[1] 陈跃良, 陈亮, 卞贵学,等. 先进舰载战斗机腐蚀防护控制与日历寿命设计[J]. 航空学报, 2021, 42(8):525786.CHEN Y L, CHEN L, BIAN G X, et al. Corro-sion protection control and calendar life design of advanced carrier-based aircraft[J]. Acta Aer-onautica et Astronautica Sinica 2021, 42(8): 525786 (in Chinese).[2] 陈跃良, 段成美, 吕国志. 军用飞机日历寿命预测技术研究现状及关键技术问题[J]. 中国工程科学, 2002, 4(4):69-74.CHEN Y L, DUAN C M, LV G Z. Current sta-tus and key technique of predictive technique for calendric life of military aircraft[J]. Engi-neering Science, 2002, 4(4):69-74(in Chinese).[3] 陈跃良, 卞贵学, 张勇, 等.飞机结构电偶腐蚀数值模拟[M]. 北京: 国防工业出版社, 2020: 2-3.CHEN Y L, BIAN G X, ZHANG Y, et al. Nu-merical simulation of galvanic corrosion in air-craft structures[M]. Beijing: National Defense Industry Press, 2020: 2-3 (in Chinese).[4] 陈跃良, 金平, 林典雄, 等. 海军飞机结构腐蚀控制及强度评估[M]. 北京: 国防工业出版社, 2009: 1-13.CHEN Y L, JIN P, LIN D X, et al. Corrosion control and strength evaluation of naval aircraft structure[M]. Beijing: National Defense Indus-try Press, 2009: 1-13(in Chinese).[5] 陈跃良, 张勇. 军用飞机结构日历寿命相关问题的思考[J]. 航空工程进展, 2010, 1(4): 311-316.CHEN Y L, ZHANG Y. Considerations on the calendar life of military aircraft structures[J]. Advances in Aeronautical Science and Engi-neering, 2010, 1(4): 311-316(in Chinese).[6] 刘文珽 李玉海. 飞机结构日历寿命体系评定技术[M]. 北京: 航空工业出版社, 2004.LIU W T, LI Y H. Evaluation technology of aircraft structure calendar life system[M]. Bei-jing: Aviation Industry Press, 2004 (in Chi-nese).[7] 李玉海, 刘文珽, 杨旭. 军用飞机结构日历寿命体系评定应用范例[M]. 北京: 航空工业出版社, 2005.LI Y H, LIU W T, YANG X. Application exam-ple of calendar life system evaluation of mili-tary aircraft structure[M]. Beijing: Aviation In-dustry Press, 2005 (in Chinese).[8] 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.ZHANG F Z. Principle and method of calculat-ing real corrosion tolerance value of aircraft structure[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(5): 524457 (in Chinese).[9] 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 metal-lic calendar life[J]. Acta Aeronautica et Astro-nautica Sinica, 2016, 37(2): 381-389 (in Chi-nese).[10] 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):390-396.ZHANG F Z. Calculation formula and test method of calendar life of metallic coating[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(2): 390-396 (in Chinese).[11] 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):397-403.ZHANG F Z. Scatter factor and values of me-tallic calendar life[J]. Acta Aeronautica et As-tronautica Sinica, 2016, 37(2):397-403 (in Chinese).[12] 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 Aero-nautica et Astronautica Sinica, 2000, 21(4):349-351 (in Chinese).[13] 赵海军, 郭泉, 金平. 加速预腐蚀与疲劳试验估算飞机结构日历寿命的新方法[J]. 腐蚀科学与防护技术, 2007, 19(3):229-232.ZHAO H J, GUO Q, JIN P. A new estimating method of calendar life for aircraft structures using an accelerated pre corrosion and fatigue test[J]. Corrosion Science and Protection Tech-nology, 2007, 19(3): 229-232 (in Chinese).[14] 张耀. 军用飞机疲劳损伤容限耐久性设计手册[M]. 北京: 中国航空研究院, 1994.ZHANG Y. Military aircraft fatigue damage tolerance durability design manual[M]. Beijing: China Aviation Research Institute, 1994.[15] Goranson U G. Elements of structural integrity assurance[J]. International Journal of Fatigue, 1994, 16(1):43-65.[16] 刘文珽, 黄季墀, 刘小冬, 等. 军用飞机结构疲劳设计细节疲劳额定值方法指南[M]. 北京: 国防工业出版社, 2012: 21-23.LIU W T, HUANG J C, LIU X D, et al. Mili-tary aircraft structural fatigue design detail fa-tigue rating methodological guide[M]. Beijing: National Defense Industry Press, 2012: 21-23 (in Chinese).