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某水上飞机升降舵调整片操纵杆腐蚀裂纹分析
引用本文:刘祖铭,曹定国.某水上飞机升降舵调整片操纵杆腐蚀裂纹分析[J].腐蚀科学与防护技术,2004,16(5):331-333.
作者姓名:刘祖铭  曹定国
作者单位:1. 中国特种飞行器研究所,荆门,448035;中南大学,粉末冶金国家重点实验室,长沙,410083
2. 中国特种飞行器研究所,荆门,448035
基金项目:“九五”国防科技重点预研项目 ( 2 2 16 1)资助项目
摘    要:采用扫描电子显微镜(SEM)和金相显微镜对某水上飞机升降舵调整操纵杆裂纹进行了观察和分析,确认操纵杆裂纹是由腐蚀引起的,腐蚀产物的体积效应是操纵杆开裂的应力来源;并对腐蚀产物的体积效应进行了计算,求得LY12CZ铝合金操纵杆产生应力腐蚀开裂的临界腐蚀半径Rscc.对装配缝隙进行适当密封,可以避免操纵杆腐蚀和开裂.

关 键 词:应力腐蚀  体积效应  铝合金  
文章编号:1002-6495(2004)05-0331-03
修稿时间:2003年2月22日

ANALYSIS OF CORROSION INDUCED CRACKING FOR A CONTROL ROD OF ELEVATOR TAB FOR A WATER-PLANE
LIU Zu ming ,CAO Ding guo China Special Vehicle Research Institute,Jingmen , State Key Laboratory of Powder Metallurgy,Central South University,Changsha.ANALYSIS OF CORROSION INDUCED CRACKING FOR A CONTROL ROD OF ELEVATOR TAB FOR A WATER-PLANE[J].Corrosion Science and Protection Technology,2004,16(5):331-333.
Authors:LIU Zu ming    CAO Ding guo China Special Vehicle Research Institute  Jingmen  State Key Laboratory of Powder Metallurgy  Central South University  Changsha
Affiliation:LIU Zu ming 1,2,CAO Ding guo 1 1 China Special Vehicle Research Institute,Jingmen 448035, 2 State Key Laboratory of Powder Metallurgy,Central South University,Changsha 410083
Abstract:Cracks on a control rod of the elevator tab for a water plane were analyzed by scanning electron miroscopy(SEM) and metallurgical microscope.It is believed that cracks were induced by corrosion,and the volume effect of corrosion products was the stress source of cracking.The critical radius R scc for stress corrosion cracking to initiation on the LY12CZ rod was calculated.The corrosion and cracking of this rod can be avoided through sealing the relevant clearance properly by assembling.
Keywords:stress corrosion cracking  volume effect of corrosion products  LY12CZ Al  alloy  control rod of elevator tab  aircraft structure  
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