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REPAIR DEVICE FOR AERONAUTICAL MOTOR CASE FLANGE

机译:航空发动机外壳法兰的维修装置

摘要

Device for the repair of an aircraft engine casing flange (1) extending radially with respect to the axis of rotation of the engine and comprising a series of scallops (2) drilled with a hole (3) regularly disposed on the circumference of said flange, said device being intended to overcome the absence of at least one of said festoons and comprising at least one reinforcing flange (7) adapted to be fixed on healthy festoons (2) of said flange of casing (1) through through or blind holes (9) whose spacing reproduces the spacing of the holes (3) of the festoons of said casing flange, characterized in that said reinforcing flange (7) has two orthogonal symmetry planes, one being a radial plane and the second an axial plane passing through the axis of rotation of the engine, with reference to its positioning on the housing flange (1).
机译:用于修理飞机发动机壳体法兰(1)的装置,该装置相对于发动机的旋转轴径向延伸,并包括一系列扇贝(2),该扇贝钻有规则地设置在所述法兰的圆周上的孔(3),所述装置旨在克服至少一个所述胎记的缺乏,并且包括至少一个加强凸缘(7),所述加强凸缘适于通过通孔或盲孔(9)固定在所述壳体(1)的所述凸缘的健康胎记(2)上。 ),其间距再现了所述套管法兰的花键的孔(3)的间距,其特征在于,所述加强法兰(7)具有两个正交的对称平面,一个是径向平面,第二个是穿过轴线的轴向平面参照其在外壳法兰(1)上的定位确定发动机的旋转角度。

著录项

  • 公开/公告号FR2942854A1

    专利类型

  • 公开/公告日2010-09-10

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号FR20090051425

  • 申请日2009-03-06

  • 分类号F02C7/20;B64F5;

  • 国家 FR

  • 入库时间 2022-08-21 18:26:34

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