graded weldments |
| 01/31/2002 | US20020012590 Gas turbine bucket wall thickness control |
| 01/31/2002 | US20020012589 Blade platform cooling |
| 01/31/2002 | US20020012588 Gas turbine engine |
| 01/31/2002 | US20020012587 Gas turbine engine blade |
| 01/31/2002 | DE10035224A1 Verfahren und Rohling zum Herstellen von rhomboidischen Schaufeln für axiale Strömungsmaschinen Procedures and blank for the manufacture of rhomboidal blades for axial flow machines |
| 01/30/2002 | EP1176297A1 Internal combustion rotary turbomotor |
| 01/30/2002 | EP1176127A2 Fiber reinforced composite article, fiber containing member, and method for making |
| 01/30/2002 | EP1175956A1 Metallic article with integral end band under compression and method for making |
| 01/30/2002 | EP1175517A1 Stop-off for diffusion coating |
| 01/29/2002 | US6341942 Rotator member and method |
| 01/29/2002 | US6341941 Steam turbine |
| 01/29/2002 | US6341939 Tandem cooling turbine blade |
| 01/29/2002 | US6341936 FOD inspection of laser shock peened gas turbine engine airfoils |
| 01/29/2002 | US6341747 Nanocomposite layered airfoil |
| 01/29/2002 | US6341419 Loop stacked rotor assembly |
| 01/24/2002 | WO2001065086A8 Internal combustion rotary turbomotor |
| 01/24/2002 | US20020009362 Rotor for a prime mover and/or driven machine and the use of the rotor |
| 01/24/2002 | DE10029060A1 Turboluftstrahltriebwerk mit Wärmetauscher Turbojet engine with heat exchanger |
| 01/23/2002 | EP1174589A1 Dustseparator for cooling air in gas turbine |
| 01/23/2002 | EP1174587A2 Method of adjusting component airflow |
| 01/23/2002 | EP1174586A1 Cooling channels for a rotor of a machine or engine |
| 01/23/2002 | EP1174210A2 Method and blank for manufacturing rhomboidal blades for axial-flow fluid machines |
| 01/23/2002 | EP1173664A1 Cooling air system |
| 01/23/2002 | EP1173657A1 Turbine blade and method for producing a turbine blade |
| 01/23/2002 | EP1173656A1 High pressure turbine cooling of gas turbine engine |
| 01/23/2002 | CN1078309C 水利机械 Water Machinery |
| 01/22/2002 | US6340284 Turbine blade with actively cooled shroud-band element |
| 01/22/2002 | US6339878 Method of repairing an airfoil |
| 01/17/2002 | WO2001040660A3 Centrifugal impeller assembly |
| 01/17/2002 | US20020006329 Nozzle airfoil having movable nozzle ribs |
| 01/16/2002 | EP1172524A2 Method for deploying shroud segments of different thickness in a turbine engine |
| 01/16/2002 | EP1172523A2 Method and apparatus for supplying cooling air to turbine rotors |
| 01/16/2002 | EP1172460A2 A method for applying a high-temperature bond coat on a metal substrate |
| 01/16/2002 | CN1331380A Fan vane with same shape as its seat |
| 01/15/2002 | US6339208 Method of forming cooling holes |
| 01/15/2002 | US6338611 Conforming platform fan blade |
| 01/15/2002 | US6338609 Convex compressor casing |
| 01/15/2002 | CA2065679C Shroud cooling assembly for gas turbine engine |
| 01/15/2002 | CA2039990C Steam turbine integral control stage blade group |
| 01/10/2002 | US20020004143 Multilayer; substrates, adhesion layer |
| 01/10/2002 | US20020004010 Retention system and method for the blades of a rotary machine |
| 01/10/2002 | US20020004002 Turbo machines |
| 01/09/2002 | EP1170463A2 Turbine disc |
| 01/09/2002 | EP1169495A1 Electrochemical stripping of turbine blades |
| 01/09/2002 | EP0913492B1 Low heat expansion alloy |
| 01/09/2002 | EP0760051B2 Airfoil with dual source cooling |
| 01/09/2002 | EP0723625B1 Active tip flow bypass in stator vane channel |
| 01/09/2002 | CN1330209A Turbomachine blade unit |
| 01/09/2002 | CN1330208A Guide blade with consistent base |
| 01/08/2002 | US6336790 Axial flow power tool turbine machine |
| 01/08/2002 | CA2252274C Gas turbine spindle bolt seal device |
| 01/08/2002 | CA2230325C Steam cooled gas turbine system |
| 01/08/2002 | CA2030989C High temperature - low temperature rotor for turbines |
| 01/03/2002 | WO2002001036A1 Drilling turbine |
| 01/03/2002 | DE10031116A1 Axial securing device for rotor blades of axial turbo machines, consists of securing body with power-absorbent section and securing section with two holder elements |
| 01/02/2002 | EP1167840A1 Brush seal for turbomachine airfoils |
| 01/02/2002 | EP1167721A2 Method and system for cooling a gas turbine plant |
| 01/02/2002 | EP1167694A2 Cooled nozzle vane |