发明名称 Turbine blade comprising a cooling circuit
摘要 The blade (10a) has a center section (C) geometrically divided into four adjacent concave zones and four adjacent convex zones arranged on both sides of a skeleton line (S) of the blade. The central section has a concave cooling circuit with a set of radial cavities (24a, 26a, 28a) occupying three adjacent concave zones and a convex cooling circuit with another set of radial cavities (30a, 32a, 34a) occupying the convex zones and the remaining concave zones.
申请公布号 EP1790819(A1) 申请公布日期 2007.05.30
申请号 EP20060124041 申请日期 2006.11.14
申请人 SNECMA 发明人 DESCHAMPS, PASCAL;ENEAU, PATRICE;POTIER, THOMAS
分类号 F01D5/18 主分类号 F01D5/18
代理机构 代理人
主权项
地址