直升机基本可靠性预计方法应用  

Application of Helicopter Basic Reliability Prediction Method

作　　者：周健 郝宗敏[1] ZHOU Jian;HAO Zong-min(China Helicopter Design Institute,Jingdezhen 333001,China)

机构地区：[1]中国直升机设计研究所,景德镇333001

出　　处：《价值工程》2018年第29期250-252,共3页Value Engineering

摘　　要：本文介绍了直升机整机、系统和设备三个层次在不同的研制阶段采取相应的可靠性预计方法,确立了直升机各层次可靠性预计的一般流程以及各层次之间的关联性,提出在各层次进行基本可靠性预计的注意事项,并结合案例说明了所选取方法、分析流程等的可行性。This paper introduces the three levels of helicopters, systems and equipment to adopt corresponding reliability prediction methods in different development stages, and establishes the general process of reliability prediction at all levels of the helicopter and the correlation between the various levels, puts forwards the precautions for basic reliability prediction at each level, and explains the feasibility of the selected method and analysis process in combination with the case.

关 键 词：直升机 基本可靠性预计 

分 类 号：V275.1[航空宇航科学与技术—飞行器设计]