| 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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| 01/05/2012 | WO2012000742A1 Process for producing an adhesion- and scratch-resistant protective layer on a metallic workpiece |
| 01/05/2012 | US20120003103 Turbine rotor assembly |
| 01/05/2012 | US20120003102 Dense vertically cracked thermal barrier coatings |
| 01/05/2012 | US20120003101 Casting method for manufacturing a work piece |
| 01/05/2012 | US20120003100 Composite turbomachine blade |
| 01/05/2012 | US20120003099 Molten metal impeller |
| 01/05/2012 | US20120003097 Axial flow fan |
| 01/05/2012 | US20120003091 Rotor assembly for use in gas turbine engines and method for assembling the same |
| 01/05/2012 | US20120003082 Cooling device of turbocharger of engine for vehicle |
| 01/05/2012 | US20120003081 Air-cooled turbocharger with optional internal pressure relief valve |
| 01/05/2012 | US20120003077 Annular multi-rotor double-walled turbine |
| 01/05/2012 | DE19921644B4 Kühlbare Schaufel für eine Gasturbine Coolable blade for a gas turbine |
| 01/05/2012 | DE102011051388A1 Rotoranordnung zur Verwendung in Gasturbinen und Verfahren zur Montage derselben A rotor assembly for use in gas turbine and method of assembling the same |
| 01/05/2012 | DE102010026084A1 Applying material layer on workpiece made of material containing titanium aluminide, comprises heating workpiece by induction at preheating temperature and applying powdery additive on heated surface of workpiece by deposition welding |
| 01/05/2012 | DE102010025637A1 Method for manufacturing and repairing blisk, involves positioning blisk in original starting position of tool exactly corresponding to respective processing or measuring apparatus during welding and measuring processes |
| 01/05/2012 | CA2804098A1 Blade having an integrated composite spar |
| 01/05/2012 | CA2803561A1 Solid state resistance welding for airfoil repair and manufacture |
| 01/05/2012 | CA2803157A1 Process for manufacturing a metal part by selectively melting a powder |
| 01/05/2012 | CA2799707A1 Turbomachine blade having complementary even/odd geometry and its manufacturing method |
| 01/05/2012 | CA2799706A1 Turbomachine blade having complementary asymmetrical geometry |
| 01/04/2012 | EP2402565A1 Method and device for cooling steam turbine generating equipment |
| 01/04/2012 | EP2402559A1 Turbine blade with tip shroud |
| 01/04/2012 | EP2402558A1 Vanes for directing exhaust to a turbine wheel |
| 01/04/2012 | EP2402557A2 Turbine rotor assembly |
| 01/04/2012 | EP2402112A2 Method for Producing a Shrouded Impeller from Two or More Components |
| 01/04/2012 | EP2401477A2 Method for attaching or producing an annular shroud for a turbine rotor and turbine rotor |
| 01/04/2012 | EP2401476A2 Method and apparatus for pre-spinning rotor forgings |
| 01/04/2012 | CN202100282U Rear supercharging turboexpander of gas bearing |
| 01/04/2012 | CN1525048B Gas turbine engine turbine nozzle bifurcated impingement baffle |
| 01/04/2012 | CN102308062A Turbine wheel and shaft joining processes |
| 01/04/2012 | CN102308060A Diffuser/rectifier assembly for a turbine engine |
| 01/04/2012 | CN102307827A Process for producing sintered sialon ceramic |
| 01/04/2012 | CN102305164A Gravity engine |
| 01/04/2012 | CN102305152A Hybrid exhaust aircraft engine |
| 01/03/2012 | US8087897 Fluid rotor |
| 01/03/2012 | US8087893 Turbine blade with showerhead film cooling holes |
| 01/03/2012 | US8087892 Turbine blade with dual serpentine flow circuits |
| 01/03/2012 | US8087891 Turbine blade with tip region cooling |
| 01/03/2012 | US8087885 Stacked annular components for turbine engines |
| 01/03/2012 | US8087881 Damped stator assembly |
| 01/03/2012 | US8087879 Device for cooling the slots of a rotor disk in a turbomachine having two air feeds |
| 01/03/2012 | US8087874 Retention structures and exit guide vane assemblies |
| 01/03/2012 | US8087871 Turbomachine compressor wheel member |
| 01/03/2012 | CA2461519C Lighter turbomachine blade and process for manufacturing the same |
| 12/29/2011 | WO2011161385A1 Method for producing a metal reinforcement for a turbomachine blade |
| 12/29/2011 | WO2011161371A1 Bladed rotor disk made of composite material for a gas turbine engine with clamped blade root/disk connection |
| 12/29/2011 | WO2011161357A1 Core for the manufacture of a turbine blade having impact-cooled leading edge cavity |
| 12/29/2011 | WO2011161188A1 Gas turbine blade |
| 12/29/2011 | WO2011160930A1 Gas turbine blade |
