首页> 外国专利> FITTING FOR FASTENING SATELLITE BODY STRUCTURE PANEL AND SATELLITE BODY STRUCTURE PANEL

FITTING FOR FASTENING SATELLITE BODY STRUCTURE PANEL AND SATELLITE BODY STRUCTURE PANEL

机译:卫星机身结构面板和卫星机身结构面板的装配

摘要

PROBLEM TO BE SOLVED: To solve the following problem in a sandwich panel used for an artificial satellite structure: a mass thereof becomes larger due to a large amount of components used because the sandwich panel with standard dimensions requires connection by a doubler or the like when a sandwich panel with dimensions larger than standard dimensions is applied and an additional fitting with bolt holes requires attachment of a fitting with bolt holes called an insert to fasten a web panel.;SOLUTION: A fastening fitting with at least two bolt holes is bonded between a sandwich panel skin and a core and is fastened by using a bolt and a U-shaped fastening fitting bonded to the sandwich panel to thereby perform fastening between a patch of the sandwich panel and the sandwich panel. Thus, reductions in the number of component items and weight can be achieved.;COPYRIGHT: (C)2013,JPO&INPIT
机译:要解决的问题:为了解决在人造卫星结构中使用的夹芯板中的以下问题:由于使用了大量的组件,因此其质量变大,因为标准尺寸的夹芯板在使用时需要通过倍增器等进行连接。夹层板的尺寸大于标准尺寸,并且附加了带螺栓孔的配件时需要连接带有螺栓孔的配件(称为插入件)以固定腹板。解决方案:解决方案:两个螺栓之间的紧固件至少有两个夹层板表皮和芯部,并通过使用螺栓和结合到夹层板上的U形紧固配件紧固,从而在夹层板的贴片和夹层板之间进行紧固。因此,可以减少部件数量和重量。.版权所有:(C)2013,JPO&INPIT

著录项

  • 公开/公告号JP2013184574A

    专利类型

  • 公开/公告日2013-09-19

    原文格式PDF

  • 申请/专利权人 MITSUBISHI ELECTRIC CORP;

    申请/专利号JP20120051236

  • 发明设计人 MORISAWA NOBUYUKI;

    申请日2012-03-08

  • 分类号B64G1/22;

  • 国家 JP

  • 入库时间 2022-08-21 17:03:11

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