航空学报 > 2000, Vol. 21 Issue (3): 196-201

飞机结构件在当量环境谱下加速腐蚀试验和日历寿命估算方法

张栋   

  1. 空军第一研究所 北京 100076
  • 收稿日期:1999-03-03 修回日期:1999-10-10 出版日期:2000-06-25 发布日期:2000-06-25

ACCELERATED CORROSION TEST OF THE AIRCRAFT STRUCTURE UNDER EQUIVALENT ENVIRONMENT SPECTRUM AND THE COMPUTING METHOD FOR THE CALENDAR LIFE

ZHANG Dong   

  1. The First Research Institute Airforce,Beijing 100076, China
  • Received:1999-03-03 Revised:1999-10-10 Online:2000-06-25 Published:2000-06-25

摘要: 首次成功地进行了构件在当量环境谱下的加速腐蚀试验,取得了防护层日历有效期和基体腐蚀扩展速率;建立了一套由试验数据估算日历首翻期、日历翻修间隔、日历总寿命的方法和公式;提出了由使用中真实的腐蚀损伤数据来估算日历首翻期的方法;在构件加速腐蚀试验和使用中真实腐蚀损伤数据统计处理的基础上,给出了 HX型机群日历寿命。

关键词: 飞机结构, 加速试验, 日历寿命, 估算方法

Abstract: It has been first successfully completed on the accelerated corrosion test of the aircraft structure under equivalent environment spectrum,and the calendar effective time of protection coating systems ( yo) and corrosion propagation rate( v ) of the body are obtained. A set of method and formula for the computation of calendar first D check, calendar time since overhaul and total calendar life is presented by using tests data. It is obtained that the calendar first D check y1=yo +yc , calendar time since overhaul yN =y1-(yoyO ), and the total calendar life YT =yo (1+R+…+RN)+(N+1)YC+NYS.Using aircraft service corrosion damage date, the computed method of calendar first D check is found. Based on components accelerated corrosion test and statistical data of service corrosion damage, the calendar life for the aircraft of HX type is given out.

Key words: aircraft st ructures, accelerated test, calendar life, comput ing method

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