[1] 张福泽. 飞机停放日历寿命腐蚀温度谱的编制方法和相应腐蚀介质的确定[J]. 航空学报, 2001, 22(4):359-362. 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):359-362(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] 张福泽. 金属机件腐蚀损伤日历寿命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).
[4] 张福泽, 叶序彬, 宋军. 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, YE X B, SONG J. 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).
[5] 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. Area determination method of aircraft calendar life[J]. Acta Aeronautica et Astronautica Sinica, 2001, 22(6):549-552(in Chinese).
[6] 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).
[7] 张福泽. 包含疲劳载荷的金属结构日历寿命确定方法:1069377[P]. 2012-10-31. ZHANG F Z. Include fatigue loading determine method of metal structure calendar life:1069377[P]. 2012-10-31(in Chinese).
[8] 宋均, 郭洪全. 三种航空材料的T-H曲线试验报告[R]. 北京:北京航空材料研究院, 2000. SONG J, GUO H Q. Test report of T-H curves for three kinds of aeronautical materials[R]. Beijing:Beijing Institute of Aeronautical Materials, 2000(in Chinese).
[9] 谢伟杰, 李荻, 胡艳玲, 等. LY12CZ和7075T7351铝合金在EXCO溶液中腐蚀动力学的统计研究[J]. 航空学报, 1999, 20(1):34-38. XIE W J, LI D, HU Y L, et al. Statistical study of corrosion kinetics law for LY12CZ and 7075T7351 aluminum alloy in EXCO solution[J]. Acta Aeronautica et Astronautica Sinica, 1999, 20(1):34-38(in Chinese).
[10] 高镇同. 飞机疲劳分散系数:BH-B884[R]. 北京:北京航空学院, 1982. GAO Z T. Fatigue scatter factors of aircraft:BH-B884[R]. Beijing:Beijing Institue of Aeronautics and Astronautics, 1982(in Chinese).
[11] 国防技术委员会. 军用飞机强度规范:第6分册:GJB67.6-85[S]. 北京:国防技术委员会, 1986. Defense Technology Commission. Military airplane structural strength specification:The 6th volume:GJB67.6-85[S]. Beijing:Defense Technology Commission, 1986(in Chinese). |