摘要
对成败型航空发动机部件可靠性增长试验抽样数的确定问题进行了研究。推导出了初始故障数服从典型离散分布时的最小化最大准则（Max-Min准则）,提出了一种逐次抽样样本估计值反馈修正方法。最后给出了一个应用实例,验证了该方法的有效性。
How to decide the sample number of reliability growth tests for success-failure components of aero-engine was researched. The mathematical model was established with maximal success number of left products after experiments as object function. The initially minimized maximum rule to fix sample numbers of reliability growth tests was deduced. At last, an example was proposed to illustrate this method and it was indicated that the rule was robust and practical.
出处
《海军航空工程学院学报》
2010年第5期488-492,共5页
Journal of Naval Aeronautical and Astronautical University
关键词
成败型航空发动机部件
系统性缺陷
可靠性增长试验
样本估计值反馈循环修正
初始最小化最大准则
success-failure components of aero-engine
systemic defaults
reliability growth test
circular modification with sample estimate feedback
initially minimized maximum rule
