DRAINAGE SYSTEM
    1.
    发明申请
    DRAINAGE SYSTEM 有权
    排水系统

    公开(公告)号:US20160236769A1

    公开(公告)日:2016-08-18

    申请号:US14977928

    申请日:2015-12-22

    IPC分类号: B64C7/00

    CPC分类号: B64C5/02 B64C1/1453

    摘要: There is provided a drainage system of an aircraft which discharges moisture having entered inside horizontal tails, which are structures of an airframe of an aircraft, toward the rear end of a fuselage, the drainage system including: a drainage channel which includes an introduction end and a discharge end, and by a capillary action delivers moisture introduced from the introduction end toward the discharge end; and a heater which heats and dries the moisture delivered through the drainage channel. The drainage channel of the present invention is preferably composed of a paper drainage material. It is also preferable that the introduction end of the drainage channel is provided in a lowermost region in the vertical direction within an area in which moisture can accumulate inside the horizontal tails while the aircraft is parked.

    摘要翻译: 提供了一种飞机的排水系统,其排出作为机身的机身的结构的飞机内侧的水平尾部朝向机身的后端排出的水分,该排水系统包括:排水通道,其包括引入端和 排出端,并且通过毛细管作用将从引入端引入的湿气输送到排出端; 以及对通过排水通道输送的水分进行加热和干燥的加热器。 本发明的排水通道优选由排纸材料构成。 还优选的是,在飞行器停放的同时,在水平尾部内的水分积聚的区域内,排水通道的引导端部设置在垂直方向的最下部的区域。

    METHOD FOR REPAIRING LIGHTNING PROTECTION MATERIAL, AND MEMBER PROVIDED WITH LIGHTNING PROTECTION MATERIAL
    2.
    发明申请
    METHOD FOR REPAIRING LIGHTNING PROTECTION MATERIAL, AND MEMBER PROVIDED WITH LIGHTNING PROTECTION MATERIAL 审中-公开
    用于维护防雷材料的方法,以及提供防雷材料的部件

    公开(公告)号:US20160137310A1

    公开(公告)日:2016-05-19

    申请号:US14876137

    申请日:2015-10-06

    IPC分类号: B64D45/02 B64C1/12

    CPC分类号: B64D45/02

    摘要: The present invention provides a method for repairing a lightning protection material that is made of a metal material and is provided along a surface of a member formed by using a fiber reinforced resin includes: bonding a repair material made of a metal material over a lost region of the member where the lightning protection material is lost by using a liquid adhesive and a sheet-shaped holder that contains and holds the adhesive and is arranged at the lost region.

    摘要翻译: 本发明提供一种修复由金属材料制成的防雷材料的方法,沿着通过使用纤维增强树脂形成的构件的表面设置,包括:将由金属材料制成的修补材料粘结在失去的区域上 通过使用液体粘合剂而损坏防雷材料的构件和包含并保持粘合剂并且布置在丢失区域的片状保持器。

    REPAIR METHOD OF REPAIR TARGET PORTION, AND REPAIRED PRODUCT OBTAINED FROM REPAIRING
    3.
    发明申请
    REPAIR METHOD OF REPAIR TARGET PORTION, AND REPAIRED PRODUCT OBTAINED FROM REPAIRING 有权
    维修对象部分修理方法及修理后的维修产品

    公开(公告)号:US20140295124A1

    公开(公告)日:2014-10-02

    申请号:US14226983

    申请日:2014-03-27

    IPC分类号: B29C73/10

    摘要: The present invention relates to a repair method using a pre-cured repairing patch, and a repaired product obtained from repairing using the repairing patch, and the present invention securely bonds a repairing patch, where an out-of-plane stiffness is required, to a repair target. In order to cover a repair target portion 23 formed in an outer panel 2 with a repairing patch 30, and bond the repairing patch 30 to a repair target, repairing plates 31, 32 that are formed of fibers and thermosetting resin, and pre-cured before repairing are used as the repairing patch 30, and a laminating step S4 of laminating the repairing plates 31, 32, and a bonding step S7 of bonding the repairing plates 31, 32 to each other are performed.

