发明名称 Access door between cockpit and cabin of aircraft has lock which operates from cockpit side and releases automatically if air pressure difference between cockpit and cabin exceeds set value
摘要 <p>The access door (8) between an aircraft cockpit and cabin has a cockpit side (8a) and a cabin side (8b). The door has a leaf (22) to close the opening (20) and opens towards the cabin. The door has a lock (30) operated from the cockpit side and released automatically when the pressure difference between the cockpit and the cabin, corresponding to the air pressure against the cockpit and cabin sides, is above a preset level.</p>
申请公布号 FR2848179(A1) 申请公布日期 2004.06.11
申请号 FR20020015526 申请日期 2002.12.09
申请人 AIRBUS FRANCE 发明人 ROQUES SERGE;PUJOL OLIVIER;PROST DOMINIQUE;MALAVALLE PHILIPPE
分类号 B64C1/14;B64D45/00;E05B65/10;(IPC1-7):B64C1/14;E06B7/02 主分类号 B64C1/14
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