发明名称 |
Rotor blade for a centripetal turbine |
摘要 |
<p>A trailing edge of a radial turbine rotor blade is formed so that a deflection angle of a blade surface in a downstream side of a maximum blade thickness portion is a predetermined value or less, by forming the trailing edge of the radial rotor blade so as to be inclined from a center line of a blade thickness toward an extension line of a suction surface. Since the trailing edge of the rotor blade is thus formed, a rapid increase of the deflection angle is prevented in a trailing edge portion of the rotor blade. Accordingly, a rapid ascent portion and a rapid deceleration portion are not generated in a suction surface velocity in a main stream unlike the conventional case. <IMAGE></p> |
申请公布号 |
EP1369553(A2) |
申请公布日期 |
2003.12.10 |
申请号 |
EP20030010273 |
申请日期 |
2003.05.07 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
HIGASHIMORI, HIROTAKA;OSAKO, KATSUYUKI;SHIRAISHI, TAKASHI;MIKOGAMI, TAKASHI |
分类号 |
F01D5/04;F01D5/14;F02B39/00;(IPC1-7):F01D5/04 |
主分类号 |
F01D5/04 |
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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