| 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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| 05/27/2014 | US8734114 Blade for a gas turbine engine comprising composite material having voids configured to act as crack initiation points when subject to deformation wave |
| 05/27/2014 | US8734112 Asymmetrical rotor blade slot attachment |
| 05/27/2014 | US8734111 Platform cooling passages and methods for creating platform cooling passages in turbine rotor blades |
| 05/27/2014 | US8734108 Turbine blade with impingement cooling cavities and platform cooling channels connected in series |
| 05/27/2014 | US8734107 Ceramic-based tip cap for a turbine bucket |
| 05/27/2014 | US8734101 Composite vane mounting |
| 05/27/2014 | US8734095 Gas turbine |
| 05/27/2014 | US8732948 Method of manufacturing impeller for centrifugal blower |
| 05/27/2014 | CA2728968C Hp turbine vane airfoil profile |
| 05/27/2014 | CA2598532C Turbomachine rotor blade |
| 05/22/2014 | WO2014078305A1 Process for forming a long gas turbine engine blade having a main wall with a thin portion near a tip |
| 05/22/2014 | WO2014078121A1 Contoured stator shrouds |
| 05/22/2014 | WO2014077909A2 Multi-lobed cooling holes in gas turbine engine components having thermal barrier coatings |
| 05/22/2014 | WO2014076829A1 Gas turbine member having thermal barrier coating |
| 05/22/2014 | WO2014076408A1 Monobloc preform and blade for turbo machine |
| 05/22/2014 | WO2014076407A1 Monobloc blade preform and module for a turbo machine intermediate casing |
| 05/22/2014 | WO2014075947A1 Modified surface around a hole |
| 05/22/2014 | WO2014075895A1 Turbine blade with cooling arrangement |
| 05/22/2014 | WO2014075894A1 Milling unit for drive-out device |
| 05/22/2014 | WO2014035516A3 Gas turbine engine turbine vane airfoil profile |
| 05/22/2014 | US20140141276 Method For Applying A Protective Layer, Component Coated With A Protective Layer, And Gas Turbine Comprising Such A Component |
| 05/22/2014 | US20140140860 Aerofoil cooling |
| 05/22/2014 | US20140140859 Uber-cooled multi-alloy integrally bladed rotor |
| 05/22/2014 | US20140140858 Compressor blade with nozzle |
| 05/22/2014 | US20140140857 Rotor assembly and method of using same |
| 05/22/2014 | US20140140852 Blade root, corresponding blade, rotor disc, and turbomachine assembly |
| 05/22/2014 | US20140140849 Gas turbine engine compressor rotor assembly and balancing system |
| 05/22/2014 | US20140140841 Turbine bucket shroud arrangement and method of controlling turbine bucket interaction with an adjacent turbine bucket |
| 05/22/2014 | US20140140833 Turbine shroud mounting and sealing arrangement |
| 05/22/2014 | DE102013112791A1 Turbinenschaufel-Mantelanordnung und Verfahren zur Steuerung der Turbinenschaufelwechselwirkung mit einer benachbarten Turbinenschaufel Turbine blade shroud assembly and method for controlling the turbine blade interaction with an adjacent turbine blade |
| 05/21/2014 | EP2733310A1 Modified surface around a hole |
| 05/21/2014 | EP2733309A1 Turbine blade with cooling arrangement |
| 05/21/2014 | EP2733308A2 Turbine engines with ceramic vanes and methods for manufacturing the same |
| 05/21/2014 | EP2733307A1 Milling unit for expulsion device |
| 05/21/2014 | EP2733233A2 Interlayer composite substrates |
| 05/21/2014 | EP2732136A1 Flow directing member for gas turbine engine |
| 05/21/2014 | EP2732057A1 Compressor blade and method for the production thereof |
| 05/21/2014 | CN103814193A 包括用于涡轮发动机的由cmc所制造的涡轮机喷嘴或压气机定子叶片以及耐磨支撑环的组件，以及包括这种组件的涡轮机或压气机 Includes a turbine compressor stator blades or nozzles are manufactured by the cmc and the wear of the support ring assembly for a turbine engine component comprising such a turbine or compressor |
| 05/21/2014 | CN103814192A 高弯度压缩机转子叶片 High camber compressor rotor blades |
| 05/21/2014 | CN103807022A 一种双向涡叶内冷负压航空氢动力发动机 Cold Air negative pressure within a two-way scroll hydrogen-powered engine leaves |
| 05/21/2014 | CN103807006A 排气涡轮增压器 An exhaust turbocharger |
| 05/21/2014 | CN103806955A 一种汽轮机的通流结构 Through-flow structure for a steam turbine |
| 05/21/2014 | CN103806954A 叶片组件及其组装方法 Vane assembly and method of assembling the |
| 05/21/2014 | CN103806953A 一种带倾角的新型气膜孔 A new film cooling holes with a dip |
| 05/21/2014 | CN103806952A 一种具有前缘凹腔的涡轮叶片 A turbine blade having a leading edge cavity |
| 05/21/2014 | CN103806951A 一种缝气膜冷却加扰流柱的组合式涡轮叶片 One kind of film cooling plus seam modular turbine blade spoiler column |
| 05/21/2014 | CN103806950A 一种具有叶尖压力面尾缘切除结构的涡轮叶片 Having a turbine blade tip trailing edge of the pressure surface removal structure |
| 05/21/2014 | CN103806949A 用于汽轮机叶片的超音速叶型 Turbine blades for supersonic airfoil |
| 05/21/2014 | CN103806948A 涡轮增压器和用于它的可变喷嘴筒体 Turbocharger and variable nozzle barrel for its |
