ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Scatter factor and values of metallic calendar life
Received date: 2015-09-30
Revised date: 2015-12-01
Online published: 2015-12-22
This paper studies the scatter factor of calendar life, and through research on the distribution regularities of the test data of metallic corrosion, a calculation model of scatter factor which is in consistence of the regularities is determined. Standard deviation is calculated through the corrosion test data. Scatter factor value used in corrosion test is calculated by the given standard deviation.
ZHANG Fuze . Scatter factor and values of metallic calendar life[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016 , 37(2) : 397 -403 . DOI: 10.7527/S1000-6893.2015.0327
[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).
/
| 〈 |
|
〉 |
CJA