| 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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| 11/13/2007 | US7293962 Cooled turbine blade or vane |
| 11/13/2007 | US7293961 Zigzag cooled turbine airfoil |
| 11/13/2007 | US7293956 Rolled ring air baffle for a gas turbine engine rotating cavity |
| 11/12/2007 | CA2587096A1 Aircraft engine compressor assembly comprising hammer attachment blades with inclined roots |
| 11/08/2007 | WO2007047096A3 Titanium-aluminide turbine wheel and shaft assembly, and method for making same |
| 11/08/2007 | US20070258822 Axial Fan |
| 11/08/2007 | US20070258820 Torque converter blade with self-locking blade tab |
| 11/08/2007 | US20070258815 Turbine blade with wavy squealer tip rail |
| 11/08/2007 | US20070258814 Turbine airfoil with integral chordal support ribs |
| 11/08/2007 | US20070258813 Rotor for a Power Plant |
| 11/08/2007 | DE3908166B4 Prallgekühltes Gebilde Impingement cooled structure |
| 11/08/2007 | DE102007020863A1 Drehende Maschinen und Zusammenbauverfahren Rotating machines and assembly method |
| 11/08/2007 | DE102007007090A1 Gas turbine has cooling air transfer system with several tubular nozzles which are independently arranged in a circle inside a chamber, encompass the rotor and can discharge cooling air |
| 11/08/2007 | CA2633323A1 Third stage turbine airfoil |
| 11/07/2007 | EP1852575A1 Stationary blade ring of axial compressor |
| 11/07/2007 | EP1852572A2 Ceramic matrix composite turbine engine vane |
| 11/07/2007 | EP1852524A2 Method for manufacturing thermal barrier coatings with improved thermal insulation characteristics |
| 11/07/2007 | EP1852521A1 Thermal barrier coatings and processes for applying same |
| 11/07/2007 | EP1243878B1 Cold air refrigerating system and turboexpander turbine for this system |
| 11/07/2007 | EP0919701B2 Sealing structure for joint surfaces of flanges of gas turbine |
| 11/07/2007 | CN101067382A Methods and apparatus for thermal barrier coatings with improved overall thermal insulation characteristics |
| 11/07/2007 | CN101067381A Gas turbine has cooling air transfer system |
| 11/07/2007 | CN100347414C Method of manufacturing steam turbine |
| 11/07/2007 | CN100347411C Gas-turbine engine turbon-nozzle arc section with single-branch open cavity hollow blade |
| 11/07/2007 | CN100347410C Uniform strength blade moulding of radical flow type turbine radial element impeller and its method |
| 11/07/2007 | CN100347409C Second stage turbine bucket airfoil |
| 11/07/2007 | CN100347408C First-stage high pressure turbine bucket airfoil |
| 11/07/2007 | CN100347317C Lower fluence boundary and low flow lasr shock peening |
| 11/06/2007 | US7291946 Damper for stator assembly |
| 11/06/2007 | US7291408 Thermal barrier coatings with low thermal conductivity |
| 11/06/2007 | US7290988 Device for blocking a ring for axially retaining a blade, associated rotor disk and retaining ring, and rotor and aircraft engine comprising them |
| 11/06/2007 | US7290986 Turbine airfoil with curved squealer tip |
| 11/06/2007 | US7290806 Assembly fixture |
| 11/06/2007 | US7290385 Approach to extending life of gas turbine engine |
| 11/01/2007 | WO2007122022A1 Turbine blade |
| 11/01/2007 | WO2007081957A3 Method of determining graph isomorphism in polynomial-time |
| 11/01/2007 | US20070253828 Damping arrangement for a blade of an axial turbine |
| 11/01/2007 | US20070253826 Shaped rotor blade for reduced loads and vibration |
| 11/01/2007 | US20070253823 Turbine blade tab attachment means for a torque converter dampening spring retainer and a method of manufacturing said attachment means |
| 11/01/2007 | US20070253822 System for retaining blades in a rotor |
| 11/01/2007 | US20070253820 Adjustable device for balancing a fan |
| 11/01/2007 | US20070253817 Hot Gas Component of a Turbomachine Including an Embedded Channel |
| 11/01/2007 | US20070253816 Vane platform cooling |
| 11/01/2007 | US20070253815 Cooled gas turbine aerofoil |
| 11/01/2007 | US20070251924 Method and apparatus for rebuilding gas turbine engines |
| 10/31/2007 | EP1849965A2 Vane platform cooling |
| 10/31/2007 | EP1849963A2 Nested turbine bucket closure group |
