发明名称 Cockpit door of aircraft
摘要 The cockpit door has a hinge on one side and a latch device on the other side that can be operated only from the cockpit side. To the inner side of the door panel is mounted a reinforcement member 100 having a body formed by laminating layers of aromatic polyamide fiber sheets and thermoplastic adhesive and subjecting the same to hot pressing to form an integral member. Mounting portions 150 and 160 are formed to the rim portion of the reinforcement member body 110, and rivet inserting holes 180 are machined to the portions. The mounting portions are bent by 90 degrees, and fixed to a frame using rivets. <IMAGE>
申请公布号 EP1440884(A3) 申请公布日期 2005.07.06
申请号 EP20030023044 申请日期 2003.10.14
申请人 JAMCO CORPORATION 发明人 TAKAHAMA, HIRONOBU
分类号 E06B5/00;B64C1/14;B64D45/00;(IPC1-7):B64D45/00;F41H5/04 主分类号 E06B5/00
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