论文部分内容阅读
对SAE AIR 5120中有关发动机监视系统可靠性的定义、设计思想、人为因素、试验验证、服役后可靠性增长等重点内容进行了分析,并结合我国航空发动机监视系统可靠性设计的实际需求,提出了采用全寿命周期的设计思想、考虑人为因素的影响、进行逐级分步的试验验证和在产品服役后开展可靠性增长工作等建议,为我国航空发动机监视系统可靠性设计标准的制定提供了技术支持。
SAE AIR 5120 in the definition of engine monitoring system reliability, design ideas, human factors, test validation, reliability increase after service and other key elements were analyzed, combined with the actual demand of our country aeroengine monitoring system reliability design, put forward Adopting the design idea of full life cycle, considering the influence of human factors, carrying out step-by-step step-by-step verification of test and work on reliability growth after service of products, etc. provide the design standards for the reliability of China’s aero-engine monitoring system Technical Support.