| 10/31/2007 | EP1849962A1 Retention system for blades on a rotor |
| 10/31/2007 | EP1849961A2 Enhanced serpentine cooling with flow divider |
| 10/31/2007 | EP1849960A2 Turbine blade having internal cooling passage |
| 10/31/2007 | EP1849959A2 Steam turbine and turbine rotor |
| 10/31/2007 | EP1849881A2 Steam turbine |
| 10/31/2007 | EP1848876A1 Method for prolonging the fatigue life of a blade footing of a turobmachine blade |
| 10/31/2007 | EP1727970B1 Method and apparatus for establishing the state of the rotor of a turbomachine |
| 10/31/2007 | CN101063414A Steam turbine and rotor |
| 10/31/2007 | CN101063412A Nested turbine bucket closure group |
| 10/31/2007 | CN101063411A Vane platform cooling |
| 10/31/2007 | CN100346060C Guider of radial flow turbine |
| 10/31/2007 | CN100346059C 涡轮叶片和燃气轮机 Turbine blades and turbine |
| 10/31/2007 | CN100346058C Turbo blade or vane |
| 10/30/2007 | US7287961 Retaining arrangement |
| 10/30/2007 | US7287960 Titanium aluminide wheel and steel shaft connection thereto |
| 10/30/2007 | US7287959 Blunt tip turbine blade |
| 10/30/2007 | US7287958 Methods and apparatus for assembling rotatable machines |
| 10/27/2007 | CA2585875A1 Rotor blade retention system |
| 10/26/2007 | CA2585846A1 Use of eddy currents to measure the thicknesses of walls, specifically blade walls |
| 10/25/2007 | WO2007119832A1 Ni-BASED HEAT-RESISTANT ALLOY FOR GAS TURBINE COMBUSTOR |
| 10/25/2007 | WO2007119696A1 Blade |
| 10/25/2007 | WO2007119404A1 Ni-BASE SUPERALLOY, METHOD FOR PRODUCING SAME, AND TURBINE BLADE OR TURBINE VANE COMPONENT |
| 10/25/2007 | WO2007095902A8 Method for producing and repairing an integrally bladed rotor |
| 10/25/2007 | US20070248465 Optimized aerodynamic profile for a turbine blade |
| 10/25/2007 | US20070248464 Nested Turbine Bucket Closure Group |
| 10/25/2007 | US20070248463 Wedge repair of mechanically retained vanes |
| 10/25/2007 | US20070248462 Multiple cooling schemes for turbine blade outer air seal |
| 10/25/2007 | US20070248457 Rub coating for gas turbine engine compressors |
| 10/25/2007 | US20070247806 Supporting frame with locating function |
| 10/25/2007 | US20070246183 Refractory metal core wall thickness control |
| 10/25/2007 | US20070246149 Method for fabricating integral composite structural material |
| 10/24/2007 | EP1847697A1 Method and device for a gas turbine reheat system. |
| 10/24/2007 | EP1847696A1 Component for a secondary combustion system in a gas turbine and corresponding gas turbine. |
| 10/24/2007 | EP1847684A1 Turbine blade |
| 10/24/2007 | EP1847683A1 Optimised aerodynamic profile for a turbine vane |
| 10/24/2007 | EP1847682A1 Method for supplying a fluid to the main gas stream in a turbine and associated turbine blade. |
| 10/24/2007 | EP1847681A2 Wedge repair of mechanically retained vanes |
| 10/24/2007 | EP1397533B1 Method and device for locally removing coatings from parts |
| 10/24/2007 | CN200964873Y Exhaust turbosupercharger transonic turbine for diesel locomotive |
| 10/24/2007 | CN101059080A Methods and apparatus for mechanical retainment of non-metallic fillers in pockets |
| 10/24/2007 | CN101058862A Booster turbine and method of manufacturing the same |
| 10/24/2007 | CN100344396C Process and apparatus for manufacturing a turbine component, turbine components and use of apparatus |
| 10/23/2007 | US7286966 Rotation planning apparatus and rotation planning system |
| 10/23/2007 | US7285312 Atomic layer deposition for turbine components |
| 10/23/2007 | US7284959 Apparatus and method for securing a rotor blade in a rotor of a turbine-type machine |
| 10/23/2007 | US7284958 Separable blade platform |
| 10/23/2007 | US7284957 Composite integrally bladed rotor |
| 10/23/2007 | CA2399710C Method for producing local aluminide coating |
| 10/20/2007 | CA2585815A1 Airfoil optimized for a turbine blade |
| 10/18/2007 | WO2007116621A1 Axial flow fluid device and blade |
| 10/18/2007 | WO2007115533A1 Method for repairing a guide vane segment |
| 10/18/2007 | US20070243071 Laser shock peened gas turbine engine compressor airfoil edges |
| 10/18/2007 | US20070243067 Gas turbine or compressor blade |