首页> 外国专利> STEAM TURBINE NOZZLE SEGMENT HAVING TRANSITIONAL INTERFACE, AND NOZZLE ASSEMBLY AND STEAM TURBINE INCLUDING SUCH NOZZLE SEGMENT

STEAM TURBINE NOZZLE SEGMENT HAVING TRANSITIONAL INTERFACE, AND NOZZLE ASSEMBLY AND STEAM TURBINE INCLUDING SUCH NOZZLE SEGMENT

机译:具有过渡界面的汽轮机喷嘴段,包括这种喷嘴段的喷嘴组件和汽轮机

摘要

Various embodiments include steam turbine static nozzles having transitional interfaces. In one embodiment a steam turbine static nozzle blade includes: an airfoil; an inner sidewall integral with a first side of the airfoil; and an outer sidewall integral with a second side of the airfoil; the inner sidewall and the outer sidewall each including: a first side having one of: an arcuate concave surface extending substantially an entire length of the sidewall, or an arcuate convex surface extending substantially the entire length of the sidewall; and a second side opposing the first side and having an angled interface extending substantially the entire length of the sidewall.
机译:各种实施例包括具有过渡界面的蒸汽涡轮静态喷嘴。在一个实施例中,蒸汽轮机静态喷嘴叶片包括:翼型;和与机翼的第一侧成一体的内侧壁;和与机翼的第二侧成一体的外侧壁;内侧壁和外侧壁均包括:第一侧面,其具有以下之一:基本上在侧壁的整个长度上延伸的弧形凹面,或基本上在侧壁的整个长度上延伸的弧形凸面;以及第二侧面与第一侧面相对并具有倾斜的界面,该倾斜的界面基本上在侧壁的整个长度上延伸。

著录项

  • 公开/公告号US2017030209A1

    专利类型

  • 公开/公告日2017-02-02

    原文格式PDF

  • 申请/专利权人 GENERAL ELECTRIC COMPANY;

    申请/专利号US201615290478

  • 发明设计人 STEVEN SEBASTIAN BURDGICK;

    申请日2016-10-11

  • 分类号F01D9/04;

  • 国家 US

  • 入库时间 2022-08-21 13:46:37

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