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    • 3. 发明申请
    • STEAM TURBINE SINGLET NOZZLE DESIGN FOR BREECH LOADED ASSEMBLY
    • 蒸汽涡轮喷嘴喷嘴设计用于BREECH装载组件
    • US20120148395A1
    • 2012-06-14
    • US12966476
    • 2010-12-13
    • Dominick Joseph WertherSteven Sebastian Burdgick
    • Dominick Joseph WertherSteven Sebastian Burdgick
    • F04D29/40B23P15/00
    • F01D9/042
    • A steam turbine nozzle airfoil with integral inner and outer sidewalls is engaged with an inner ring and an outer ring in a nozzle assembly. Previous designs required large clearances between radial surfaces to permit simultaneous circumferential loading of the inner and outer sidewall into the inner and outer rings. The inventive arrangement provides for breech loading of the inner sidewall into the inner ring which allows near line-to-line radial contact on the hooks between the rings and the integral sidewalls of the Singlet nozzle airfoil. Tighter radial clearance overcome problems with loose assembly such as movement during welding, gaps leading to stress risers and performance issues associated with nozzle throat control.
    • 具有整体内壁和外侧壁的汽轮机喷嘴翼型件与喷嘴组件中的内环和外环接合。 以前的设计需要径向表面之间的大间隙,以允许内侧壁和外侧壁同时周向地加载到内圈和外圈中。 本发明的装置提供了内侧壁进入内环的后膛加载,其允许在环之间的钩和单列喷嘴翼型的整体侧壁之间的近线对线的径向接触。 更紧密的径向间隙克服了松动组装的问题,例如焊接过程中的移动,导致应力梯度的间隙和与喷嘴喉部控制相关的性能问题。
    • 4. 发明申请
    • Turbine Singlet Nozzle Assembly with Mechanical and Weld Fabrication
    • 具有机械和焊接加工的涡轮单列喷嘴组件
    • US20100232934A1
    • 2010-09-16
    • US12402081
    • 2009-03-11
    • Steven Sebastian BurdgickAndrew Paul Greif
    • Steven Sebastian BurdgickAndrew Paul Greif
    • F01D17/12
    • F01D9/042F01D9/044
    • Embodiments of this invention include a nozzle assembly for a turbine, the nozzle assembly including an airfoil, inner and outer sidewalls, and inner and outer rings. Each of these sidewalls and rings are coupled together at an interface through a combination of a mechanical interconnection on one end and a welded connection on the other end. The mechanical interconnection includes either the sidewalls or the rings having a protruding hook and the other having a corresponding hook recess. The interconnection can also include axial and radial mechanical stops. The configuration may further include one or more surfaces at an interface between a ring and a sidewall angled away from the interface to form a narrow groove. The configuration further may include a ring with a consumable root portion.
    • 本发明的实施例包括用于涡轮机的喷嘴组件,喷嘴组件包括翼型件,内侧和外侧壁以及内外环。 这些侧壁和环中的每一个通过在一端上的机械互连和另一端的焊接连接的组合在界面处耦合在一起。 机械互连包括具有突出钩的侧壁或环,而另一个具有相应的钩凹部。 互连还可以包括轴向和径向机械止动件。 该构造可以进一步包括在环和与界面成角度的侧壁之间的界面处的一个或多个表面,以形成窄槽。 该构造还可以包括具有消耗根部的环。