[17] 董彦民, 刘文珽, 杨超. 军用飞机结构耐久性设计的细节疲劳额定值方法[J]. 航空学报, 2010: 2357-2364.DONG Y M, LIU W T, YANG C. Military air-craft durability design method based on detail fatigue rating[J]. Acta Aeronautica et Astro-nautica Sinica, 2010, 31(12): 2357-2364 (in Chinese).[18] 陈跃良, 吴省均, 卞贵学, 等. 基于Gerber模型的DFR腐蚀折算系数及其试验测定[J]. 材料导报, 2019, 33(16):2793-2798.CHEN Y L, WU X J, BIAN G X, et al. Theo-retical and experimental determination of DFR-corrosion-influence-factors based on Gerber model[J]. Materials Reports. 2019, 33(16): 2793-2798(in Chinese).[19] 张建宇, 鲍蕊, 陈勃,等. 腐蚀环境下疲劳分析的DFR方法研究[J]. 北京航空航天大学学报, 2004, 30(6):547-550.ZHANG J Y, BAO R, CHEN B, et al. Study on DFR method under corrosion environment for fatigue analysis[J]. Journal of Beijing Uni-versity of Aeronautics and Astronautics, 2004, 30(6):547-550 (in Chinese).[20] 蒋祖国, 田丁栓, 周占廷. 飞机结构载荷/环境谱[M]. 电子工业出版社, 2012.58-59.JIANG Z G, TIAN D S, ZHOU Z T. Aircraft structure load / environment spectrum[M]. Bei-jing: Publishing House of Electronics Industry, 2012: 58-59 (in Chinese).[21] 郑晓玲. 民用飞机金属结构耐久性与损伤容限设计[M]. 上海: 上海交通大学出版社, 2013: 103-105.ZHENG X L. Durability and damage tolerance design for metal structures of the civil air-craft[M]. Shanghai: Shanghai Jiao Tong Uni-versity Press, 2013: 103-105 (in Chinese).[22] 薛景川, 郭定文, 邵闯. DFR、DCR和DSR疲劳损伤分析体系综论[J]. 结构强度研究, 2006(1):1-7.XUE J C, GUO D W, SHAO C. The analysis system of DFR, DCR and DSR fatigue dam-age[J] Study of Structural Strength, 2006(1):1-7(in Chinese).[23] 王荣. 金属材料的腐蚀疲劳[M]. 西安:西北工业大学出版社, 2001: 57-60.WANG R. Corrosion fatigue of metal materi-als[M]. Xi`an: Northwest University of Tech-nology Press, 2001: 57-60(in Chinese).[24] 张建宇, 刘爱民, 费斌军. 腐蚀环境下的随机耐久性分析方法[J]. 北京航空航天大学学报, 2000, 26(5):556-560.ZHANG J Y, LIU A M, FEI B J. Stochastic crack growth approach under corrosion envi-ronment for durability analysis[J]. Journal of Beijing University of Aeronautics and Astro-nautics, 2000, 26(5):556-560(in Chinese).[25] 赵天亮. E690钢在模拟海水中的腐蚀疲劳裂纹萌生行为及机理研究[D]. 北京科技大学, 2018.ZHAO T L. Corrosion fatigue crack initiation behaviors and mechanisms of E690 steel in simulated seawater[D]. University of Science and Technology Beijing, 2018 (in Chinese).[26] 隋福成, 刘文珽. 飞机等幅疲劳试验载荷谱编制技术研究[J]. 机械强度, 2008, 30(2):266-269.SUI F C, LIU W T. Study on the technique of developing constant amplitude load spectrum for aircraft fatigue test[J]. Journal of Mechani-cal Strength. 2008, 30(2):266-269(in Chinese).[27] 刘文珽, 王智, 隋福成. 单机寿命监控技术指南[M]. 北京: 国防工业出版社, 2010:78-84.LIU W T, WANG Z, SUI F C. Technical guide for single aircraft life monitoring[M]. Beijing: National Defense Industry Press, 2010:78-84 (in Chinese).[28] 吴富民. 结构疲劳强度[M]. 西安,西北工业大学出版社, 1985: 26-27.Wu F M. Structural fatigue strength[M]. Xi`an: Northwestern Polytechnical University Press, 1985: 26-27 (in Chinese).[29] 陈群志, 房振乾. 飞机结构日历寿命及腐蚀防护研究应关注的问题[J]. 装备环境工程, 2012, 9(6):72-77.CHEN Q Z, FANG Z Q. Consideration on some calendar life and corrosion protection questions of aircraft structures[J]. Equipment Environment Engineering, 2012, 9(6):72-77(in Chinese).[30] 鲍蕊, 张建宇, 郑晓玲,等. DFR腐蚀影响系数及其试验测定[J]. 北京航空航天大学学报, 2006, 32(6):639-644.BAO R, ZHANG J Y, ZHENG X L, et al. The-oretical and experimental determination of DFR-corrosion-influence-factors[J]. Journal of Beijing University of Aeronautics and Astro-nautics, 2006, 32(6):639-644 (in Chinese). |