摘要
在总结整机可靠性分配工作的工程约束的基础上 ,针对性地提出了一种实用性好的整机基本可靠性指标与任务可靠性指标协调分配模型。该模型在某教练飞机的可靠性分配中进行了运用 。
Based on the analysis of the engineering restrictions for whole aircraft reliability allocation, a practicable model for basic & mission reliability coordinated allocation is put forward in this paper. The model has been used in a trainer aircraft reliability allocation task, and its rationality and engineering applicability are proved.
出处
《航空学报》
EI
CAS
CSCD
北大核心
2001年第5期461-464,共4页
Acta Aeronautica et Astronautica Sinica