Cargo barrier net
    2.
    发明公开
    Cargo barrier net 有权
    Frachtfangnetz

    公开(公告)号:EP2202149A3

    公开(公告)日:2014-12-31

    申请号:EP09180164.7

    申请日:2009-12-21

    IPC分类号: B64D9/00 B60P7/08 B60R21/06

    摘要: A cargo barrier net (2) for an aircraft comprising: a net mesh, defined by a plurality of net strands (4, 6); a plurality of securing means (14) attached to at least some of the net strands (4, 6), for securing the cargo barrier net (2) across an internal space of an aircraft; and at least one tear webbing (18, 30) located between a securing means (14) and a net strand (4, 6), wherein the tear webbing (18, 30) is configured to tear progressively when a load is applied to it, thereby increasing the effective length of net strand (4, 6) to which it is attached and redistributing the load to other net stands (4, 6) in the cargo barrier net (2).

    摘要翻译: 1.一种用于飞行器的货物防护网(2),包括:网状网,由多个网线(4,6)限定; 多个固定装置(14),其附接到所述网线(4,6)的至少一些,用于将所述货物屏障网(2)固定在飞行器的内部空间上; 以及位于固定装置(14)和网状股(4,6)之间的至少一个撕裂织带(18,30),其中所述撕裂织带(18,30)构造成在施加负载时逐渐撕裂 从而增加其连接的网线4,6(4,6)的有效长度,并且将负载重新分配到货物隔离网(2)中的其它网架(4,6)上。

    Cargo barrier net
    3.
    发明公开
    Cargo barrier net 有权
    FrachtfangnetzfürFlugzeuge

    公开(公告)号:EP2202149A2

    公开(公告)日:2010-06-30

    申请号:EP09180164.7

    申请日:2009-12-21

    IPC分类号: B64D9/00

    摘要: A cargo barrier net (2) for an aircraft comprising: a net mesh, defined by a plurality of net strands (4, 6); a plurality of securing means (14) attached to at least some of the net strands (4, 6), for securing the cargo barrier net (2) across an internal space of an aircraft; and at least one tear webbing (18, 30) located between a securing means (14) and a net strand (4, 6), wherein the tear webbing (18, 30) is configured to tear progressively when a load is applied to it, thereby increasing the effective length of net strand (4, 6) to which it is attached and redistributing the load to other net stands (4, 6) in the cargo barrier net (2).

    摘要翻译: 1.一种用于飞行器的货物防护网(2),包括:网状网,由多个网线(4,6)限定; 多个固定装置(14),其附接到所述网线(4,6)的至少一些,用于将所述货物屏障网(2)固定在飞行器的内部空间上; 以及位于固定装置(14)和网状股(4,6)之间的至少一个撕裂织带(18,30),其中所述撕裂织带(18,30)构造成在施加负载时逐渐撕裂 从而增加其连接的网线4,6(4,6)的有效长度,并且将负载重新分配到货物隔离网(2)中的其它网架(4,6)上。