Secure tightening of a CMC fastener for the heat shield of re-entry vehicles

被引:46
|
作者
Boehrk, H. [1 ]
Beyermann, U. [1 ]
机构
[1] DLR, Inst Struct & Design, German Res Ctr, Deutsch Zentrum Luft & Raumfahrt, D-70569 Stuttgart, Germany
关键词
CMC; Ceramic; Fastener; Re-entry; Heat-shield;
D O I
10.1016/j.compstruct.2009.07.002
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The results of static and hot tests of ceramic matrix composite fasteners for heat shield attachment to a re-entry vehicle are presented. Herein, the effect of the high temperature cycle occurring during atmospheric re-entry on the reduction of the tightening torque of the CMC fasteners is investigated. From cold testing, it is found that the Young's modulus of the material decreases with first-time loading and, therefore, previous loading of the fasteners before their application is recommended. In hot testing of a fully integrated fastener connection, the material temperatures within the connection are experimentally simulated. It is shown that with previous straining, a significant improvement of the fastener is achieved. The loosening torque is no longer reduced by thermally induced stretching of the fastener. (C) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码:107 / 112
页数:6
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