发明授权
- 专利标题: Gas turbine rotating blade
- 专利标题(中): 燃气轮机旋转叶片
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申请号: US37111申请日: 1998-03-09
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公开(公告)号: US6019579A公开(公告)日: 2000-02-01
- 发明人: Hiroki Fukuno , Yasuoki Tomita , Kiyoshi Suenaga
- 申请人: Hiroki Fukuno , Yasuoki Tomita , Kiyoshi Suenaga
- 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: JPX9-054646 19970310
- 主分类号: F01D5/08
- IPC分类号: F01D5/08 ; F01D5/18 ; F02C3/30 ; F02C7/18
摘要:
A gas turbine rotating blade comprises a serpentine passage provided in the blade width direction in plural rows in a blade profile portion except the portion near the trailing edge having a small blade thickness, a steam cooling passage provided around the outer periphery of a platform, an air passage provided in the blade width direction in the vicinity of the trailing edge of blade profile portion, an impingement plate provided under the platform on the inside of the steam cooling passage, slot holes formed so as to branch off from the air passage and be directed to the trailing edge, and slits formed in the platform above the impingement plate. Therefore, the blade profile portion is cooled by the steam passing through the serpentine passage and the air passing through the air passage, so that the cooling construction is not complicated, and cooling is performed effectively. For the platform, the outer periphery thereof is cooled by steam and the inside thereof by air effectively.
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