求飞机结构真实腐蚀容限的原理和方法

doi:10.7527/S1000-6893.2020.24457

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求飞机结构真实腐蚀容限的原理和方法

张福泽

北京航空工程技术研究中心, 北京 100076

收稿日期:2020-06-24 修回日期:2020-08-03 出版日期:2021-05-15 发布日期:2020-08-21
通讯作者: 张福泽 E-mail:zhangfuzemail@163.com

Principle and method of calculating real corrosion tolerance value of aircraft struture

ZHANG Fuze

Beijing Aeronautical Technology Research Center, Beijing 100076, China

Received:2020-06-24 Revised:2020-08-03 Online:2021-05-15 Published:2020-08-21

摘要/Abstract

摘要： 本文通过静强度、疲劳强度和腐蚀3个学科的综合研究，分别给出飞机结构（下称机件）在静载荷作用下的应力与腐蚀损伤D的分布曲线和机件在疲劳载荷作用下的寿命与腐蚀损伤D的分布曲线。根据这两条曲线和机件使用的容限应力值及总疲劳寿命值，便可分别求出机件在静载荷作用下的腐蚀损伤容限值和机件在疲劳载荷作用下的腐蚀损伤容限值以及同一机件同时受静载荷和疲劳载荷作用的腐蚀损伤容限值。此外，本文提出了用一个腐蚀损伤容限值保证同一机件的总疲劳寿命和总日历寿命皆安全的方法，以及总疲劳寿命和总日历寿命的匹配设计和匹配使用等问题。研究结论适用于大气、海洋、土壤等环境的腐蚀机件，解决了国际机械和腐蚀领域一直未解决的一些难题。

关键词: 腐蚀损伤容限, 日历寿命, 疲劳寿命, 静载荷, 疲劳载荷

Abstract: Through the comprehensive study of static strength, fatigue strength and corrosion, the distribution curve of stress and corrosion damage D of aircraft structure (subscript parts) under static load and the distribution curve of life and corrosion damage D of parts under fatigue load are studied respectively in this paper. According to these two curves and the tolerance, stress value and total fatigue life value of the parts, the tolerance values of the corrosion damage of the parts under static load, the tolerance values of the corrosion damage of the parts under fatigue load and the tolerance values of the corrosion damage of the same parts under static load and fatigue load can be calculated respectively. In addition, the method of using a corrosion damage tolerance value to ensure the safety of the total fatigue life and the total calendar life of the same part, and the matching design and matching use of the total fatigue life and the total calendar life are also studied. These conclusions are applicable to the corrosive parts in atmosphere, ocean, soil and other environments, and solve some unsolved problems in the field of international machinery and corrosion.

Key words: corrosion damage tolerance, calendar life, fatigue life, static load, fatigue load

中图分类号:

V215.5

张福泽. 求飞机结构真实腐蚀容限的原理和方法[J]. 航空学报, 2021, 42(5): 524457-524457.

ZHANG Fuze. Principle and method of calculating real corrosion tolerance value of aircraft struture[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(5): 524457-524457.

