%0 Journal Article
%T ANALYSIS OF CRACKING OF JOINT BOLT FOR WING AND FUSELAGE OF AN AIRCRAFT<br>飞机机翼与机身连接螺栓裂纹分析
%A XU Zhi-gang
%A ZHANG Dong
%A FU Guo-ru
%A <br>徐志刚
%A 张栋
%A 傅国如
%J 腐蚀科学与防护技术
%D 2005
%I 
%X The cracks at the joint bolt for the wing and fuselage of an aircraft were observed,when the aircraft was experienced a field maintenance,as a result of analyzing the relevant macroscopic and microscopic features of the fracture,measuring the change of chemical compositions around cracks,as well as combining the repairing process for bolts,the reason for the cracks generation was found out.
%K brittle fracture
%K stress corrosion
%K hydrogen brittle<br>脆性断裂
%K 应力腐蚀
%K 氢脆
%U http://www.alljournals.cn/get_abstract_url.aspx?pcid=5B3AB970F71A803DEACDC0559115BFCF0A068CD97DD29835&cid=AB188D3B70B071C57EB64E395D864ECE&jid=9F6E6EC8BA5BB62698F6640073DDD6E1&aid=376CFE641D90B62C&yid=2DD7160C83D0ACED&vid=BCA2697F357F2001&iid=E158A972A605785F&sid=11CEECA6DA9E4AC5&eid=EBD6B792C9111B87&journal_id=1002-6495&journal_name=腐蚀科学与防护技术&referenced_num=0&reference_num=2