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
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页码:107 / 112
页数:6
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