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Internal ferrule of an intermediate casing, associated intermediate casing with lamellae forming shock absorbers

机译:中间套管的内部套圈,带有薄片形成减震器的相关中间套管

摘要

The invention relates to a rectifier assembly (30) of a turbomachine, comprising: - an internal ferrule (10) of a casing comprising, from an axis of rotation of the turbomachine, a radially external surface (11) comprising an alternation of slots (12) and cross members (13), the cross members (13) extending axially, - at least one straightening blade (4) comprising a blade root (41) arranged in a slot (12); - at least a strip (20) comprising a central part supported by the cross member and side parts (22, 23) extending from the central part and suspended in the slots (12) surrounding each cross member; - at least one fin (5) comprising a platform (51) disposed above each cross member (13); each cross member (13) comprises a notch forming a radial recess in the cross member (131) and formed in the middle of the cross member (13) taken in an axial direction, the notch supporting said strip (20), each strip (131 ) being able to be deformed by a blade root (41) so that the central part is deformed to fill a radial play between the cross member and the fin (5) disposed between each blade. Figure for the abstract: Fig. 2
机译:本发明涉及涡轮机的整流器组件(30),包括: - 壳体的​​内部套圈(10),包括从涡轮机的旋转轴线,径向外表面(11)包括槽(如图12所示,横向构件(13),轴向延伸的横向构件(13), - 至少一个矫直刀片(4),所述矫直刀片(4)包括布置在槽(12)中的刀片根(41); - 至少一种条带(20),包括由从中心部分延伸的横向构件和侧部(22,23)支撑的中心部分,并悬挂在每个横梁周围的槽(12)中; - 至少一个翅片(5),包括设置在每个横梁(13)上方的平台(51);每个横向构件(13)包括在横向构件(131)中形成径向凹槽的凹口,并且形成在沿轴向的横向构件(13)的中间,所述凹口支撑所述条带(20),每个条带( 131)能够被刀片根(41)变形,使得中心部分变形以填充设置在每个叶片之间的横向构件和翅片(5)之间的径向播放。摘要图:图2

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