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    • 8. 发明专利
    • High temperature member for gas turbine
    • 用于气体涡轮机的高温部件
    • JP2006307842A
    • 2006-11-09
    • JP2006080264
    • 2006-03-23
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • UECHI HIDEYUKIKAWADA YUTAKAMATSUURA MASAAKISUENAGA KIYOSHISUGISHITA HIDEAKIYAMAMOTO HIROYUKIHANEDA SATORU
    • F01D5/18F01D9/02F02C7/18
    • PROBLEM TO BE SOLVED: To provide a high temperature member for gas turbine having a film cooling hole which can eliminate an unevenness of film cooling in such a way that a thickness of film of cooling medium, formed in a surface of the high temperature member for the gas turbine, can be processed in uniformity in the width direction.
      SOLUTION: A high temperature member 10 for the gas turbine, in which heat transfer from hot gas is suppressed by forming a film of the cooling medium in the surface with the cooling medium blown off from a plurality of film cooling hole 14, is characterized in that a flow-path in an outflow section 16 of the film cooling hole 14 is widened toward the end in the width direction along the surface 10a and the film of the cooling medium formed in the surface 10a is formed uniformly in the surface 10a.
      COPYRIGHT: (C)2007,JPO&INPIT
    • 要解决的问题:提供一种具有膜冷却孔的燃气轮机的高温部件,其能够消除膜冷却的不均匀性,使得形成在高的表面中的冷却介质的膜的厚度 用于燃气轮机的温度部件可以在宽度方向上均匀地加工。 解决方案:通过在从多个膜冷却孔14吹出的冷却介质的表面形成冷却介质的膜来抑制来自热气体的热传递的燃气轮机的高温部件10, 其特征在于,薄膜冷却孔14的流出部分16中的流动路径沿着表面10a向宽度方向的端部加宽,并且形成在表面10a中的冷却介质的膜在表面上均匀地形成 10A。 版权所有(C)2007,JPO&INPIT