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SET FOR A TURBOMACHINE

机译:设置为涡轮机

摘要

The invention relates to an assembly for a turbomachine, comprising - a combustion chamber (1) comprising at its downstream end a downstream flange (6) extending radially, - a distributor (2) disposed downstream of the combustion chamber ( 1) and comprising a platform (11, 12) from which extends at least one blade (13) radially, the platform (11, 12) comprising an upstream flange extending radially and delimiting, with the downstream flange ( 6) arranged opposite, a space (15) opening into the combustion chamber (1) at its radially internal end and closed at its radially external end, by sealing means (17, 18) fixed to the distributor (2) , characterized in that the downstream flange (6) of the combustion chamber (1) comprises at least one cooling orifice (27a, 27b, 27c, 27d) straight and passing through said flange (6) opening into space ( 15), opposite the platform (11, 12) of the distributor (2).
机译:本发明涉及一种用于涡轮机的组件,包括:-燃烧室(1),在其下游端包括径向延伸的下游凸缘(6);-分配器(2),其布置在燃烧室(1)的下游并且包括:平台(11、12)从其径向延伸出至少一个叶片(13),该平台(11、12)包括上游凸缘,该上游凸缘径向地延伸,并且与下游凸缘(6)相对地界定出空间(15)开口通过固定在分配器(2)上的密封装置(17、18)在其径向内端处进入燃烧室(1)并在其径向外端处封闭,其特征在于,燃烧室的下游凸缘(6)(图1)包括至少一个冷却孔(27a,27b,27c,27d),所述冷却孔笔直并穿过所述凸缘(6),开口进入与分配器(2)的平台(11、12)相对的空间(15)。

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