摘要
从系统可靠性评估的角度出发,针对飞机方案论证阶段或初步设计阶段的设计重点和数据特点,提出一种新的结构可靠性区间估算分析方法,供方案论证阶段或初步设计阶段的飞机结构可靠性评估用。该方法简单、实用,对飞机的结构方案的可靠性评估与评价有指导意义。
According to the specialty and keystone of aircraft preliminary design, a novel approach to structure reliability interval estimation is developed, which could be used in General Configuration Definition Phase （GCDP） or Preliminary Design Phase of aircraft design. This approach is simple and very useful to engineering.
出处
《民用飞机设计与研究》
2012年第1期40-41,52,共3页
Civil Aircraft Design & Research
关键词
结构可靠性
区间估算
飞机结构
方案论证阶段
structure reliability
interval estimation
aircraft structure
general configuration definition phase
