发明授权
- 专利标题: Gas turbine blade
- 专利标题(中): 燃气轮机叶片
-
申请号: US34130申请日: 1998-03-03
-
公开(公告)号: US6039531A公开(公告)日: 2000-03-21
- 发明人: Kiyoshi Suenaga , Yasuoki Tomita , Hiroki Fukuno
- 申请人: Kiyoshi Suenaga , Yasuoki Tomita , Hiroki Fukuno
- 申请人地址: JPX Tokyo
- 专利权人: Mitsubishi Heavy Industries, Ltd.
- 当前专利权人: Mitsubishi Heavy Industries, Ltd.
- 当前专利权人地址: JPX Tokyo
- 优先权: JPX9-049031 19970304
- 主分类号: F01D5/18
- IPC分类号: F01D5/18 ; F01D5/20 ; F01D5/30 ; F01D11/08 ; F02C7/16 ; F02C7/18
摘要:
The present disclosure provides a gas turbine blade in which the tip end thereof is cooled effectively to decrease the metal temperature for the prevention of burning and the temperature gradient of blade metal is decreased to prevent the occurrence of cracking. In the gas turbine blade provided with a cooling passage therein, a protrusion is provided inwardly of the peripheral walls of the blade, which define the blade profile and the protrusion is positioned on the outer surface of blade tip end wall directly above a cooling passage within the blade.
公开/授权文献
- USD372100S Cervical collar 公开/授权日:1996-07-23
信息查询