1) solid motor safe device
固体发动机保险机构
2) launch insurance mechanism
发射保险机构
3) trigger lock
触发机构保险器
4) Solid engine
固体发动机
1.
Based on the structure characteristic of the solid engine, the principle of the sealing ring and the distributions of contact pressure stress at the sealing contact areas were analyzed, the sufficient and necessary conditions of sealing were given for solid engine.
根据固体发动机密封结构的特点 ,从密封圈的密封机理出发 ,对固体发动机密封的充分必要条件及密封界面的接触压应力分布进行分析 ,研究了粘弹性材料的压缩回弹特性、应力松弛特性和一些可能的密封失效因素 ,为固体发动机结构密封工作可靠性及密封圈的正确选用提供了依据。
5) solid motor
固体发动机
1.
A kind of automatic segmentation method for solid motor CT image;
固体发动机CT图像的一种自动分割方法
2.
Displacement analysis of solid motor grain under long-time gravity load;
长期自重载荷作用下固体发动机药柱的位移分析
3.
The analysis of pressure leak process for solid motor being cut off;
固体发动机切割分离泄压过程分析
6) Solid rocket motor
固体发动机
1.
The structure integrity analysis of solid rocket motor grain with cohesive cavity;
含内聚空洞的固体发动机药柱结构完整性分析
2.
The heat transfer through the case and liner of a solid rocket motor to the outside of the propellant grain was simulated numerically by use of the thermal conductivity equation with source term.
采用带源项的热传导方程,对固体火箭发动机在外界热源作用下的加热过程进行了数值模拟,分析了固体发动机内推进剂在外界热源作用下的燃烧特点,并确定了发动机产生热危险性的临界温度和起始燃烧时间。
3.
The response of solid rocket motor that exposed to the thermal load was simulated by use of the thermal conductivity equations with source term.
采用带源项的热传导方程,对固体火箭发动机在遭受热载荷时的响应情况进行了数值模拟,有效地评估了在外界热载荷作用下固体发动机的危险性,并提出了减少发动机热危险性的措施。
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
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