| 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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| 01/22/2008 | CA2461699C Hybrid ceramic material composed of insulating and structural ceramic layers |
| 01/19/2008 | CA2594046A1 Procedure for the manufacture of a one-piece bladed disc and mold used in said procedure |
| 01/18/2008 | CA2582899A1 Highly slenderness rotor |
| 01/17/2008 | WO2008006797A1 Turbocharger having a catalytic coating |
| 01/17/2008 | WO2008006692A1 Reduction of flexural vibration amplitudes of turbine rotors |
| 01/17/2008 | WO2007107602A3 Quasicrystalline compound and the use thereof as a heat insulating layer |
| 01/17/2008 | US20080014347 Method for manufacturing a erosion preventative diamond-like coating for a turbine engine compressor blade |
| 01/17/2008 | US20080014095 Turbofan engine and method of operating the same |
| 01/17/2008 | US20080014094 Coated bucket damper pin |
| 01/17/2008 | US20080014084 Turbofan case and method of making |
| 01/17/2008 | US20080014083 Turbofan case and method of making |
| 01/17/2008 | US20080010996 Turbofan case and method of making |
| 01/17/2008 | US20080010970 Turbofan case and method of making |
| 01/17/2008 | DE102007023681A1 Turbocharger has profile center line with curved region between trailing edge and first transition point, straight region between first and second transition points, further curved region between second transition point and leading edge |
| 01/17/2008 | DE102006031388A1 Verfahren für die Reparatur und/oder den Austausch von Einzelelementen eines Bauteils einer Gasturbine A method for the repair and / or replacement of individual elements of a component of a gas turbine |
| 01/16/2008 | EP1878879A1 Turbocharger with catalytic coating |
| 01/16/2008 | EP1878874A2 Integral main body-tip microcircuite for blades |
| 01/16/2008 | EP1878873A2 Turbine engine alloys and crystalline orientations |
| 01/16/2008 | EP1878872A2 Turbofan engine and its blades |
| 01/16/2008 | EP1878871A1 Reduction of the amplitude of rotor flexural vibrations |
| 01/16/2008 | EP1877218A1 Method of repairing a threaded generator rotor blower assembly |
| 01/16/2008 | EP1432571B1 Hybrid ceramic material composed of insulating and structural ceramic layers |
| 01/16/2008 | EP1287173B1 $g(G)-TIAL ALLOY-BASED COMPONENT COMPRISING AREAS HAVING A GRADUATED STRUCTURE |
| 01/16/2008 | EP1012445B2 Blade for a turbo-machine |
| 01/16/2008 | CN101105429A Turbine blade fatigue life evaluating method |
| 01/16/2008 | CN101105150A An engine core stand arrangement and method of removal and transportation of an engine core |
| 01/16/2008 | CN100362213C Turbine bucket tip shroud edge profile |
| 01/16/2008 | CN100362212C Hot gas path component with a meshed and dimpled cooling structure |
| 01/16/2008 | CN100362211C Airfoil shape for a turbine bucket |
| 01/15/2008 | US7318704 Gas turbine engine structure |
| 01/15/2008 | CA2449335C Turbine blade and gas turbine |
| 01/15/2008 | CA2251756C Strain tolerant ceramic coating |
| 01/10/2008 | WO2008004877A1 Sealing means between rotor and housing in a water turbine |
| 01/10/2008 | WO2008003651A1 Secondary ventilation system for turbocharger turbine |
| 01/10/2008 | US20080008599 Integral main body-tip microcircuits for blades |
| 01/10/2008 | US20080008598 Turbine airfoil cooling system with near wall vortex cooling chambers |
| 01/10/2008 | US20080008595 Compressor wheel |
| 01/10/2008 | US20080008594 Disk wheel of a rotor of a turbomachine |
| 01/10/2008 | US20080008593 Turbine blade self locking seal plate system |
| 01/10/2008 | US20080008589 Method and apparatus for balancing gas turbine engines |
| 01/10/2008 | US20080008581 Rotor for jet turbine engine having both insulation and abrasive material coatings |
| 01/10/2008 | CA2655939A1 Sealing means between rotor and housing in a water turbine |
| 01/09/2008 | EP1876336A2 Gas turbine component for jet engines and method for manufacturing gas turbine components for jet engines |
| 01/09/2008 | EP1876335A1 Secondary-air system for turbocharger turbine |
| 01/09/2008 | EP1876325A2 External datum system and film cooling hole positioning using core locating holes |
| 01/09/2008 | EP1876324A2 Gas turbine blade |
| 01/09/2008 | EP1875058A1 Gas turbine engine cooling system and method |
| 01/09/2008 | EP1875045A1 Turbine wheel |
| 01/09/2008 | CN101103178A 可变喷嘴涡轮增压器 Variable nozzle turbocharger |
