发明名称 |
PRESSURE RELIEF LATCH MECHANISM |
摘要 |
A latch mechanism for use in attaching portions or panels on an aircraft. The latch mechanism and related method include a detent mechanism for releasably coupling a bolt portion of the latch to a handle portion of the latch. The latch allows the bolt and handle to conjointly pivot with respect to a corresponding mounting bracket. The latch operates to relieve pressure in an excess pressure condition when the forces associated with the detention mechanism are overcome. |
申请公布号 |
WO2011069103(A1) |
申请公布日期 |
2011.06.09 |
申请号 |
WO2010US58957 |
申请日期 |
2010.12.03 |
申请人 |
HARTWELL CORPORATION;ROZEMA, TIMOTHY S. |
发明人 |
ROZEMA, TIMOTHY S. |
分类号 |
E05C19/12 |
主分类号 |
E05C19/12 |
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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