    摘要翻译: 本发明涉及一种使用预固化修复补片的修复方法以及使用修补补片进行修复的修补产品,并且本发明将需要的平面外刚度的修复补片牢固地结合到 修复目标。 为了覆盖用修补补片30形成在外板2中的修补目标部分23,并将修补补片30粘合到修复对象上,由纤维和热固性树脂形成的修复板31,32和预固化 在修复之前用作修补贴片30,并且执行层压修复板31,32的层压步骤S4和将修复板31,32彼此粘合的粘合步骤S7。

    METHOD FOR LOCATING MACHINING POSITION IN REPAIR MATERIAL, AND REPAIRING METHOD
    4.
    发明申请
    METHOD FOR LOCATING MACHINING POSITION IN REPAIR MATERIAL, AND REPAIRING METHOD 审中-公开
    用于定位修复材料中的加工位置的方法和修复方法

    公开(公告)号:US20160137316A1

    公开(公告)日:2016-05-19

    申请号:US14875982

    申请日:2015-10-06

    IPC分类号: B64F5/00 G01N29/07 B23P6/00

    摘要: The present invention provides a method for locating a machining position in a repair material that is arranged on a member including a machined portion formed by predetermined machining, the method including: a step of arranging a marker including a portion having a different propagation characteristic of an ultrasonic wave from that of a peripheral portion in the machined portion existing in the member before the repair material is arranged on the member; and a step of applying the ultrasonic wave to the member covered with the repair material and locating the machining position at a position of the marker captured by the ultrasonic wave after the repair material is arranged on the member.

    摘要翻译: 本发明提供了一种在修补材料中定位加工位置的方法,该修补材料布置在包括通过预定加工形成的加工部分的构件上,该方法包括:将包括具有不同传播特性的部分的标记 在修复材料上存在于构件中的加工部分中的周边部分的超声波布置在构件上; 以及将修复材料布置在构件上之后,将超声波施加到覆盖有修补材料的构件并将加工位置定位在由超声波捕获的标记的位置处的位置。

    METHOD FOR REPAIRING HONEYCOMB CORE SANDWICH STRUCTURAL BODY AND REPAIRED PRODUCT
    6.
    发明申请
    METHOD FOR REPAIRING HONEYCOMB CORE SANDWICH STRUCTURAL BODY AND REPAIRED PRODUCT 有权
    修复蜂窝结构体和修复产品的方法

    公开(公告)号:US20140295123A1

    公开(公告)日:2014-10-02

    申请号:US14221595

    申请日:2014-03-21

    IPC分类号: B32B43/00 B64C3/26 B64C1/12

    摘要: A method for repairing a honeycomb core sandwich structural body according to the present invention is a method in which a damaged portion that is formed in a honeycomb core sandwich structural body where a honeycomb structured core is held between a first outer skin and a second outer skin and that reaches the core through the first outer skin is repaired, the method including: a repair material mounting step of mounting a repair material on the damaged portion, the repair material including a patch that covers an opening of the damaged portion, and one or a plurality of braces that support the patch; a patch bonding step of bonding the patch to the first outer skin; and a brace bonding step of bonding the brace to the second outer skin or the core.

    摘要翻译: 根据本发明的蜂窝芯夹层结构体的修复方法是将蜂窝结构体芯保持在第一外皮和第二外皮之间的蜂窝芯夹层结构体中形成的损伤部 并且通过所述第一外皮到达所述芯部的方法包括:修复材料安装步骤,将修复材料安装在所述损坏部分上,所述修复材料包括覆盖所述损坏部分的开口的贴片,以及一个或 多个支撑贴片的支架; 将贴片粘合到第一外皮上的贴片结合步骤; 以及将所述支架粘合到所述第二外皮或所述芯的支撑结合步骤。