| 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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| 06/20/2012 | EP2464829A2 Turbine blade having a constant thickness airfoil skin |
| 06/20/2012 | EP2464828A1 Vibration-damping shim for a fan blade |
| 06/20/2012 | EP2154265B1 A method for manufacturing a part of a rotary machine |
| 06/20/2012 | CN202280481U 低阻涵流式空气涡轮发电系统 Low resistance bypass air flow turbine power generation system |
| 06/20/2012 | CN1982654B Blunt tip turbine blade |
| 06/20/2012 | CN102510953A Rotor disk for a turbo machine |
| 06/20/2012 | CN102505967A Rotor section for a rotor of a turbo machine, rotor blade for a turbo machine and blocking element |
| 06/20/2012 | CN101793166B Curved saw wheel steamer |
| 06/20/2012 | CN101528641B Composite material part with a silicon-containing ceramic matrix protected against corrosion |
| 06/20/2012 | CN101501302B Rotor blade for a high speed rotary-wing aircraft |
| 06/20/2012 | CN101153548B Stationary-rotating assemblies having surface features for enhanced containment of fluid flow, and related processes |
| 06/20/2012 | CN101148994B 灰孔圆顶叶片 Gray leaf dome hole |
| 06/19/2012 | US8202056 Morphable composite structure |
| 06/19/2012 | US8202054 Blade for a gas turbine engine |
| 06/19/2012 | US8202045 Blower fan for low profile environment |
| 06/19/2012 | CA2668750C Film cooling structure |
| 06/15/2012 | CA2760120A1 Thermal inspection and machining systems and methods of use |
| 06/14/2012 | WO2012078375A1 Bladed disk assembly |
| 06/14/2012 | WO2012077365A1 Radial turbine |
| 06/14/2012 | WO2012076591A1 Shroud of a rotor blade |
| 06/14/2012 | WO2012076588A1 Fluid flow machine especially gas turbine penetrated axially by a hot gas stream |
| 06/14/2012 | WO2012076581A1 Axial-flow machine |
| 06/14/2012 | US20120148412 Fatigue resistant cast titanium alloy articles |
| 06/14/2012 | US20120148406 Turbine rotor disks and turbine assemblies |
| 06/14/2012 | US20120148405 Cooling circuit for a drum rotor |
| 06/14/2012 | US20120148401 Blade disk arrangement for blade frequency tuning |
| 06/14/2012 | US20120148396 Fluid-flow machine - blade with hybrid profile configuration |
| 06/14/2012 | US20120148383 Gas turbine vane with cooling channel end turn structure |
| 06/14/2012 | DE102011056346A1 Verfahren zur Herstellung einer Komponente mit einer zweischichtigen Strukturbeschichtung A process for preparing a component having a two layer coating structure |
| 06/14/2012 | DE102011056345A1 Kühlkreislauf für einen trommelartigen Rotor Cooling circuit for a drum-like rotor |
| 06/14/2012 | DE102011056321A1 Singlet-Leitapparatkonstruktion einer Dampfturbine für eine von hinten bestückte Anordnung Singlet Leitapparatkonstruktion a steam turbine for a populated from behind arrangement |
| 06/14/2012 | DE102011056181A1 Komponenten mit Kühlkanälen und Herstellungsverfahren Components with cooling channels and methods of manufacture |
| 06/14/2012 | DE102010063071A1 Kühlvorrichtung für ein Strahltriebwerk A cooling apparatus for a jet engine |
| 06/14/2012 | DE102010053798A1 Strömungsmaschine - Schaufel mit hybrider Profilgestaltung Flow machine - blade with hybrid tread design |
| 06/14/2012 | DE102004057025B4 Verfahren zum Installieren von ortsfesten Schaufeln einer Turbine und Turbinenstruktur mit einem radialen Spannstift Method for installing stationary blades of a turbine and turbine structure with a radial clamping pin |
| 06/14/2012 | CA2819893A1 Fluid flow machine especially gas turbine penetrated axially by a hot gas stream |
| 06/14/2012 | CA2819026A1 Bladed disk assembly |
| 06/13/2012 | EP2463481A2 Blade disk arrangement for blade frequency tuning |
| 06/13/2012 | EP2463480A2 Blade with hybrid airfoil |
| 06/13/2012 | EP2463479A2 Turbine rotor disks and turbine assemblies |
| 06/13/2012 | EP2463406A2 Steam turbine |
| 06/13/2012 | EP2462352A1 Hub for a propeller having variable pitch blades |
| 06/13/2012 | EP2462320A2 Blade |
| 06/13/2012 | EP2461938A1 Optimized method for manufacturing a one-piece bladed disc by abrasive water jet |
| 06/13/2012 | EP2461937A1 Optimized method for manufacturing a one-piece bladed disc by abrasive water jet |
| 06/13/2012 | EP2461936A1 Repair of turbine components and solder alloy therefor |
| 06/13/2012 | CN1995708B Blade with parallel serpentine cooling channels |
| 06/13/2012 | CN1982655B Z-shape cooled turbine airfoil |
| 06/13/2012 | CN1970995B Axial and circumferential seal for stacked rotor and/or stator assembly |
| 06/13/2012 | CN1818349B High efficiency fan cooling holes for turbine airfoil |
| 06/13/2012 | CN102498264A Blade fastening having safety device for turbine blades |
| 06/13/2012 | CN102498263A Method and device for testing profiled grooves |
| 06/13/2012 | CN102493849A Turbine blade |
