The invention discloses a flat plate type satellite configuration, and relates to the field of satellite overall configuration design. The planar satellite configuration may include: an upper mounting plate; a lower mounting plate; the carbon fiber frame is clamped between the upper mounting plate and the lower mounting plate, so that the flat plate type satellite configuration is in a flat plate shape on the whole, the carbon fiber frame is composed of a plurality of rod-shaped pieces which are independent of one another, each rod-shaped piece is fixed to the upper mounting plate and the lower mounting plate, and the carbon fiber frame is clamped between the upper mounting plate and the lower mounting plate. The carbon fiber frame comprises a closed peripheral part and a central part inside the peripheral part, the two ends of each rod piece of the central part are fixed to the rod pieces of the peripheral part through corner boxes, and every two adjacent rod pieces in the peripheral part are also fixed to each other through corner boxes. Therefore, the production process is simplified, the adaptability and the flexibility are improved, and the structural strength and the stability of the satellite can be ensured.
本发明公开了一种平板式卫星构型,涉及卫星总体构型设计领域。该平板式卫星构型可以包括:上安装板;下安装板;碳纤维框架,所述碳纤维框架夹置在所述上安装板与所述下安装板之间,使得所述平板式卫星构型整体上呈平板状,其中,所述碳纤维框架由相互独立的多个杆状件构成,每个杆状件均固定至所述上安装板以及所述下安装板,其中,所述碳纤维框架包括闭合的外周部分以及所述外周部分内部的居中部分,所述居中部分的每个杆状件的两个端部借助于角盒固定至所述外周部分的杆状件,并且所述外周部分中相邻的两个杆状件之间也借助于角盒固定至彼此。由此简化了生产过程,提高了适应性和灵活性,而且能够确保卫星的结构强度和稳定性。
Flat plate type satellite configuration
一种平板式卫星构型
2024-05-24
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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