HYBRID COMPOSITE STRUCTURAL MEMBER

    公开(公告)号:EP3152114B1

    公开(公告)日:2018-12-05

    申请号:EP15728369.8

    申请日:2015-06-02

    CPC classification number: B64D11/0648 B64D11/06 B64D11/0649 B64D11/0696

    Abstract: A passenger seat (100) that includes at least one back rest frame (191-194) with at least one through-hole, at least one lateral structural member (101,102) that is perpendicular to the at least one back rest frame (191-194) and is disposed in the at least one through-hole, and at least one floor attachment frame (195,196) with at least one through-hole that is coaxial with the at least one through-hole of the at least one back rest frame (191-194). Each lateral structural member include an internal composite tube (101,102) that extends a full lateral width of the passenger seat and a plurality of outer tubes (151-162) disposed on an outer surface of the internal composite tube.

    TUBE DE STRUCTURE DE TYPE HYBRIDE, NOTAMMENT POUR SIÈGE AÉRONAUTIQUE
    9.
    发明公开
    TUBE DE STRUCTURE DE TYPE HYBRIDE, NOTAMMENT POUR SIÈGE AÉRONAUTIQUE 审中-公开
    TUBE DE STRUCTURE DE型HYBRIDE,NOTAMMENT POURSIÈGEAÉRONAUTIQUE

    公开(公告)号:EP3174791A1

    公开(公告)日:2017-06-07

    申请号:EP15744272.4

    申请日:2015-07-16

    CPC classification number: B64D11/0649 B64D11/06 Y02T50/46

    Abstract: The invention relates to a hybrid tube (22), in particular for an aircraft seat structure S, said structure comprising ribs (10) intended to receive the hybrid tube (22), said hybrid tube (22) including a monolithic carbon tube (24) and at least one sleeve (26) made from a ductile material and connected to the carbon tube by means of gluing, shrink-fitting or over-moulding.

    Abstract translation: 本发明涉及一种特别用于飞机座椅结构S的混合管(22),所述结构包括旨在容纳混合管(22)的肋(10),所述混合管(22)包括整体式碳管(24) )和至少一个由延性材料制成的套筒(26),并通过粘合,热缩或包覆成型与碳管连接。

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