Window panel for an airframe and method of producing same

申请号 US14469146 申请日 2014-08-26 公开(公告)号 US09902483B2 公开(公告)日 2018-02-27
申请人 Airbus Operations GmbH; 发明人 Pierre C. Zahlen; Johannes Born; Lars Meyer; Gregor Baumbach; Claus Hanske; Jens Prowe; Johan Oentoro; M. Ichwan Zuardy; Wouter Brok; Martin Metten;
摘要 The present disclosure pertains to a window panel for a body structure of a vehicle, especially an airframe of an aircraft or spacecraft, including a first skin which extends over a first side of the panel to form an outer skin of the vehicle body structure; a second skin which extends over a second side of the panel to form an inner skin of the vehicle body structure; and a core, especially a foam core, located between and covered by the first and second skins in a sandwich structure. The window panel includes at least one window aperture formed through the first layer, the core, and the second layer. The core may be confined to or extends over a limited extent, region or part of the panel. Thus, the first skin and/or the second skin may extend over or cover a greater area of the panel than the core.
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