发明名称 |
Apparatus and method for passive venting of rocket motor or ordnance case |
摘要 |
Passive venting apparatus and method for a rocket motor or ordnance device containing propellant or explosive material enclosed in a case, which presents an explosion hazard when subjected to external heat. A combustible strip is secured to the exterior surface of the case and is constructed to burn and generate sufficient heat when exposed to predetermined external heat to weaken the adjacent portion of the case and effect rupture of the case to vent interior gases therein prior to autoignition of the propellant or explosive.
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申请公布号 |
US6952995(B2) |
申请公布日期 |
2005.10.11 |
申请号 |
US20020042391 |
申请日期 |
2002.01.11 |
申请人 |
AEROJET-GENERAL CORPORATION |
发明人 |
FRIEDLANDER, III MARK PEYSER |
分类号 |
F02K9/38;F42B39/20;(IPC1-7):F41A9/00 |
主分类号 |
F02K9/38 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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