STRUCTURE OF NOZZLE FOR FLUID TANK PIPING
    1.
    发明公开
    STRUCTURE OF NOZZLE FOR FLUID TANK PIPING 审中-公开
    流体罐管道喷嘴的结构

    公开(公告)号:EP3187431A1

    公开(公告)日:2017-07-05

    申请号:EP15836372.1

    申请日:2015-07-23

    IPC分类号: B65D25/42 B65D90/00

    摘要: A structure whereby a piping nozzle (22) can be simply attached to a tank body (12) in a short amount of time without limitations to the work location. A cylinder (32) of a nozzle body (24) is inserted through the interior and exterior of the tank body (12) via a nozzle body insertion hole (36) in the tank body (12). A skirt (34) is provided on an end portion of the cylinder (32), and expands annularly from the end portion of the cylinder (32) in the interior of the tank body (12). A sealing member (26) is interposed between an inner surface (1202) of the tank body (12) and the skirt (34) around the nozzle body insertion hole (36). A spacer member (28) is disposed on an outer surface of the tank body (12) around the cylinder (32). By tightening a nut (30) on a male screw (3202) of the cylinder (32) of the nozzle body (24), a portion of the tank body (12) around the nozzle body insertion hole (36) is sandwiched by the skirt (34) of the nozzle body (24) and the spacer member (28).

    摘要翻译: 可以在短时间内简单地将管道喷嘴(22)连接到罐体(12)而不限制工作位置的结构。 喷嘴体(24)的气缸(32)通过罐体(12)内的喷嘴体插入孔(36)插入到罐体(12)的内部和外部。 裙部(34)设置在圆筒(32)的端部上,并且从圆筒(32)的端部在箱体(12)的内部环状地膨胀。 密封构件(26)插入在罐体(12)的内表面(1202)和围绕喷嘴主体插入孔(36)的裙部(34)之间。 间隔件(28)设置在罐体(12)的围绕圆筒(32)的外表面上。 通过将螺母(30)拧紧在喷嘴体(24)的圆筒(32)的外螺纹(3202)上,罐体(12)的围绕喷嘴体插入孔(36)的部分被夹在 喷嘴主体(24)的裙部(34)和间隔构件(28)。

    AIRCRAFT WATER TANK
    2.
    发明公开
    AIRCRAFT WATER TANK 审中-公开

    公开(公告)号:EP3708519A1

    公开(公告)日:2020-09-16

    申请号:EP18876362.7

    申请日:2018-06-29

    IPC分类号: B65D90/12 B64D11/04 B65D88/14

    摘要: An aircraft water tank is provided that allows for an increase in thickness of a metal plate while suppressing an increase in thickness of an attachment plate portion, and that prevents the attachment plate portion from being damaged. With an aircraft water tank 10 being suspended by a fuselage via bushes 36, a load applied to each of the bushes 36 is transferred from the bush 36 and an attachment hole 34 to a metal plate 32. The load transferred to metal plate 32 is transferred to a total of four prepreg projection portions P4D, P5D, P4D, and P5D at a section of a thick wall portion 32A of the metal plate 32 and transferred to a total of eight prepreg projection portions P2D, P3D, P4D, P5D, P2D, P3D, P4D, and P5D at a section of a thin wall portion 32B.