| 01/09/2008 | CN101102867A Method for local application of diffusion aluminide coating |
| 01/09/2008 | CN101100951A Gradually widened slot staggered rib passage suitable for internal cooling member as turbine blade |
| 01/09/2008 | CN100360713C Anti-corrosion heat-resistant zine diffusion alloy claddiy material |
| 01/08/2008 | US7316539 Vane assembly with metal trailing edge segment |
| 01/08/2008 | CA2426135C Fan blade compliant shim |
| 01/08/2008 | CA2353904C Reduction in the noise produced by a rotor blade of a wind turbine |
| 01/03/2008 | WO2008001043A1 Measurement of aerofoil blades |
| 01/03/2008 | WO2008000247A1 Method for the corrosion protection of ceramic surfaces, bodies comprising such ceramic surfaces and use thereof |
| 01/03/2008 | WO2008000014A2 Guide vane arrangement for a driving mechanism |
| 01/03/2008 | WO2007125382A3 Third stage turbine airfoil |
| 01/03/2008 | WO2003052240A3 Gas turbine system |
| 01/03/2008 | US20080004170 Sintered silicon nitride |
| 01/03/2008 | US20080003108 Turbomachine rotor and turbomachine comprising such a rotor |
| 01/03/2008 | US20080003107 Rotational airfoil balance system |
| 01/03/2008 | US20080003105 Cooling device |
| 01/03/2008 | US20080000610 Method of forming concavities in the surface of a metal component, and related processes and articles |
| 01/03/2008 | US20080000063 Component with a Filled Recess |
| 01/03/2008 | CA2652953A1 Guide-vane arrangement for an engine |
| 01/02/2008 | EP1873401A2 Turbomachine rotor and turbomachine comprising such a rotor |
| 01/02/2008 | EP1873356A1 Shaft for turbomachine and process for manufacturing |
| 01/02/2008 | EP1873355A1 Turbine rotor blade |
| 01/02/2008 | EP1873354A2 Leading edge cooling using chevron trip strips |
| 01/02/2008 | EP1873353A2 High coverage cooling hole shape |
| 01/02/2008 | EP1871922A2 Coating, substrate provided with a coating and method for the application of a corrosion-resistant coating |
| 01/02/2008 | EP1871567A2 Method of welding a gamma-prime precipitate strengthened material |
| 01/02/2008 | EP1871556A1 Bi-cast blade ring for multi-alloy turbine rotor |
| 01/02/2008 | EP1429917B1 Ceramic matrix composite structure having integral cooling passages and method of manufacture |
| 01/02/2008 | CN101096914A Turbomachine rotor and turbomachine comprising such a rotor |
| 01/02/2008 | CN100359142C Methods and apparatus for supplying cooling fluid to turbine nozzles |
| 01/02/2008 | CN100359137C First stage protective cover structure of turbomachine and reinforced maintenance method |
| 01/02/2008 | CN100359136C Housing for tubine blade and assembling method thereof |
| 01/02/2008 | CN100359135C Airfoil shape for a turbine bucket |
| 01/02/2008 | CN100359134C Turbine blades with notches on roots |
| 01/02/2008 | CN100359133C Gas turbine disc rim with air cooling duct shortened axially and declined peripherily |
| 01/01/2008 | US7314670 Welded component |
| 12/29/2007 | CA2593193A1 Turbine engine rotor and turbine engine comprising such a rotor |
| 12/27/2007 | WO2007148338A2 Rotor for a compressor |
| 12/27/2007 | US20070297918 Gas turbine engine with contoured air supply slot in turbine rotor |
| 12/27/2007 | US20070297917 Leading edge cooling using chevron trip strips |
| 12/27/2007 | US20070297916 Leading edge cooling using wrapped staggered-chevron trip strips |
| 12/27/2007 | US20070297914 Enhanced axial air mover system with grill |
| 12/27/2007 | US20070297910 Liner panel |
| 12/27/2007 | US20070297908 Turbine rotor blade groove entry slot lock structure |
| 12/27/2007 | US20070297905 Woven Turbomachine Impeller |
| 12/27/2007 | US20070297904 Compressor Of A Gas Turbine And Gas Turbine |
| 12/27/2007 | US20070297898 Aerofoil |
| 12/27/2007 | DE102006028279A1 Repairing method for gas turbine components, particularly for integral bladed gas turbine rotors, involves removing damaged section from gas turbine components, and repairing intermediate piece is repaired with two connecting sections |
| 12/26/2007 | EP1870563A1 Fluid injection system for a platform |
| 12/26/2007 | EP1870562A2 Compressor synchronising ring sector or turbomachine nozzle guide vane sector |
| 12/26/2007 | EP1870561A2 Leading edge cooling of a gas turbine component using staggered turbulator strips |
| 12/26/2007 | EP1870492A1 Metal phosphate coating for oxidation resistance |