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AIRCRAFT VERTICAL TAIL ATTACHMENT APPARATUS AND AIRCRAFT VERTICAL TAIL ATTACHMENT METHOD

机译:飞机垂直尾翼附着装置和飞机垂直尾翼附着方法

摘要

PROBLEM TO BE SOLVED: To enable safe and reliable attachment of a vertical tail to a rear fuselage with fewer personnel without using a ceiling crane device and to improve fuselage production efficiency.SOLUTION: A vertical tail attachment apparatus 1 includes: a pair of tower structures 2F and 2R installed upright on an assembly floor to face each other, and having a rear fuselage arrangement space S therebetween in which a rear fuselage RF can be arranged along a fuselage longitudinal direction X; a beam 3 that is installed between the tower structures 2F and 2R, that can rise/fall along a vertical direction Z, that can rotate about an axis along the fuselage longitudinal direction X, and that rises/falls and rotates while holding a vertical tail VS; and an elevating rotation mechanism 5 that causes the beam 3 to rise/fall along the vertical direction Z of the tower structures 2F and 2F, and that rotates the beam 3 such that the vertical tail VS held by the beam 3 changes an attitude from a generally horizontal attitude to a vertical attitude in response to the rise of the beam 3 from a lower side of the tower structures 2F and 2F to an upper side thereof.
机译:要解决的问题:在不使用天花板起重机装置的情况下,以更少的人员来确保垂直尾巴安全可靠地附接到后机身,并提高机身生产效率。解决方案:垂直尾巴附设装置1包括:一对塔架结构图2F和图2R竖立安装在组装地板上以彼此面对,并且具有在后机身布置空间S之间的后机身布置空间S,后机身RF可以沿着机身纵向X布置。安装在塔架结构2F和2R之间的梁3,其可以沿竖直方向Z上升/下降,可以围绕沿机身纵向X的轴线旋转,并且在保持竖直尾部的情况下上升/下降和旋转VS;升降旋转机构5,其使梁3沿塔架结构2F,2F的上下方向Z升降,并使梁3旋转,以使由梁3保持的垂直尾部VS相对于塔架3的姿势变化。响应于梁3从塔架结构2F和2F的下侧到其上侧的上升,通常在水平方向到竖直方向的姿态。

著录项

  • 公开/公告号JP2015093622A

    专利类型

  • 公开/公告日2015-05-18

    原文格式PDF

  • 申请/专利权人 MITSUBISHI HEAVY IND LTD;

    申请/专利号JP20130235260

  • 发明设计人 YANAGIHARA HIDEYASU;

    申请日2013-11-13

  • 分类号B64F5/00;B64C5/06;

  • 国家 JP

  • 入库时间 2022-08-21 15:34:53

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