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飞机服役环境当量加速腐蚀折算方法研究
引用本文:穆志韬,柳文林,于战樵.飞机服役环境当量加速腐蚀折算方法研究[J].海军航空工程学院学报,2007,22(3):301-304.
作者姓名:穆志韬  柳文林  于战樵
作者单位:1. 海军航空工程学院,青岛分院,山东,青岛,266041
2. 海军航空工程学院,飞行器工程系,山东,烟台,264001;海军航空工程学院,研究生管理大队,山东,烟台,264001
3. 海军航空工程学院,研究生管理大队,山东,烟台,264001
摘    要:文中依据飞机服役机场地面环境谱与腐蚀损伤等当量原则,建立了环境加速腐蚀当量折算关系,给出了飞机结构主要高强度铝合金材料的当量折算系数α及HR-α、T-α曲线。依据建立的当量折算关系编制的加速环境谱,对飞机铝合金构件进行加速腐蚀试验研究,得到了温度(T)、相对湿度(RH)对环境当量折算系数的影响规律,为飞机结构防腐控制及日历寿命研究提供了工程技术依据。

关 键 词:飞机结构  环境谱  加速腐蚀折算  当量关系
文章编号:1673-1522(2007)03-0301-04
修稿时间:2006年12月30

Research on Accelerated Corrosion Equivalent Conversion Method of Aircraft Service Environment
MU Zhi-tao,LIU Wen-lin and YU Zhan-qiao.Research on Accelerated Corrosion Equivalent Conversion Method of Aircraft Service Environment[J].Journal of Naval Aeronautical Engineering Institute,2007,22(3):301-304.
Authors:MU Zhi-tao  LIU Wen-lin and YU Zhan-qiao
Abstract:According to the airport ground environmental spectrum and the equivalent quantization rule of corrosion damage, it has been established that the equivalent conversion relation between the accelerated corrosion environment and the airport service environment and it has been obtained the equivalent coefficient (?) of high strength aluminum alloy material used in aircraft principle structural parts and HR??, T??curves. Based on the accelerated spectrum obtained from equivalent analysis, the accelerated corrosion test for high strength aluminum alloy has been done, and then the affected law that temperature (T), relative humidity (RH) to environmental equivalent conversion coefficient is obtained, which offers an effective technical approach for evaluating the calendar life of an aircraft and some engineering advice for corrosion prevention control of aircraft structures.
Keywords:aircraft structure  environmental spectrum  accelerated corrosion  equivalent relation
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