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.
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
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