Patents
Patents for F01D 5 - Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members (32,915)
05/2014
05/14/2014CN103790641A 涡轮机叶片尖端罩 Turbine blade tip shroud
05/14/2014CN103790640A 防轮盘爆裂叶片 Anti-blade wheel burst
05/14/2014CN103790639A 一种叶轮机端区叶片前缘边条修型方法 One kind of turbine blade leading edge of the end zone type repair method
05/14/2014CN102031995B 多合金涡轮机转子段、焊接涡轮机转子及其制造方法 Multiple alloy turbine rotor section, welded turbine rotor and a method of manufacturing
05/14/2014CN101666244B 涡轮机械用涡轮机叶片和减少该叶片上涡流效果的方法 Turbomachinery with turbine blades and reduce the effect on the blade vortex method
05/13/2014US8721294 Airfoil with galvanically isolated metal coating
05/13/2014US8721293 Turbine wheel with an axial retention system for vanes
05/13/2014US8721291 Flow directing member for gas turbine engine
05/13/2014US8721290 Processes for producing components containing ceramic-based and metallic materials
05/13/2014US8721285 Turbine blade with incremental serpentine cooling channels beneath a thermal skin
05/13/2014US8721284 Hollow-cast casting with a closure device
05/13/2014US8721282 Active twist hollow beam system
05/13/2014US8721281 Cooled blade for a gas turbine
05/13/2014US8721271 Oil cooler
05/13/2014US8721265 Multiple staged compressor with last stage airfoil cooling
05/13/2014CA2697741C Combined acoustic absorber and heat exchanging outlet guide vanes
05/13/2014CA2599037C Process for the fabrication of crystal seeds simultaneous with the casting of single-crystal parts
05/13/2014CA2593193C Turbine engine rotor and turbine engine comprising such a rotor
05/08/2014WO2014070849A1 Bore cavity thermal conditioning system
05/08/2014WO2014070817A1 Blade outer air seal
05/08/2014WO2014070698A1 Turbine rotor assembly
05/08/2014WO2014070695A1 Damper for a turbine rotor assembly
05/08/2014WO2014070509A1 Process for producing a turbine rotor
05/08/2014WO2014070438A1 Belly band seal with underlapping ends
05/08/2014WO2014070437A1 Gas turbine including belly band seal anti-rotation device
05/08/2014WO2014070403A1 Local heat treatment and thermal management system for engine components
05/08/2014WO2014070356A1 Nickel-based superalloy and articles
05/08/2014WO2014070279A2 Endwall contouring
05/08/2014WO2014070051A1 A porous coating applied onto an aerial article
05/08/2014WO2014069216A1 Turbine blade
05/08/2014WO2014068222A1 Method for resurfacing at least one arm of an intermediate casing of a turbomachine
05/08/2014WO2014067869A1 An aerofoil and a method for construction thereof
05/08/2014WO2014067868A1 Methods of manufacturing blades of turbomachines by wire electric discharge machining, blades and turbomachines
05/08/2014WO2014021982A3 Turbomachinery component cooling scheme
05/08/2014US20140127033 Turbomachine wheel assembly having slotted flanges
05/08/2014US20140127032 Casting method, apparatus, and product
05/08/2014US20140127027 Turbine rotor for a thermal electric power station
05/08/2014US20140127025 Wind turbine rotor blade and method for installing a wind turbine rotor blade
05/08/2014US20140127021 Impeller for a centrifugal slurry pump
05/08/2014US20140127020 Integral cover bucket assembly
05/08/2014US20140127019 Uni-directional axial turbine blade assembly
05/08/2014US20140127016 Band-type fan structure
05/08/2014US20140127013 Gas turbine engine airfoil cooling circuit
05/08/2014US20140127005 Method for producing a component, component and turbomachine having a component
05/08/2014US20140124615 Preventing Rotation of a Fixed Ring of a Swashplate
05/08/2014US20140123677 Gas turbine engine airfoil profile
05/08/2014DE102013111874A1 Manufacturing method of component for gas turbine engine involves forming grooves, each with cross-sectional are in predetermined ranged with respect to area derived from product of width of opening and depth of re-entrant shaped groove
05/08/2014DE10001516B4 Zerstörungsfreies Verfahren zur Bestimmung der Schichtdicke einer metallischen Schutzschicht auf einem metallischen Grundmaterial A nondestructive method for determining the thickness of a metallic protective layer on a metal base material
05/07/2014EP2728172A1 Rotor blade mold assembly and method for forming rotor blade
05/07/2014EP2728121A2 Locking blade for a rotor
05/07/2014EP2728120A2 Integral cover bucket assembly
