发明名称 SNAP-IN WINDOW ASSEMBLY AND METHOD
摘要 An aircraft window assembly with a readily attachable window assembly for efficient and easy installation and maintenance of aircraft windows is provided. The aircraft has a sidewall having an inner perimeter that defines an opening. An inner window frame is readily attachable to the sidewall adjacent to the inner perimeter. The inner window frame defines a first opening. An outer window frame is readily attachable to the inner wind ow frame adjacent the first opening and the outer window frame defines a second opening. The outer window frame and the inner window frame are releasably coupled within the first opening of the inner window frame. The snap-in window assembly is readily detachable fr om the sidewall adjacent to the inner perimeter.
申请公布号 CA2405923(A1) 申请公布日期 2003.04.25
申请号 CA20022405923 申请日期 2002.10.01
申请人 THE BOEING COMPANY 发明人 JONES, GARY E.
分类号 B64C1/14;(IPC1-7):B64C1/14;B60J1/08 主分类号 B64C1/14
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