| 05/21/2014 | CN103806947A 排汽面积5.0m<sup>2</sup>大负荷末级叶片 Exhaust area of 5.0m <sup> 2 </ sup> big load last stage blades |
| 05/21/2014 | CN103806946A 排汽面积2.1m<sup>2</sup>变转速工业汽轮机低压级组末级叶片 Exhaust area of 2.1m <sup> 2 </ sup> variable speed low-level group of industrial steam turbine last stage blades |
| 05/21/2014 | CN103805883A 一种火电汽轮机转子用钢 One kind of thermal power turbine rotor steel |
| 05/21/2014 | CN102465240B 沉淀硬化型马氏体不锈钢及使用有该不锈钢的汽轮机部件 Precipitation hardening martensitic stainless steel and the use of stainless steel turbine components |
| 05/20/2014 | US8727735 Rotor assembly and reversible turbine blade retainer therefor |
| 05/20/2014 | US8727734 Blade retainer clip |
| 05/20/2014 | US8727733 Gas turbine compressor last stage rotor blades with axial retention |
| 05/20/2014 | US8727730 Composite turbine bucket assembly |
| 05/20/2014 | US8727727 Components with cooling channels and methods of manufacture |
| 05/20/2014 | US8727725 Turbine vane with leading edge fillet region cooling |
| 05/20/2014 | US8727724 Turbine bucket having a radial cooling hole |
| 05/20/2014 | US8727723 Receptor for wind turbine blade lightning protection |
| 05/20/2014 | US8727718 Turbine rotor for a gas turbine |
| 05/20/2014 | US8727712 Abradable coating with safety fuse |
| 05/20/2014 | US8727710 Mateface cooling feather seal assembly |
| 05/20/2014 | US8727702 Hoop snap spacer |
| 05/20/2014 | US8727699 Rotating machinery with damping system |
| 05/20/2014 | US8726504 Method of producing turbine blade |
| 05/15/2014 | WO2014074396A1 External cooling fluid injection system in a gas turbine engine |
| 05/15/2014 | WO2014074368A1 Air injection system for cooling a rotor in a gas turbine engine and method of cooling such rotor |
| 05/15/2014 | WO2014074190A2 Endwall contouring |
| 05/15/2014 | WO2014072661A1 Method and device for manufacturing turbine blades |
| 05/15/2014 | WO2014072022A1 Adjustable diffuser for an exhaust gas pipe section of a turbine |
| 05/15/2014 | WO2014035517A3 Gas turbine engine turbine vane platform core |
| 05/15/2014 | WO2014031202A3 Assembled blade platform |
| 05/15/2014 | WO2014021981A3 Vortex generators for improved film effectiveness |
| 05/15/2014 | US20140134455 Interfacial diffusion barrier layer including iridium on a metallic substrate |
| 05/15/2014 | US20140134447 Pt-al-hf/zr coating and method |
| 05/15/2014 | US20140133996 Wear resistant slurry pump parts produced using hot isostatic pressing |
| 05/15/2014 | US20140133994 Gas turbine with pyrometer |
| 05/15/2014 | US20140133991 Gas turbine engine fan blade lock assembly |
| 05/15/2014 | US20140133990 Hub Piloting Diameter With Relief Cuts |
| 05/15/2014 | US20140133989 Turbine engine part forming a compressor stator or a turbine nozzle, and method for fabricating same |
| 05/15/2014 | US20140133987 Highly integrated leading edge of an aircraft lifting surface |
| 05/15/2014 | US20140133986 Turbine engine rotor, method of producing the same, method of joining ni-based superalloy member and steel member, and junction structure of ni-based superalloy member and steel member |
| 05/15/2014 | US20140133982 Propulsion device having unducted counter-rotating and coaxial rotors |
| 05/15/2014 | US20140133962 Interturbine vane with multiple air chambers |
| 05/15/2014 | DE102011084153B4 Sicherungsvorrichtung zur Sicherung eines Schaufelelements in einer Nut einer Laufscheibe Securing device for securing a blade member in a groove of a running disk |
| 05/15/2014 | DE102005025213B4 Schaufel einer Axialströmungsmaschine A blade axial flow |
| 05/14/2014 | EP2730746A1 Turbine nozzle having non-linear cooling conduit |
| 05/14/2014 | EP2730745A1 Blade assembly for a turbo engine |
| 05/14/2014 | EP2730744A1 Exhaust gas turbo charger |
| 05/14/2014 | EP2730743A2 Shaft of a gas turbine engine |
| 05/14/2014 | EP2730669A1 Nickel-based superalloys |
| 05/14/2014 | EP2730371A1 Device for setting a predetermined radial gap size of the blades of a turbomachine |
| 05/14/2014 | EP2730370A1 Method and device to adjust a predetermined radial tip clearance of a turbomachine blade |
| 05/14/2014 | EP2730364A1 Weld pool backing at the edge area |
| 05/14/2014 | CN203594670U 紧固垫片及燃气轮机转子紧固装置 Fastening pads and turbine rotor fastening device |
| 05/14/2014 | CN203594474U 一种带旋转叶轮的气动马达 A tape rotation of the impeller Qidongmada |
| 05/14/2014 | CN103797134A 压缩机叶片及其制造方法 Compressor blades and its manufacturing method |
| 05/14/2014 | CN103796818A 制造用于涡轮发动机的由复合材料所制造的涡轮机喷嘴或压气机定子叶片的扇体的方法，以及包括由所述扇体所组成喷嘴或定子叶片的涡轮机或压气机 The method of manufacturing a fan body nozzles or turbine stator blades of the compressor for a turbine engine fabricated from a composite material, and includes a nozzle or stator vanes of the fan by a body consisting of a turbine or compressor |