05/07/2014EP2728119A1 Microchannel cooled turbine component and method of forming a microchannel cooled turbine component
05/07/2014EP2728118A2 Components with asymmetric cooling channels and methods of manufacture
05/07/2014EP2728117A1 Turbine blade tip with tip shelf diffuser holes
05/07/2014EP2728116A1 An aerofoil and a method for construction thereof
05/07/2014EP2728115A1 Gas turbine engine end-wall component and corresponding method
05/07/2014EP2728114A1 A platform cooling device for a blade of a turbomachine and a blade for a turbomachine
05/07/2014EP2728034A1 Components with micro cooled coating layer and methods of manufacture
05/07/2014EP2728033A1 Components with micro cooled patterned coating layer and methods of manufacture
05/07/2014EP2727681A1 A manufacturing process of a lightened turbomachine blade
05/07/2014CN203584577U 一种压气机与涡轮的连接结构 Connection structure of a compressor and the turbine
05/07/2014CN203584472U 一种涡轮叶尖结构及涡轮叶片 A turbine and turbine blade tip structure
05/07/2014CN203584471U 一种异型气膜孔结构及涡轮叶片 One kind of film cooling holes shaped structure and the turbine blades
05/07/2014CN203584470U 一种叉排扰流柱端面结构及涡轮气冷叶片 One kind of staggered pin fin end structures and air-cooled turbine blades
05/07/2014CN203584469U 涡轮叶片叶冠以及航空发动机涡轮 Crown and aviation turbine vane turbo engine
05/07/2014CN203584468U 一种带有侵入式壁面温度测试的涡轮叶片结构 A turbine blade structure with invasive wall temperature test
05/07/2014CN203584467U 一种涡轮钻具的涡轮转子 A turbine rotor turbine drill
05/07/2014CN203584466U 一种汽轮机双胞胎叶片 Twin steam turbine blade
05/07/2014CN103781995A 用于确定作为用于轴流式涡轮机的旧叶片的替换件的替换叶片的轮廓的方法 Means for determining a replacement of old blade for an axial turbine blade profile of the replacement method of
05/07/2014CN103781942A 局部清洁方法及设备 Local cleaning method and apparatus
05/07/2014CN103781588A 为叶片前缘制作保护加强件的方法 Production methods to protect the reinforcing member for the blade leading edge
05/07/2014CN103775135A 燃气涡轮和用于这样的燃气涡轮的涡轮叶片 The turbine blades of a gas turbine and a gas turbine used in such
05/07/2014CN103775134A 不同程度粗糙的叶片及其制造方法 Varying degrees of coarse blade and its manufacturing method
05/07/2014CN103775133A 涡轮机械叶片加强件 Turbomachinery blade stiffeners
05/07/2014CN103774134A 具有隔热涂层的燃气轮机用高温部件 Gas turbine with a thermal barrier coating with high temperature components
05/07/2014CN103774048A 沉淀硬化型马氏体不锈钢和使用其的汽轮机长叶片 Precipitation hardening martensitic stainless steel and use their long turbine blades
05/07/2014CN102261266B 防止移动的涡轮机叶片 Prevent movement of the turbine blades
05/07/2014CN102084088B 带有螺旋前边缘的混合叶轮 Mixing impeller with the front edge of the spiral
05/07/2014CN101936191B 用于组装旋转机器的方法及设备 Method and apparatus for assembling a rotating machine
05/07/2014CN101892866B 用于转子叶片的低应力周向燕尾榫保持系统及方法 Low stress circumferential dovetail for the rotor blades keep the system and method
05/07/2014CN101749059B 废气涡轮增压器中的减振 Exhaust gas turbocharger damping
05/07/2014CN101694168B 带有持久位置保持系统的涡轮机 Turbines with a lasting position holding system
05/06/2014US8714931 Turbine bucket airfoil profile
05/06/2014US8714930 Airfoil shape for turbine bucket and turbine incorporating same
05/06/2014US8714929 Turbine assembly and method for securing a closure bucket
05/06/2014US8714927 Microcircuit skin core cut back to reduce microcircuit trailing edge stresses
05/06/2014US8714926 Turbine component cooling channel mesh with intersection chambers
05/06/2014US8714921 Fan shroud with modular vane sets
05/06/2014US8714909 Platform with cooling circuit
05/06/2014CA2719817C Gas turbine engine blade for aircraft and manufacturing method thereof
05/01/2014WO2014066566A1 Gas turbine engine rotor drain feature
05/01/2014WO2014066515A1 Vane assembly for an unducted thrust producing system
05/01/2014WO2014066503A1 Unducted thrust producing system
05/01/2014WO2014066501A1 Casting core for a cooling arrangement for a gas turbine component
05/01/2014WO2014066495A1 Cooling arrangement for a gas turbine component
05/01/2014WO2014066199A1 Reduction of equally spaced turbine nozzle vane excitation
05/01/2014WO2014066159A1 Gas turbine including belly band seal anti-rotation device
05/01/2014WO2014065968A1 Composite blade with uni-tape airfoil spars
05/01/2014WO2014064567A1 Method for building stages of centrifugal radial turbines
05/01/2014WO2014031203A3 Airfoil cover system
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