- 专利标题： Electronic thermally-initiated venting system (ETIVS) for rocket motors
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申请号： US13999547申请日： 2014-04-10
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公开(公告)号： US10670381B1公开(公告)日： 2020-06-02
- 发明人: Paul E. Anderson , Michael D. Haddon
- 申请人： THE GOVERNMENT OF THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY
- 申请人地址： US DC Washington
- 专利权人： The United States of America, as Represented by the Secretary of the Navy
- 当前专利权人： The United States of America, as Represented by the Secretary of the Navy
- 当前专利权人地址： US DC Washington
- 代理机构： Naval Air Warfare Center Weapons Division
- 代理商 James M. Saunders
- 主分类号： F42B39/14
- IPC分类号： F42B39/14 ; F42C11/00
摘要：
An electronic thermally-initiated venting system (ETIVS) for rocket motors includes at least one linear-shaped charge attached to a rocket motor housing. At least one exploding foil initiator (EFI) is attached to the linear-shaped charge. At least one electronic thermally-initiated venting system circuit is electrically-connected to the EFI. The EFI is configured to auto-fire when the electronic thermally-initiated venting system circuit relays a current pulse through the EFI. The linear-shaped charge is configured to initiate when the current pulse is relayed through the EFI.
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