| 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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| 02/05/2004 | US20040022630 Gas turbine blade |
| 02/05/2004 | US20040022629 Turbine blade or vane |
| 02/05/2004 | US20040022622 Gas turbine |
| 02/05/2004 | US20040021828 Laser projection system to facilitate layup of complex composite shapes |
| 02/05/2004 | US20040020216 Anti-score plates |
| 02/05/2004 | US20040020203 High-pressure ratio turbocharger |
| 02/05/2004 | US20040020186 Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines |
| 02/05/2004 | US20040020049 Process and blank for preparing rhomboidal blades for axial turbo engines |
| 02/04/2004 | EP1387060A2 Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines |
| 02/04/2004 | EP1387040A1 Method of protecting partial areas of a component |
| 02/04/2004 | EP1386980A2 Process for coating the interior of gas turbine blades |
| 02/04/2004 | EP1386060A1 Turbine or compressor device and method for assembling the device |
| 02/04/2004 | EP1386058A1 Structure comprising a rotor and fixed perturbation sources and method for reducing vibrations in said structure |
| 02/04/2004 | EP1385668A1 Method of repairing a turbin blade tip |
| 02/04/2004 | CN1473236A Sealing structure of spindle bolt and gas turbine |
| 02/03/2004 | US6686060 Yttria-stabilized zirconia containing niobia and/or titania; reducing thermal conductivity; gas turbine engine protective film |
| 02/03/2004 | US6685435 Turbine blade assembly with stranded wire cable dampers |
| 02/03/2004 | US6685434 Second stage turbine bucket airfoil |
| 02/03/2004 | US6685431 Method for repairing a turbine vane |
| 02/03/2004 | US6684626 Aircraft gas turbine engine with control vanes for counter rotating low pressure turbines |
| 01/31/2004 | CA2435192A1 Hollow fan hub under blade bumper |
| 01/29/2004 | US20040018299 Method of forming a diffusion coating on the surface of a workpiece |
| 01/29/2004 | US20040018092 Methods and apparatus for manufacturing rotor shafts |
| 01/29/2004 | US20040018091 Turbomachine blade |
| 01/29/2004 | US20040018082 Cooling structure of stationary blade, and gas turbine |
| 01/29/2004 | US20040016853 Method and apparatus for modulating flow separation |
| 01/29/2004 | US20040016239 Miniature gas turbine engine with unitary rotor shaft for power generation |
| 01/29/2004 | DE10233033A1 Strömungs-Arbeits-Maschine mit überhöhtem Rotor-Stator-Kontraktionsverhältnis Flow-working machine with excessive rotor-stator contraction ratio |
| 01/29/2004 | DE10202995B4 Rotorblatt für eine Windkraftanlage mit einer Dämpfereinrichtung Rotor blade for a wind turbine with a damper device |
| 01/28/2004 | EP1384897A2 Method and apparatus for modulating flow separation |
| 01/28/2004 | EP1384896A2 Method and apparatus for modulating airfoil lift |
| 01/28/2004 | EP1384855A2 Cooling structure of stationary blade, and gas turbine |
| 01/28/2004 | EP1384854A2 Methods and apparatus for manufacturing rotor shafts |
| 01/28/2004 | EP1384539A1 Metal matrix composite part and process for its manufacture |
| 01/28/2004 | EP1183442B1 Cast on-board injection nozzle with adjustable flow area |
| 01/28/2004 | EP0911488B1 Gas turbine cooled stationary blade |
| 01/28/2004 | CN1470745A Dovetail pin drilling method |
| 01/27/2004 | US6683641 Apparatus for inspecting the interior of hollow articles |
| 01/27/2004 | US6682821 Substrates selected from silicon nitride, carbide or sialon, having protective coatings for use in internal combustion engines, turbines, rotors, nozzles, linings or ducts; heat and wear resistance |
| 01/27/2004 | US6682306 Moving blades for steam turbine |
| 01/27/2004 | US6682304 Cooled gas turbine blade |
| 01/27/2004 | US6682301 Reduced shock transonic airfoil |
| 01/27/2004 | US6682022 Boundary layer control of aerodynamic airfoils |
| 01/27/2004 | US6682021 System and method for actively manipulating and controlling fluid flow over a surface |
| 01/22/2004 | WO2004007913A1 Improved low cycle fatigue life (lcf) impeller design concept |
| 01/22/2004 | US20040013802 Metal-organic chemical vapor deposition (MOCVD); for use with aircraft |
| 01/22/2004 | US20040013528 Fan blade assembly |
| 01/22/2004 | US20040013525 Aerofoil |
| 01/22/2004 | US20040013523 Method of distributing rotor blades in a turbomachine |
