首页> 外国专利> LOAD-BEARING PANEL OF SPACECRAFT CASE (VERSIONS)

LOAD-BEARING PANEL OF SPACECRAFT CASE (VERSIONS)

机译:航天飞机箱的承重面板(版本)

摘要

FIELD: rocketry and space engineering; structural members of spacecraft case.;SUBSTANCE: proposed load-bearing panel has frame and load-bearing lower and upper bases with cellular filler arranged in between bases and frame. For communication of interiors of honeycomb cells, provision is made for drain holes in side surfaces of each honeycomb cell. According to first version, communication of interiors of honeycomb cells is carried out through drain holes available in at least one member of frame; according to second version, drain holes are made in at least one load-bearing members of panel smoothly over area of its surface; according to third version, drain holes are made in at least one member of frame and in least one load-bearing base of panel smoothly over area of its surface. Total areas of drain holes in said structural members are determined with total volume of gas medium in honeycomb cells, drainage coefficient of drain holes and maximum pressure differential of gas medium acting on bases of panel taken into account.;EFFECT: enhanced structural strength of load-bearing members of spacecraft case without increase of their mass; facilitated procedure of manufacture and ease in mounting the panels; enhanced operational reliability.;4 cl, 4 dwg
机译:领域:火箭与太空工程;物质:拟议的承重面板具有框架和承重的下部和上部基座,在基座和框架之间布置有蜂窝状填充物。为了连通蜂窝单元的内部,在每个蜂窝单元的侧面上设置了排水孔。根据第一版本,通过至少在框架的一个构件中可用的排泄孔进行蜂窝单元内部的连通。根据第二种形式,在面板的至少一个承重构件上在其表面的整个区域上平滑地形成排水孔。根据第三种形式,在框架的至少一个构件和面板的至少一个承重基座上平滑地在其表面区域上开有排水孔。所述结构构件中的排水孔的总面积由蜂窝状单元中的气体介质的总体积,排水孔的排水系数和作用于面板底部的气体介质的最大压差共同决定。效果:增强的载荷结构强度-不增加质量的航天器箱的承重成员;简化了制造过程并易于安装面板;增强的操作可靠性。; 4 cl,4 dwg

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号