发明名称 |
BLADE OF A GAS TURBINE |
摘要 |
The blade has such a shape that the diameters of circles inscribing the belly and back sides at different positions of adjacent blades decreases as one goes from the front edge to the rear edge. Since the blade has such a shape, even if the influent angle and effluent angle of gases are increased, a deceleration passage is not formed in the passage between the adjacent moving blades.
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申请公布号 |
CA2366969(A1) |
申请公布日期 |
2002.07.12 |
申请号 |
CA20022366969 |
申请日期 |
2002.01.09 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
UEMATSU, KAZUO;ITO, EISAKU |
分类号 |
F01D5/14;F01D5/18;(IPC1-7):F01D5/14 |
主分类号 |
F01D5/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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