The invention relates to a shrouded turbine guide vane. The vanes (1) comprise an outer casing (7) fixed to an inner platform (5) and an outer platform (4) and a cooling circuit consisting of an attached component (13). The attached component is fastened to the inner platform (5) by its base (12) and to the case (6) by a sleeve (14) passing through the outer platform (4). The casings (7) and the outer platform (7) may expand freely.
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申请公布号
EP0531202(A1)
申请公布日期
1993.03.10
申请号
EP19920402384
申请日期
1992.09.02
申请人
SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, "S.N.E.C.M.A."