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device for repairing an aircraft engine crankcase flange, aircraft engine module, aircraft engine and repair process for an aircraft engine crankcase flange

机译:飞机发动机曲轴箱法兰的修理装置,飞机发动机模块,飞机发动机以及飞机发动机曲轴箱法兰的修理方法

摘要

DEVICE FOR THE REPAIR OF AN AERONAUTICAL ENGINE CLEANING FLANGE, AERONAUTICAL ENGINE MODULE, AERONAUTICAL ENGINE AND AERONAUTICAL ENGINE CLEANING FLANGE REPAIR Device for repairing an aircraft engine crankcase flange (1) radially in relation to the axis of rotation of the motor and comprising a series of festoons (2), drilled with a hole (3), regularly arranged in the circumference of the doto flange, said device comprising at least one reinforcement flange (7) itself to be fixed in festoons are (2) of said crankcase flange (1) by means of through or blind holes (9), said reinforcement flange (7) presenting two orthogonal symmetry planes. It is characterized by the fact that said device on the other hand comprises a reconditioning flange (8) mounted, by means of a first part (12), on the reinforcement flange (7) with the aid of fixing means (10) positioned on one of the symmetry planes of said reinforcement flange.
机译:航空发动机清洁法兰的修理装置,航空发动机模块,航空发动机和航空发动机清洁法兰的修理装置相对于电动机的旋转轴线沿径向维修飞机发动机曲轴箱凸缘(1)的装置,包括一系列齿孔(2)上钻有一个孔(3),该齿孔规则地排列在doto法兰的圆周上,所述装置包括至少一个本身固定在花键中的加强法兰(7),该装置是所述曲轴箱法兰(1)(2)。借助通孔或盲孔(9),所述加强凸缘(7)具有两个正交的对称平面。其特征在于,所述装置另一方面包括修整凸缘(8),该修整凸缘(8)借助于第一部分(12)安装在加强凸缘(7)上,借助于定位在其上的固定装置(10)。所述加强凸缘的对称平面之一。

著录项

  • 公开/公告号BRPI1013243B1

    专利类型

  • 公开/公告日2020-07-07

    原文格式PDF

  • 申请/专利权人 SNECMA;

    申请/专利号BR2010PI13243

  • 申请日2010-03-03

  • 分类号F01D9/02;F01D25/24;

  • 国家 BR

  • 入库时间 2022-08-21 11:18:04

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