| 01/22/2004 | US20040013521 Hybrid rotor, method of manufacturing the hybrid rotor, and gas turbine |
| 01/22/2004 | US20040013520 Fluid flow machine (turbomachine) with increased rotor-stator ratio |
| 01/22/2004 | US20040013518 Gas turbine engine casing and rotor blade arrangement |
| 01/22/2004 | US20040013516 System to feed cooling air into a gas turbine rotor |
| 01/22/2004 | US20040013515 Turbine blade having angled squealer tip |
| 01/22/2004 | US20040012151 Sealing arrangement |
| 01/22/2004 | US20040011443 Nickel base superalloys and turbine components fabricated therefrom |
| 01/22/2004 | US20040011012 Rotary machine |
| 01/21/2004 | EP1382858A1 Distribution method for rotor blades of a turbomachine |
| 01/21/2004 | EP1382800A2 A fan blade assembly |
| 01/21/2004 | EP1382799A2 Gas turbine engine casing and rotor blade arrangement |
| 01/21/2004 | EP1382798A2 Rotary machine |
| 01/21/2004 | EP1382797A2 Fluid machine flow path with increased stage contraction ratios |
| 01/21/2004 | EP1382715A1 Protection of a gas turbine component by a vapor-deposited oxide coating |
| 01/21/2004 | EP1382697A1 Superalloy for single crystal turbine vanes |
| 01/21/2004 | EP1381481A2 Multi-wall core and process |
| 01/21/2004 | CN1469792A Process for drilling holes in a metallic workpiece having a thermal barrier coating |
| 01/21/2004 | CN1469035A 涡轮 Turbine |
| 01/21/2004 | CN1469030A Turbine blade wall cooling device and producing method thereof |
| 01/21/2004 | CN1135148C Non-circular shape cooling hole and processing method thereof |
| 01/20/2004 | US6679681 Flush tenon cover for steam turbine blades with advanced sealing |
| 01/15/2004 | WO2004005581A1 Highly oxidation resistant component |
| 01/15/2004 | WO2004005580A1 Highly oxidation resistant component |
| 01/15/2004 | WO2004005565A1 Casting steel having high strength and low thermal expansion |
| 01/15/2004 | WO2004004953A2 Diffusion bond mixture for healing single crystal alloys |
| 01/15/2004 | WO2002027145A8 Vane assembly for a turbine and combustion turbine with this vane assembly |
| 01/15/2004 | US20040009072 Method for manufacturing a turbine wheel rotor |
| 01/15/2004 | US20040009067 Impeller for an axial flow fan and a method of mounting a blade on a hub for such fan |
| 01/15/2004 | US20040009066 Turbine blade and gas turbine |
| 01/15/2004 | US20040009060 Low cycle fatigue life (LCF) impeller design concept |
| 01/15/2004 | US20040007830 Sealing structure of spindle bolt, and gas turbine |
| 01/15/2004 | DE19858913B4 Schutzschicht Protective layer |
| 01/14/2004 | EP1380759A1 Stress defender holes in jointings |
| 01/14/2004 | EP1380725A2 Method of producing and assembling a cooling device inside an axial-flow gas turbine blade, and blade produced using such a method |
| 01/14/2004 | EP1380724A2 Cooled turbine blade |
| 01/14/2004 | EP1380723A1 Cooling method and pre-swirler for gas turbine blades as well as a turbine comprising such a pre-swirler |
| 01/14/2004 | EP1380722A1 Balancing apparatus and method for rotor shaft flange |
| 01/14/2004 | EP1380672A1 Highly oxidation resistant component |
| 01/14/2004 | EP1380657A1 Single sided laser shock peening |
| 01/14/2004 | CN1467366A Failsafe film cooled wall |
| 01/14/2004 | CN1467365A Structural cover for gas turbine engine bolted flanges |
| 01/14/2004 | CN1467364A Rotor blade for a centripetal turbine |
| 01/13/2004 | US6677560 Apparatus for inductively heating a workpiece |
| 01/13/2004 | US6677064 Device adapted for use in a high temperature environment in excess of about 1200 degrees c., comprising: ceramic single oxide base layer disposed on the substrate surface; and ceramic oxide reaction product material disposed on the base |
| 01/13/2004 | US6676992 Article protected by a diffusion aluminide coating applied by painting techniques |
| 01/13/2004 | US6676381 Method and apparatus for casting near-net shape articles |
| 01/13/2004 | US6676380 Turbine blade assembly with pin dampers |
| 01/13/2004 | US6676378 Turbomachine stator flap, and a method of manufacturing it |
| 01/12/2004 | CA2435070A1 Method of producing and assembling a cooling device inside an axial-flow gas turbine blade, and axial-flow gas turbine blade produced using such a method |
| 01/08/2004 | WO2004003390A1 Restraining device for fan blade root |
| 01/08/2004 | WO2004003347A1 Gas turbine ventilation circuitry |