LATERAL PLY LAYUP OF COMPOSITE SPAR
    1.
    发明公开
    LATERAL PLY LAYUP OF COMPOSITE SPAR 审中-公开
    SEITLICHES LAGEN-LAYUP EINES VERBUNDHOLMS

    公开(公告)号:EP2982598A2

    公开(公告)日:2016-02-10

    申请号:EP15177127.6

    申请日:2015-07-16

    发明人: Pitman, Brian

    IPC分类号: B64C3/18

    摘要: A structural component, including a composite tapered wing spar (1000) including a first fiber layer and a main web, wherein respective longitudinal axes (999) of fibers (1151) making up the first layer at least substantially lying on a plane corresponding to the main web of the wing spar (1000) are curved over at least most of the respective lengths of the fibers.

    摘要翻译: 一种结构部件,包括包括第一纤维层和主网的复合锥形翼梁(1000),其中构成第一层的纤维(1151)的相应纵轴(999)至少基本上位于与 翼梁(1000)的主网在至少大部分纤维长度上弯曲。

    LATERAL PLY LAYUP OF COMPOSITE SPAR
    3.
    发明公开
    LATERAL PLY LAYUP OF COMPOSITE SPAR 审中-公开
    面层铺层的复合霍尔姆斯

    公开(公告)号:EP2982598A3

    公开(公告)日:2016-05-11

    申请号:EP15177127.6

    申请日:2015-07-16

    发明人: Pitman, Brian

    IPC分类号: B64C3/18

    摘要: A structural component, including a composite tapered wing spar (1000) including a first fiber layer and a main web, wherein respective longitudinal axes (999) of fibers (1151) making up the first layer at least substantially lying on a plane corresponding to the main web of the wing spar (1000) are curved over at least most of the respective lengths of the fibers.