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NODE OF THE FUSELAGE COMPARTMENT WITH MESH AND TRADITIONAL CONSTRUCTIVE-POWER CIRCUITS

机译:网格和传统建设性电力的机身隔室节点

摘要

FIELD: aviation.SUBSTANCE: invention relates to the field of aviation structures with various structural-power circuits (SPC), in particular, to the grid power structure of the fuselage compartment of a civil aircraft. Joint unit of the fuselage compartments with a mesh and traditional SPC contains spiral ribs and an end ring rib of the mesh compartment. Moreover, the spiral ribs are released beyond the edge annular rib for a distance of at least 10 mm in such a way that the intersecting ribs form an arc of a circle with a radius of at least 10 mm. Metal frame with grooves is placed close to the end ring rib, into which are placed spiral ribs outside the end rib, covered with a lid, which is tightened to the metal frame by bolts. Sheathing and stringers of the compartment with traditional SPC are connected to the metal frame through fittings by means of a bolted connection. Sheathing of adjacent compartments is attached with an overlap to the metal frame by means of a bolted connection. Moreover, the width of the end annular rib is not less than the width of the spiral ribs.EFFECT: necessary strength of the connection of the mesh compartment with the compartments of the traditional SPC fuselage is being achieved.1 cl, 3 dwg
机译:技术领域本发明涉及具有各种结构动力电路(SPC)的航空结构领域,尤其涉及民用飞机的机身舱室的电网动力结构。带有网孔和传统SPC的机身隔室的接头单元包含网状隔室的螺旋肋和端环肋。此外,螺旋肋以超出边缘环形肋至少10mm的距离的方式被释放,使得相交的肋形成半径为至少10mm的圆弧。带有凹槽的金属框架放置在靠近端部环形肋的位置,端部肋的外侧放置有螺旋肋,并盖上盖子,并通过螺栓将其拧紧到金属框架。具有传统SPC的隔间的护套和桁条通过螺栓连接通过配件连接到金属框架。相邻隔间的护套通过螺栓连接以重叠的方式连接到金属框架。而且,端部环形肋的宽度不小于螺旋肋的宽度。效果:实现了网状隔室与传统SPC机身隔室之间连接的必要强度。1 cl,3 dwg

著录项

  • 公开/公告号RU2016145655A3

    专利类型

  • 公开/公告日2018-05-23

    原文格式PDF

  • 申请/专利权人

    申请/专利号RU20160145655

  • 发明设计人

    申请日0000-00-00

  • 分类号B64C1/12;

  • 国家 RU

  • 入库时间 2022-08-21 12:36:20

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