发明名称 КОНТУРЫ ОХЛАЖДЕНИЯ ЛОПАТКИ ГАЗОВОЙ ТУРБИНЫ
摘要 The blade has a central cooling circuit (A) with a central cavity (34) between a lower surface cavity (32) and an upper surface cavity (30). The circuit has air admission openings to supply respective upper and lower surfaces with cooling air. The circuit has respective passages allowing communication of upper radial ends of upper and central cavities, and upper radial ends of lower and central cavities.
申请公布号 RU2004122669(A) 申请公布日期 2006.01.20
申请号 RU20040122669 申请日期 2004.07.26
申请人 СНЕКМА МОТОРС (FR) 发明人 БОТРЕЛЬ Эрван (FR);ЭНО Патрис (FR)
分类号 F01D5/18;F01D5/20;F02C7/12;F02C7/18 主分类号 F01D5/18
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