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    SPLICE ASSEMBLY FOR JOINING STRUCTURAL COMPONENTS
    6.
    发明授权
    SPLICE ASSEMBLY FOR JOINING STRUCTURAL COMPONENTS 有权

    公开(公告)号：EP3028940B1

    公开(公告)日：2018-06-06

    申请号：EP15196204.0

    申请日：2015-11-25

    申请人： The Boeing Company

    发明人： Reeves, Andrew C.

    IPC分类号： B64C1/06 ,  B64C1/12

    CPC分类号： B64C1/069 ,  B64C1/061 ,  B64C1/064 ,  B64C1/12 ,  Y10T29/49622

    摘要： A splice assembly (100) may include a first splice bracket (102a) including first longitudinal axis (Xa), a first connecting member (104a), and a first mating member (106a) extending from the first connecting member (104a) along the first longitudinal axis (Xa), the first mating member (106a) including a first mating surface (108a) disposed at a non-zero first angle relative to the first longitudinal axis (Xa). The disclosed splice assembly (100) may further include a second splice bracket (102b) including second longitudinal axis (Xb), a second connecting member (104b), and a second mating member (106b) extending from the second connecting member (104b) along the second longitudinal axis (Xb), the second mating member (106b) including a second mating surface (108b) disposed at a non-zero second angle relative to the second longitudinal axis (Xb). The first mating surface (108a) and the second mating surface (108b) are complementary. Surface contact between the first mating surface (108a) and the second mating surface (108b) defines a fastening location for connecting the first splice bracket (102a) and the second splice bracket (102b).

    METHOD FOR BONDING FUSELAGE AND STRONG BACK
    9.
    发明公开
    METHOD FOR BONDING FUSELAGE AND STRONG BACK 审中-公开
    VERFAHREN ZUM VERBINDEN EINES RUMPFES UND STARKEN HECKTEILS

    公开(公告)号：EP2979810A4

    公开(公告)日：2016-11-16

    申请号：EP14774408

    申请日：2014-03-17

    申请人： MITSUBISHI HEAVY IND LTD

    发明人： YANAGIHARA HIDEYASU

    IPC分类号： B23P21/00 ,  B64F5/00

    CPC分类号： B64C1/069 ,  B23P19/10 ,  B23P2700/01 ,  B64C2001/0072 ,  B64F5/10 ,  Y02T50/433

    摘要： In the present invention, a fuselage is easily manufactured. The method of the present invention includes: scooping a trunk section (6) using a strong back (8-i), the trunk section (6) being supported by a dolly; disposing the trunk section (6) at a predetermined location by moving the strong back (8-i) using a positioner; and joining the trunk section (6) to a standard fuselage when the trunk body (6) is disposed at the predetermined location. This method for bonding a fuselage is capable of supporting the trunk section (6) by the positioner without using a crane. Therefore, according to this method for bonding a fuselage, it is possible to avoid having to provide to the trunk section (6) an outside fitting (101) used when the crane is used, and to more easily manufacture the fuselage.

    摘要翻译： 在本发明中，容易制造机身。 本发明的方法包括：使用强背（8-i）舀取躯干部分（6），所述躯干部分（6）由台车支撑; 通过使用定位器移动强力背部（8-i）将躯干部分（6）设置在预定位置; 并且当所述主体主体（6）设置在所述预定位置时，将所述主干部分（6）连接到标准机身。 这种用于接合机身的方法能够在不使用起重机的情况下由定位器支撑躯干部分（6）。 因此，根据该机身的接合方法，能够避免在使用起重机时使用的外部配件（101）向主干部（6）提供，并且能够更容易地制造机身。