| 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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| 01/23/2012 | CA2747121A1 Components with bonded edges |
| 01/20/2012 | DE202011108099U1 Dampfturbinenrotor Steam turbine rotor |
| 01/19/2012 | WO2012009021A2 Apparatus for non-clogging pumps |
| 01/19/2012 | WO2012008452A1 Fan rotor blade and fan |
| 01/19/2012 | WO2012007716A1 Vane assembly for an axial flow turbine |
| 01/19/2012 | WO2012007682A1 Method for producing a solid part |
| 01/19/2012 | WO2012007320A1 Porous ceramic coating system |
| 01/19/2012 | WO2011139313A3 Gas turbine engine vanes |
| 01/19/2012 | WO2011136833A3 Gas turbine engine and main engine rotor assembly and disassembly |
| 01/19/2012 | US20120014810 Turbine vane with dusting hole at the base of the blade |
| 01/19/2012 | US20120014809 High pressure turbine vane cooling hole distrubution |
| 01/19/2012 | US20120014808 Near-wall serpentine cooled turbine airfoil |
| 01/19/2012 | US20120014803 Turbine blade having material block and related method |
| 01/19/2012 | US20120014802 Dovetail connection for turbine rotating blade and rotor wheel |
| 01/19/2012 | US20120014800 Fan assembly |
| 01/19/2012 | US20120014783 Apparatus For Non-Clogging Pumps |
| 01/19/2012 | US20120014782 Turbocharger bearing housing assembly |
| 01/19/2012 | DE102010027588A1 Fan-Nachleitradschaufel eines Turbofantriebwerks Fan downstream guide vane of a turbofan engine |
| 01/19/2012 | DE102009033835B4 Verfahren zum Austauschen einer Schaufel eines Rotors mit integrierter Beschaufelung und ein derartiger Rotor A method for replacing a blade of a rotor with integrated blading and such a rotor |
| 01/19/2012 | DE10001109B4 Gekühlte Schaufel für eine Gasturbine Cooled blade for a gas turbine |
| 01/19/2012 | CA2805337A1 Fan rotor blade and fan |
| 01/19/2012 | CA2804957A1 Method for producing a solid part |
| 01/19/2012 | CA2746397A1 High pressure turbine vane cooling hole distribution |
| 01/18/2012 | EP2407637A2 Dovetail connection for turbine rotating blade and rotor wheel |
| 01/18/2012 | EP2407579A1 Porous ceramic coating system |
| 01/18/2012 | EP2407247A1 Turbine of a rotary dispenser |
| 01/18/2012 | EP2406484A1 Device for driving a pair of counter-rotating propellers by means of an epicyclic gear train |
| 01/18/2012 | EP2406465A1 Rotor for turbomachines with shrouded blades |
| 01/18/2012 | EP2406464A1 Rotor for turbomachines |
| 01/18/2012 | EP2406463A1 Turbine vane with dusting hole at the base of the blade |
| 01/18/2012 | EP2406462A1 Rotor element with a fluid passage and passage-blocking member, and turbine engine including the rotor element |
| 01/18/2012 | CN102325964A Method and device for cooling steam turbine generating equipment |
| 01/18/2012 | CN102322297A Corrosion-resistant nuclear steam turbine rotor and machining method thereof |
| 01/18/2012 | CN102321887A 38CrMoAl compressor blade subjected to composite surface modification and preparation process thereof |
| 01/18/2012 | CN101596665B Technology method for connecting three-body structure of titanium aluminum alloy turbine rotation shaft |
| 01/18/2012 | CN101517199B 涡轮增压器 Turbocharger |
| 01/18/2012 | CN101341312B Diagonal flow turbine, or radial turbine |
| 01/17/2012 | US8097303 Methods for producing multilayered, oxidation-resistant structures on substrates |
| 01/17/2012 | US8096778 Structural beam for a wind generator blade production method thereof |
| 01/17/2012 | US8096777 Mixed flow turbine or radial turbine |
| 01/17/2012 | US8096772 Turbine vane for a gas turbine engine having serpentine cooling channels within the inner endwall |
| 01/17/2012 | US8096771 Trailing edge cooling slot configuration for a turbine airfoil |
| 01/17/2012 | US8096770 Trailing edge cooling for turbine blade airfoil |
| 01/17/2012 | US8096769 Damper |
| 01/17/2012 | US8096768 Turbine blade with trailing edge impingement cooling |
| 01/17/2012 | US8096767 Turbine blade with serpentine cooling circuit formed within the tip shroud |
| 01/17/2012 | US8096766 Air cooled turbine airfoil with sequential cooling |
| 01/17/2012 | US8096756 Apparatus and method for controlling a compressor |