| 06/13/2012 | CN101980821B Improved method for making a one-piece bladed disk, with temporary retaining ring for bladed disks removed before a milling step |
| 06/13/2012 | CN101535654B Transonic airfoil and axial flow rotary machine |
| 06/13/2012 | CN101432504B Method of fabrication of a turbine or compressor component and turbine and compressor component |
| 06/13/2012 | CN101351620B Closure unit for the remaining space between the first and the last blades of a bladed ring inserted in a circumferencial slot of a turbomachine, and corresponding turbomachine |
| 06/13/2012 | CN101326342B Turbo-machine blade |
| 06/13/2012 | CN101063412B Nested turbine bucket closure group |
| 06/13/2012 | CN101029581B Methods and apparatus for cooling gas turbine rotor blades |
| 06/13/2012 | CN101025091B Bucket platform cooling circuit and method |
| 06/13/2012 | CN101021164B Methods and apparatus for turbine engine rotors |
| 06/12/2012 | US8197950 Dense vertically cracked thermal barrier coatings |
| 06/12/2012 | US8197213 Turboprop including a set of adjustable-pitch blades |
| 06/12/2012 | US8197211 Composite air cooled turbine rotor blade |
| 06/12/2012 | US8197210 Turbine vane with leading edge insert |
| 06/12/2012 | US8197197 Method of matching thermal response rates between a stator and a rotor and fluidic thermal switch for use therewith |
| 06/12/2012 | US8197191 Inlet section of an aircraft engine nacelle |
| 06/12/2012 | US8197189 Vibration damping of a static part using a retaining ring |
| 06/12/2012 | US8197185 Apparatus and method for cooling a turbine airfoil arrangement in a gas turbine engine |
| 06/12/2012 | CA2564172C Method for the application of a protective coating to a thermally stressed component |
| 06/12/2012 | CA2558838C Rotor end piece |
| 06/08/2012 | CA2761208A1 Blade disk arrangement for blade frequency tuning |
| 06/07/2012 | WO2012072903A1 Wear-resistant part for the support of a blade of a turbojet engine fan |
| 06/07/2012 | WO2012072384A1 Turbomachine with sealing structure between rotating and positionally fixed parts, and method for manufacturing said sealing structure |
| 06/07/2012 | WO2012072069A1 Damping means for damping a blade movement of a turbomachine |
| 06/07/2012 | WO2012022297A3 Method for connecting a turbine blade or vane to a turbine disc or to a turbine ring |
| 06/07/2012 | US20120141293 Ni-based heat resistant alloy, gas turbine component and gas turbine |
| 06/07/2012 | US20120141289 Airfoil with wrapped leading edge cooling passage |
| 06/07/2012 | US20120141288 Fabricating parts with composite material reinforcement having a single crossing line |
| 06/07/2012 | US20120141283 Rotor blade for a wind turbine and methods of manufacturing the same |
| 06/07/2012 | US20120141276 Frequency-dependent damper and rotary wing system |
| 06/07/2012 | US20120141261 Composite shroud and methods for attaching the shroud to plural blades |
| 06/07/2012 | CA2795466A1 Wear-resistant part for the support of a blade of a turbojet engine fan |
| 06/06/2012 | EP2460980A2 Method for producing an integrated bladed rotor |
| 06/06/2012 | EP2460979A1 Blade segment of a flow engine with radial support surfaces |
| 06/06/2012 | EP2460978A1 Variable geometry inlet guide vane |
| 06/06/2012 | EP2460977A1 Variable geometry inlet guide vane |
| 06/06/2012 | EP2460976A2 Gas turbine rotor containment |
| 06/06/2012 | EP2460612A1 Method of manufacturing a rotor by vertical welding, with at least one slot at the upper part being welded the last |
| 06/06/2012 | EP2459781A1 Method for manufacturing a thermal barrier |
| 06/06/2012 | EP2209588B1 A method for producing a vane, such a vane and a stator component comprising the vane |
| 06/06/2012 | DE102011055942A1 Dampfturbinensingulettverbindung für Leitapparate einer Grenzstufe mit verstiftetem oder verschraubtem innerem Ring Dampfturbinensingulettverbindung for nozzles with a cutoff level verstiftetem or bolted inner ring |
| 06/06/2012 | DE102010053170A1 Verfahren zur Herstellung einer Kantenschutzbeschichtung für Rotorblätter einer Windenergieanlage und entsprechende Kantenschutzbeschichtung A method for producing a protective coating edges for rotor blades of a wind turbine and the corresponding edge protection coating |
| 06/06/2012 | CN202266301U Turbine machine and turbine engine with same |
| 06/06/2012 | CN102485934A Method for preparing hollow blade inner chamber diffusion layer with high temperature resistance, oxidation resistance and corrosion resistance |
| 06/05/2012 | US8192168 Airfoil shape for a compressor blade |
| 06/05/2012 | US8192167 Blade fastening means of a turbine |
| 06/05/2012 | US8192166 Tip shrouded turbine blade with sealing rail having non-uniform thickness |
| 06/05/2012 | US8192165 Impeller of multiblade fan and multiblade fan having the same |