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运输机突风飞-续-飞试验载荷谱研究 被引量:3
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作者 王想生 胡玫瑰 《飞机设计》 2013年第1期40-45,共6页
目前,采用等幅谱或程序块谱已经不足以表征载荷的相互影响,随着数据处理方法与试验能力的发展,疲劳试验大多采用变幅载荷。本文介绍了突风飞-续-飞试验载荷谱,疲劳试验载荷谱的编制原则是:既要尽可能做到载荷真实,又要与计划的研制进度... 目前,采用等幅谱或程序块谱已经不足以表征载荷的相互影响,随着数据处理方法与试验能力的发展,疲劳试验大多采用变幅载荷。本文介绍了突风飞-续-飞试验载荷谱,疲劳试验载荷谱的编制原则是:既要尽可能做到载荷真实,又要与计划的研制进度和试验设备能力限制相协调。这种谱不依赖于损伤模型假设,通过统计分析确定载荷的频率和幅值。 展开更多
关键词 等幅谱 程序块谱 飞-续-飞谱 真实性 统计分析
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Influence of Low Load Truncation Level on Crack Growth for Al 2324-T39 and Al 7050-T7451 被引量:9
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作者 Tian Hailing Bao Rui +2 位作者 Zhang Jianyu Zheng Xiaoling Fei Binjun 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2009年第4期401-406,共6页
Tests with middle-crack tension (M(T)) specimens made of Al 2324-T39 and Al 7050-T7451 are conducted to investigate the influence of low load truncation level on fatigue crack growth. The six different truncated s... Tests with middle-crack tension (M(T)) specimens made of Al 2324-T39 and Al 7050-T7451 are conducted to investigate the influence of low load truncation level on fatigue crack growth. The six different truncated spectra are obtained by removing the small cycles of which amplitudes are less than the specified percentages of the maximum amplitude in the basic flight-by-flight loading spectrum and the remainder of the spectrum is untouched. The tests indicate that the mean level of fatigue crack growth life (FCGL) increases as the load truncation level is enhanced. Considering both the time saving and the influence on FCGL, there is an applicable choice (i.e. spectrum S2 or spectrum S3 in this investigation) for full scale fatigue test. The scatter of FCGL becomes much larger than that under the basic spectrum when the load truncation level is increased to a specified high level, mainly due to the occurrence of crack slanting and branching under the high level truncated loading spectra. 展开更多
关键词 fatigue crack growth aluminum alloys low load truncation flight-by-flight spectrum
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