| 01/17/2012 | US8096752 Method and apparatus for cooling a transition piece |
| 01/17/2012 | US8096751 Turbine engine component with cooling passages |
| 01/17/2012 | US8096748 Apparatus and method for double flow turbine first stage cooling |
| 01/17/2012 | US8096747 Apparatus and related methods for turbine cooling |
| 01/12/2012 | WO2012005324A1 Turbine blade and engine component |
| 01/12/2012 | WO2012004525A1 Thermal barrier for turbine blades, having a columnar structure with spaced-apart columns |
| 01/12/2012 | WO2012004094A1 Combined sealing and balancing arrangement for a turbine disc |
| 01/12/2012 | WO2011102746A3 Turbine with radial inlet and outlet rotor for use in bidirectional flows |
| 01/12/2012 | WO2011051362A3 Turbine blade of a turbine stage of a steam turbine and rotor blading or guide blading of a turbine stage of a steam turbine |
| 01/12/2012 | US20120009071 Cmc turbine stator blade |
| 01/12/2012 | US20120009069 Method to manufacture a component of a composite structure |
| 01/12/2012 | US20120009067 Rotor of a Turbomachine |
| 01/12/2012 | US20120009065 Rotor blade |
| 01/12/2012 | DE102010031213A1 Rotor einer Turbomaschine Rotor of a turbomachine |
| 01/12/2012 | CA2804632A1 Turbine blade and engine component |
| 01/12/2012 | CA2803160A1 Thermal barrier for turbine blades, having a columnar structure with spaced-apart columns |
| 01/11/2012 | EP2405117A1 Approach to extending life of gas turbine engines |
| 01/11/2012 | EP2405101A2 A composite turbomachine blade |
| 01/11/2012 | EP2405100A1 Combined sealing and balancing arrangement for a turbine disc |
| 01/11/2012 | EP2405029A1 Method for producing an adhesive scratch-proof protective coating on a metallic workpiece |
| 01/11/2012 | EP2404038A1 Integrally bladed rotor and method for producing an integrally bladed rotor |
| 01/11/2012 | EP2404037A1 Integrally bladed rotor for a turbomachine |
| 01/11/2012 | EP2404036A1 Method for producing an integrally bladed rotor |
| 01/11/2012 | CN202108546U 1800 mm last stage rotor blade on half-speed nuclear turbine |
| 01/11/2012 | CN102317579A Turbine blade assembly including a damper |
| 01/11/2012 | CN102317578A Blade union of a turbo machine |
| 01/11/2012 | CN102317577A Rotor section for a rotor of a turbomachine, rotor blade for a turbomachine |
| 01/11/2012 | CN102317576A Method for heating a turbine shaft |
| 01/11/2012 | CN102312683A Air film hole based on secondary flows of bent passage |
| 01/11/2012 | CN102312682A A composite turbomachine blade |
| 01/11/2012 | CN101535602B 涡轮叶片 Turbine blades |
| 01/11/2012 | CN101089369B Hybrid blade for a steam turbine |
| 01/10/2012 | US8092189 Axial flow pump |
| 01/10/2012 | US8092188 Variable geometry fan and method for manufacturing the blades thereof |
| 01/10/2012 | US8092187 Flatback insert for turbine blades |
| 01/10/2012 | US8092185 Impeller and cooling fan incorporating the same |
| 01/10/2012 | US8092182 Wind turbine blade support structure |
| 01/10/2012 | US8092181 Resin cross flow fan and manufacturing method thereof |
| 01/10/2012 | US8092179 Blade tip cooling groove |
| 01/10/2012 | US8092178 Turbine blade for a gas turbine engine |
| 01/10/2012 | US8092177 Turbine airfoil cooling system with diffusion film cooling hole having flow restriction rib |
| 01/10/2012 | US8092176 Turbine airfoil cooling system with curved diffusion film cooling hole |
| 01/10/2012 | US8092175 Turbine blade |
| 01/10/2012 | US8092172 Method for operating a wind turbine with reduced blade fouling |
| 01/10/2012 | US8092161 Thermal shield at casing joint |
| 01/10/2012 | US8092159 Feeding film cooling holes from seal slots |
| 01/10/2012 | US8092152 Device for cooling slots of a turbomachine rotor disk |
| 01/05/2012 | WO2012003065A1 Solid state resistance welding for airfoil repair and manufacture |
| 01/05/2012 | WO2012001324A1 Process for manufacturing a metal part by selectively melting a powder |
| 01/05/2012 | WO2012001279A1 Blade having an integrated composite spar |
| 01/05/2012 | WO2012001278A1 Turbomachine blade having an even/odd complementary geometry and its manufacturing process |
| 01/05/2012 | WO2012001269A1 Turbomachine blade with complementary asymetric geometry |