发明名称 Retaining lock for pressurised aircraft - has slidable lock sections held by axial locking pins and shear pins
摘要 The retaining-lock (3) consists of two sections (4, 5), one connected to a decompression blow-out panel (2), and the other to the separating bulkhead or floor (6). The sections can slide apart, but are held together by axial locking-pins (7, 8), and internal, radially mounted, weak-necked shear-pins (9, 10). A large pressure differential, such as experienced in an explosive decompression, shears one pin-head (9a, 10a) in each lock (3), and releases the safety-panel. USE/ADVANTAGE - Retention of hold-to-cabin decompression safety-panels in pressurised aircraft. The shear pins give more predictable operation and allow easier installation.
申请公布号 DE4103014(C1) 申请公布日期 1992.03.12
申请号 DE19914103014 申请日期 1991.02.01
申请人 DEUTSCHE AIRBUS GMBH, 2000 HAMBURG, DE 发明人 HARARAT-TEHRANI, MOHAMAD, 2800 BREMEN, DE
分类号 B64C1/18 主分类号 B64C1/18
代理机构 代理人
主权项
地址