发明名称 Partition wall in an aircraft
摘要 The invention is based on a partition wall in an aircraft, wherein the partition wall comprises a support element and a tension-mounted material. According to the invention, the support element is composed of individually formed system components, and the tension-mounted material is supported by the support element such that an area-shaped partition wall is created in the aircraft.
申请公布号 US8960602(B2) 申请公布日期 2015.02.24
申请号 US200912394344 申请日期 2009.02.27
申请人 Airbus Operations GmbH 发明人 Neumann Andreas;Mosler Michael;Breuer Matthias
分类号 B64D11/04;B64D11/00;G09F21/06 主分类号 B64D11/04
代理机构 Lerner, David, Littenberg, Krumholz & Mentlik, LLP 代理人 Lerner, David, Littenberg, Krumholz & Mentlik, LLP
主权项 1. A partition wall separating first and second longitudinally adjacent regions in an aircraft, the partition wall comprising: a support element extending across a longitudinal direction of the aircraft; a tension-mounted material; a cross-strut for stiffening the support element; and a plurality of connecting elements spaced from each other and tension-mounting the tension-mounted material to the support element at least on a first side and on a second side of the support element; wherein the support element comprises a plurality of individually formed system components of a modular system; wherein the tension-mounted material is supported by the support element substantially surrounding the tension-mounted material such that the partition wall is created in the aircraft; and wherein the partition wall is mounted to a substructure of the aircraft and affixed only in the longitudinal direction of the aircraft, thereby preventing forces acting across the longitudinal direction from being transmitted to the partition wall from the substructure or from the partition wall to the substructure.
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