3) ladle life
钢包寿命
4) life envelope
寿命包线
1.
Based on the introduction of the concept of aircraft structural life envelope(ASLE),the basic approach and practical engineering method of determining ASLE by experiments under the baseline operational conditions are presented,as well as the basic approach and practical engineering method of determining ASLE by experiments under non-baseline operational conditions.
在飞机结构寿命包线概念基础上,阐述了基准使用条件下由实验确定飞机结构寿命包线的基本方法及工程简化方法,进一步说明了在非基准使用条件下实验确定飞机结构寿命包线的基本方法及工程简化方法,为实现飞机结构单机寿命(疲劳寿命和日历寿命)监控奠定了基础。
2.
Based on the analysis of the aircraft structural life envelope(ASLE) under the baseline operational conditions,an approach of establishment of aircraft structural life envelope(ASLE) under nonbaseline operational conditions is presented.
在分析基准使用条件下飞机结构寿命包线的基础上,给出飞机结构在非基准使用条件下的寿命包线的绘制方法,阐明了在非基准使用条件下对飞机结构进行单机寿命监控的原理与方法。
3.
At last,a piece of basic life envelope of aluminum alloy samples under certain corrosive and fatigue condition is established.
以飞机结构寿命包线的理论体系为基础,以LY12CZ铝合金试件为试验对象,并模拟不同的飞行强度条件对飞机结构件疲劳寿命的影响,开展了疲劳-腐蚀周期性交替试验来确定试验件的疲劳寿命和日历寿命。
5) package life
包装寿命
6) tundish work life
中间包寿命
补充资料：钢坯加热炉低位汽包汽化冷却装置
钢坯加热炉低位汽包汽化冷却装置
钢坯加热炉低位汽包汽化冷却装置
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条