参考文献 26

[1]	张福泽. 金属机件腐蚀损伤日历寿命的计算模型和确定方法[J]. 航空学报, 1999, 20(1):75-79. ZHANG F Z. Calculation model and determination method of corrosion damage calendar life of metal parts[J].Acta Aeronautica et Astronautica Sinica,1999,20(1):75-79(in Chinese).
[2]	张福泽. 求任意腐蚀损伤的T-H曲线[J]. 航空学报, 2000, 21(4):349-351. ZHANG F Z. Method for deducing T-H curve of arbitrary corrosion damage[J]. Acta Aeronautica et Astronautica Sinica, 2000, 21(4):349-351(in Chinese).
[3]	宋钧,郭洪全. 三种航空材料腐蚀T-H曲线测试报告[R]. 北京:北京航空材料研究院, 2000. SONG Y, GUO H J. Test report of corrosion T-H curve of three kinds of aviation materials[R]. Beijing:Beijing Institute of Aeronautical Materials, 2000(in Chinese).
[4]	陈勃. LY12CZ和30CrMnSiA航空材料D-d曲线、T-H曲线和RH-H曲线的试验报告[R].北京:北京航空材料研究院,2011. CHEN B.Test report on D-D curve, T-H curve and RH-h curve of LY12CZ and 30CrMnSiA aviation materials[R]. Beijing:Beijing Institute of Aeronautical Materials, 2011(in Chinese).
[5]	张福泽. 金属腐蚀"3等线"和试验日历寿命确定方法[J].航空学报,2016,37(2):371-380. ZHANG F Z. Metallic corrosion"3 equal-line"and formula of test calendar life and its determination method[J].Acta Aeronautica et Astronautica Sinica,2016,37(2):371-380(in Chinese).
[6]	张福泽.金属涂层的日历寿命计算公式和试验方法[J].航空学报,2016,37(2):390-392. ZHANG F Z. Calculation formula and test method of calendar life of metallic coating[J].Acta Aeronautica et Astronautica Sinica,2016,37(2):390-392(in Chinese).
[7]	陈勃. LY2CZ和30 CrMnSiA航空材料涂层失效的T-H曲线测试报告[R]. 北京:北京航空材料研究院,2006. CHEN B. T-H curve test report of coating failure of ly2cz and 30 crmnsia aviation materials[R]. Beijing:Beijing Institute of Aeronautical Materials, 2006(in Chinese).
[8]	蒋祖国. 飞机结构腐蚀疲劳[M].北京:航空工业出版社,1992:20-90. JIANG Z G. Corrosion fatigue of aircraft structure[M]. Beijing:Aviation Industry Press, 1992:20-90(in Chinese).
[9]	TALBOT D, TALBOT J. Corrosion science and technology[M]. Boca Raton:CRC Press, 1998.
[10]	SZKLARSKA-SMIALOWSKA Z.[J]Corrosion Science,1999.
[11]	SMITH C J E. Corrosion and stress corrosion of aluminum-lithun alloy[R].Neuilly sur Seine:AGARD(NATO),1988.
[12]	HEUSLER K E. Fundametal aspects of the corrosion of alloys[J]. Corrision Science, 1997,39(7):1177-1191.
[13]	张福泽. 飞机日历翻修期与总日历寿命确定方法和预计公式[J].航空学报,2005,26(4):458-460. ZHANG F Z. Predicting method and formula for determining calendar repaired period and total calendar life of aircraft[J].Acta Aeronautica et Astronautica Sinica,2005,26(4):458-460(in Chinese).
[14]	张福泽. 金属材料日历寿命确定的分散系数和取值[J].航空学报,2016,37(2):307-403. ZHANG F Z. Scatter factor and values of metallic calendar life[J].Acta Aeronautica et Astronautica Sinica,2016,37(2):307-403(in Chinese).
[15]	高镇同. 飞机结构疲劳分散系数:BH-B884[R].北京:北京航空学院,1982. GAO Z T. Fatigue dispersion coefficient of aircraft structure:BH-B884[R]. Beijing:Beijing Institute of Aeronautics, 1982.
[16]	张福泽. 三维等损伤环境谱的编制原理和方法[J].航空学报,2016,37(2):381-389. ZHANG F Z. Drawing up principle and method of 3D damage environment spectrum of metallic calendar life[J]. Acta Aeronautica et Astronautica Sinica,2016, 37(2):381-389(in Chinese).
[17]	张福泽. 飞机停放日历寿命腐蚀温度谱编制方法和相应腐蚀介质的确定[J].航空学报,2001,22(4):359-361. ZHANG F Z. Method for drawing up corrosion temperature spectrum of aircraft calendar life and determination of respective corrosion medium[J].Acta Aeronautica et Astronautica Sinica,2001,22(4):359-361(in Chinese).
[18]	张福泽.张福泽文集[C]//北京:航空工业出版社,2017:178-182,260. ZHANG F Z.Zhang fuze[C]//Beijing:Aviation Industry Press, 2017:178-182,260(in Chinese).
[19]	张福泽.飞机日历寿命试验的介质成分确定和加速方法[J].航空学报,2008,29(4):873-879. ZHANG F Z. Corrosion medium composition and accelerated corrosion method of aircraft calendar life test[J].Acta Aeronautica et Astronautica Sinica,2008, 29(4):873-879(in Chinese).
[20]	周希沅. 飞机结构的当量环境谱与加速试验谱[J].航空学报,1996,17(5):613-616. ZHOU X H. equity environmental spectrum and speed test spectrum for aircraft structure[J].Acta Aeronautica et Astronautica Sinica,1996,17(5):613-616(in Chinese).
[21]	陈群志,崔长京. 海南地区温度、湿度统计报告[R].北京:北京航空工程技术中心,2010. CHEN Q Z, CUI C J. Statistical report of temperature and humidity in Hainan[R]. Beijing:Beijing Aviation Engineering Technology Center, 2010(in Chinese).
[22]	陈群志,崔长京. 重庆地区温度、湿度统计报告[R].北京:北京航空工程技术中心, 2010. CHEN Q Z, CUI C J. Statistical report of temperature and humidity in Chongqing[R]. Beijing:Beijing Aviation Engineering Technology Center, 2010(in Chinese).
[23]	张福泽.飞机日历寿命确定的"区域定寿法"[J].航空学报,2001,22(6):549-552. ZHANG F Z.Method of area determination of an aircraft calendar life[J].Acta Aeronautica et Astronautica Sinica,2001,22(6):549-552(in Chinese).
[24]	张福泽.金属日历寿命的新理论和试验的新方法对比验证研究[J].前沿科学,2015,35(9):4-10. ZHANG F Z.Comparative verification research on the theoretic and test method of metallic calendar life[J].Frontier Science, 2015, 35(9):4-10(in Chinese).
[25]	飞机结构腐蚀损伤容限研究-基础部分[R].青岛:航空工程学院青岛学院,2006. Research on corrosion damage tolerance of aircraft structure-basic part[R].Qingdao:Qingdao College of Aeronautical Engineering,2006(in Chinese).
[26]	张福泽.金属任意腐蚀损伤量的日历寿命计算模型和曲线[J].航空学报,2017,38(9):221110. ZHANG F Z.Model and curve of calendar life calculation for metal arbitrary corrosion damage value[J].Acta Aeronautica et Astronautica Sinica,2017,38(9):221110(in Chinese).

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求飞机结构真实腐蚀容限的原理和方法

Principle and method of calculating real corrosion tolerance value of aircraft struture

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