| 12/29/2011 | WO2011135234A3 Interface element between a blade root and a blade root housing of a turbine disc, and turbine rotor comprising an interface element |
| 12/29/2011 | US20110318191 Thermally loaded, cooled component |
| 12/29/2011 | US20110318189 Crossflow fan and air conditioner provided with same |
| 12/29/2011 | US20110318188 Axial centrifugal compressor with scalable rake angle |
| 12/29/2011 | US20110318187 Sealing device |
| 12/29/2011 | US20110318186 Root-End of a Wind Turbine Blade |
| 12/29/2011 | US20110318185 Lightened Axial Compressor Rotor |
| 12/29/2011 | US20110318184 Rotor for an axial flow turbomachine |
| 12/29/2011 | US20110318182 Gas compressor and method for controlling flow rate thereof |
| 12/29/2011 | US20110318181 Apparatus for preventing ice accretion |
| 12/29/2011 | US20110318172 Tandem blade design |
| 12/29/2011 | DE102011002172A1 Turbinendeckband-Abdichtungsvorrichtung Turbine shroud sealing device |
| 12/29/2011 | DE102010025238A1 Rotor for fluid-flow machine i.e. gas turbine, has groove comprising common inside edge region that defines radial outer abutment surfaces during application of centrifugal force to shovel segments |
| 12/29/2011 | CA2802943A1 Method for producing a metal reinforcement for a turbomachine blade |
| 12/28/2011 | EP2400160A1 Lightened rotor of axial compressor |
| 12/28/2011 | EP2400116A2 Sealing device of a blade root |
| 12/28/2011 | EP2400115A1 Thermally Loaded, Cooled Component |
| 12/28/2011 | EP2400114A1 A method for predicting initial unbalance in a component |
| 12/28/2011 | EP2399883A2 Article having composite coating |
| 12/28/2011 | EP2399006A1 Method for the production of an integrally bladed rotor, and rotor |
| 12/28/2011 | EP2399005A1 Blade union of a turbo machine |
| 12/28/2011 | EP2399004A1 Rotor section for a rotor of a turbomachine, rotor blade for a turbomachine |
| 12/28/2011 | EP2398936A1 Anti-erosion coating system for gas turbine components |
| 12/28/2011 | EP2398931A2 A method and arrangement for vapour phase coating of an internal surface of at least one hollow article |
| 12/28/2011 | EP2294284B1 Annular flange for attaching a rotor or stator element |
| 12/28/2011 | CN202090960U 一种湿蒸汽余热发电汽轮机 One kind of wet steam turbine cogeneration |
| 12/28/2011 | CN1826431B 机械零件的修理和制造方法及修复机械零件的制造方法 Repair and manufacturing methods of mechanical parts and manufacturing methods to repair the mechanical parts |
| 12/28/2011 | CN1621661B 安装涡轮静止叶片的方法和具有径向加载销的涡轮结构 Installation method for a turbine stationary blades and turbine structure having radial loading pin |
| 12/28/2011 | CN102301095A 涡轮机叶片系统 Turbine blade system |
| 12/28/2011 | CN102296995A 用于向涡轮引导废气的叶片 Used to guide the exhaust gas turbine blades |
| 12/28/2011 | CN102296993A 密封装置 Sealing device |
| 12/28/2011 | CN102296991A 制造汽轮机叶片的方法 Methods of manufacturing turbine blades |
| 12/28/2011 | CN101777086B 多重热循环下涡轮叶片热障涂层危险区域的预测方法 Multiple thermal cycle turbine blades under thermal barrier coating prediction method for hazardous areas |
| 12/28/2011 | CN101198768B 汽轮机用转子及其制造方法 Turbine rotor and its manufacturing method |
| 12/27/2011 | US8083492 Welded low-pressure turbine shaft |
| 12/27/2011 | US8083491 Wind turbine blade |
| 12/27/2011 | US8083489 Hybrid structure fan blade |
| 12/27/2011 | US8083487 Rotary airfoils and method for fabricating same |
| 12/27/2011 | US8083486 Turbine blade with cooling flow modulation |
| 12/27/2011 | US8083485 Angled tripped airfoil peanut cavity |
| 12/27/2011 | US8083484 Turbine rotor blade tips that discourage cross-flow |
| 12/27/2011 | US8083475 Turbine bucket angel wing compression seal |
| 12/25/2011 | CA2744202A1 Root-end of a wind turbine blade |
| 12/23/2011 | CA2743817A1 Lightened axial compressor rotor |
| 12/22/2011 | WO2011160061A2 Vortex propeller |
| 12/22/2011 | WO2011159437A1 Method of servicing an airfoil assembly for use in a gas turbine engine |
| 12/22/2011 | WO2011157971A1 Aerodynamic coupling between two annular rows of stationary vanes in a turbine engine |
| 12/22/2011 | WO2011157962A1 Airflow-straightening structure for the nacelle of an aircraft engine |
| 12/22/2011 | WO2011157957A1 Angular stator sector for a turbomachine compressor, turbomachine stator and turbomachine comprising such a sector |
| 12/22/2011 | WO2011157956A1 Angular sector of the downstream guide vanes for a turbine engine compressor, turbine engine downstream guide vanes and turbine engine including such a sector |
| 12/22/2011 | WO2011157927A1 Compressor and turbomachine with optimized efficiency |