发明名称 蒸気タービンの静翼、蒸気タービン
摘要 The present invention comprises blade members (17, 18) within which a space (14) is formed, and a leaf spring member (19) disposed in the space (14) of the blade members (17, 18) and elastically contacting inner surfaces (21, 22) of the blade members (17, 18). The leaf spring member (19) includes a positioning portion (27), an elastic contact portion (28), and a coupling portion (29). The elastic contact portion (28) includes a plurality of divided portions disposed along a longitudinal direction of the blade members (17, 18). As a result, according to the invention, the elastic contact portion (28) can elastically contact the inner surfaces (21, 22) of the blade members (17, 18) across substantially the entire surfaces of the inner surfaces (21, 22) without partial contact. Thus, the area of elastic contact between the elastic contact portion (28) and the inner surfaces (21, 22) of the blade members (17, 18) is increased, enabling a reliable suppression of flattering in a stator blade.
申请公布号 JP5660883(B2) 申请公布日期 2015.01.28
申请号 JP20100285756 申请日期 2010.12.22
申请人 发明人
分类号 F01D9/02;F01D25/04 主分类号 F01D9/02
代理机构 代理人
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