发明名称 |
Lock for aircraft H.U.D. combiner |
摘要 |
The lock has a slot formed in a first section and having first and second abutment surfaces spaced apart in the direction of the movement. A heel portion is integral with or rigidly fixed to the second section and projects from the second section into the slot and has third and fourth abutment surfaces spaced apart in the direction of the movement. The third abutment surface is arranged to engage the first abutment surface to limit relative movement in a first direction when the apparatus is unlocked. A locking wedge is mounted in the second section.
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申请公布号 |
FR2726054(A1) |
申请公布日期 |
1996.04.26 |
申请号 |
FR19950011801 |
申请日期 |
1995.10.06 |
申请人 |
PILKINGTON P E LIMITED |
发明人 |
GARDAM ALLAN;JONES ANDREW DAVID |
分类号 |
E05D11/10;G02B27/00;G02B27/01;(IPC1-7):F16B3/00 |
主分类号 |
E05D11/10 |
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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