首页> 外国专利> SUPPORTING STRUCTURE FOR COMBUSTOR TAIL CYLINDER OF GAS TURBINE

SUPPORTING STRUCTURE FOR COMBUSTOR TAIL CYLINDER OF GAS TURBINE

机译:燃气轮机燃烧尾筒的支撑结构

摘要

PURPOSE:To facilitate the cooling of a tail cylinder by forming the shape of a base member jointed into a combustor tail cylinder so that the side in the direction perpendicular to the shaft of the combustor tail cylinder long and the other side short. CONSTITUTION:A base member 13 is installed onto a combustor tail cylinder 3, and fixed onto a turbine casing through a bracket 14. As for the shape of the base member 13, the side (a) in the direction perpendicular to the shaft of the tail cylinder is made long, and the other side (b) is made short. Since the side (a) applied with a large load is made long, the area occupied by the base member 13 can be reduced. Therefore, the cooling of the tail cylinder 3 is facilitated.
机译:目的:通过形成连接到燃烧器尾筒中的底座部件的形状,使垂直于燃烧器尾筒轴的一侧较长而另一侧较短,从而方便冷却尾筒。组成:基础构件13安装在燃烧器尾缸3上,并通过托架14固定在涡轮机壳体上。基础构件13的形状(a)沿垂直于发动机轴的方向(a)尾筒变长,另一侧(b)变短。由于施加了较大负载的侧面(a)变长,所以可以减小基体13所占据的面积。因此,便于尾缸3的冷却。

著录项

  • 公开/公告号JPS6316136A

    专利类型

  • 公开/公告日1988-01-23

    原文格式PDF

  • 申请/专利权人 HITACHI LTD;

    申请/专利号JP19860157844

  • 发明设计人 IIZUKA NOBUYUKI;KUMADA KAZUHIKO;

    申请日1986-07-07

  • 分类号F02C7/20;

  • 国家 JP

  • 入库时间 2022-08-22 07:07:08

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