期刊文献+

环境对有/无防护涂层结构疲劳性能的影响 被引量:3

SOME EFFECTS ON FATIGUE PROPERTIES UNDERPROTECTION/UNPROTECTION COATING SYSTEMS
下载PDF
导出
摘要 以试验研究为基础,用两种型式的试验件试验来研究飞机结构防护涂层在典型气候和人工加速环境条件下的疲劳性能的影响,并采用结构细节疲劳额定值(DFR)方法给出在环境条件下有/无防护涂层试件的疲劳强度修正系数。由试验结果分析得到下述结论:经大气暴露的涂层试件比未经大气暴露试验的DFR值要下降11%~21%。双涂层试件比单涂层试件在相同暴露试验条件下DFR值要高。 The effects on the fatigue characterization under the typical atmosphere and accelerated simulation environments are studied based on the test of two kinds of specimens with protection coating systems for aircraft structures. Some modified coefficients for protection and unprotection coating systems under the environments are given by using structural detail fatigue rating (DFR)method. From the test results, the following conclusions can be drawn out: the DFR value of the coated specimen exposed to the weather, relative to a non exposed specimen, has dropped about 11% to 21%.Under the same condition, the DFR value of a double coating specimen is higher than that of a single coating one. All the research results here can be used as the basis to engineering structure in the area of corrosion protecting design.
出处 《航空学报》 EI CAS CSCD 北大核心 1998年第4期481-485,共5页 Acta Aeronautica et Astronautica Sinica
关键词 疲劳性能 涂层 环境防护 腐蚀 飞机 fatigue properties, coating systems, environment, protection, corrosion
  • 相关文献

参考文献3

  • 1刘一鸣,研究报告623S-9604-33,1996年
  • 2陈群志,研究报告623S-9504-06,1995年
  • 3团体著者,航空材料疲劳性能手册,1981年

同被引文献26

  • 1刘祖铭,曾凡阳,鲁礼菊,曹定国,吴有金,黄伯云.环境对LY12CZ铝合金典型螺接件疲劳性能的影响[J].中国腐蚀与防护学报,2004,24(5):267-271. 被引量:7
  • 2常红,韩恩厚,王俭秋,柯伟.飞机蒙皮涂层对LY12CZ铝合金腐蚀疲劳寿命的影响[J].中国腐蚀与防护学报,2006,26(1):34-36. 被引量:18
  • 3马雪峰,葛广平.循环序进应力加速寿命试验的模型与数据分析[J].应用概率统计,1997,13(1):11-18. 被引量:9
  • 4吴富民.结构疲劳强度[M].西安:西北工业大学出版社,1985.141-148.
  • 5SureshS 王中光 译.材料的疲劳[M].北京:国防工业出版社,1993..
  • 6Goranson U G, Miller M. Aging jet transport structural evaluation programs [ C]//A Berkovits. Aeronautical Fatigue in the Electronic Era. Warleu:Engineering Materials Advisory Services, 1998:319 353.
  • 7Segerfrojd G, Blom A F. Fatigue behavior of mechanical joints : A state - of- the - artoverview[ C] //Proceedings of the Seventh International Fatigue Congress. Vol. 1/4. Beijing, China, 1999 : 41 - 56.
  • 8Newman J C Jr, Harris C E, Piascik R S, et al. Methodology for predicting the onset of widespread fatigue damage in lapsplice joints and structure[C] //Proceedings of the Seventh International Fatigue Congress. Vol.1/4. Beijing, China, 1999:81 - 92.
  • 9Laird C, Smith G C. Crack propagation in high stress fatigue [J]. Philosophical Magazine, 1962, 8(8): 847- 857.
  • 10蒋祖国.飞机结构腐蚀疲劳[M].北京:航空工业出版社,1992.

引证文献3

二级引证文献29

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部