Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting: Structural aspects
Design of an all boron/epoxy doubler reinforcement for the F-111C wing pivot fitting: Structural aspects
复制标题
F-111C 机翼枢轴配件的全硼/环氧双倍加固设计：结构方面
DOI：
10.1016/0263-8223(89)90030-5
复制
发表时间：
1989
影响因子：
6.3
通讯作者：
Rhys Jones
中科院分区：
文献类型：
--
作者：
L. Molent;R. Callinan;Rhys Jones
本文概述了局部加强件的设计和研制的结构方面，这种局部加强件的设计和研制是为了降低F-111 C机翼枢轴接头易开裂区域的应力。对该设计的应力分析、典型试件测试、热分析和全尺寸静态测试等方面进行了总结。
This paper presents an overview of the structural aspects of the design and development of a local reinforcement designed to lower the stresses in a region of the F-111C wing pivot fitting which is prone to cracking. The stress analysis, representative specimen testing, thermal analysis and aspects of the full-scale static testing of this design are summarized.