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satellite transport box

A technology for transport boxes and satellites, which is applied in the field of satellite transport boxes, can solve the problems of cumbersome satellite transportation operations, etc., and achieve the effects of increasing the bottom surface area, improving anti-skid performance, and improving toughness and strength

Active Publication Date: 2021-07-23
烟台海上航天科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention proposes a satellite transport box to overcome the problems of cumbersome satellite transport operations in the prior art

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0032] refer to Figure 1-Figure 6 , a satellite transport box, including a box body 1, one end of the inner wall of the box body 1 close to the inner bottom is fixed with a bottom plate 2 by bolts, the top of the box body 1 is connected with a top cavity cover 13 by a hinge, and the top of the bottom plate 2 is connected with a top cavity cover 13. A supporting mechanism is installed on the outer wall, and a fixed side plate 4 is vertically welded on both sides of the top outer wall of the bottom plate 2 , a follow-up clamping mechanism is installed on the opposite side of the fixed side plate 4 , and a top cavity cover 13 is installed. The top pressing mechanism and the supporting mechanism include the main box body 20 fixed on the top outer wall of the bottom plate 2 by bolts, and the inner wall of the main box body 20 is slidably connected with the piston plate 3, and both sides of the top outer wall of the piston plate 3 are fixed by bolts There is a vertical plate 19, an...

Embodiment 2

[0034] refer to figure 1 , the follow-up clamping mechanism includes a cylinder body 8 welded horizontally to the outer wall of the opposite side of the fixed side plate 4, and the cylinder body 8 and the opposite side of the main box body 20 are fixedly connected with an L-shaped communication pipe 6. The L-shaped communication pipe 6 and the inner wall of the main box body 20 are filled with hydraulic oil.

[0035] refer to figure 1 The inner wall of one end of the cylinder body 8 is welded with a return spring 7, and the other end of the return spring 7 is welded with a piston push rod 16.

[0036] refer to figure 1 , the piston push rods 16 are all slidably connected with the inner wall of the corresponding cylinder 8, and the ends of the piston push rods 16 are all fixed with clamping plates 17 by bolts.

[0037] With the above structure, after the satellite main body is put in, under the action of gravity, the piston plate 3 is pressed to the bottom of the main box bo...

Embodiment 3

[0039] refer to figure 1 , figure 2 , Figure 4 , Figure 5 , the surface of the rubber layer is provided with equidistantly distributed inclined plane strips 30, the cross section of the inclined plane strip 30 is an obtuse-angled triangular structure, and the surface of the rubber layer is also provided with a reinforcing vertical strip 31 perpendicular to the inclined plane strip 30, and the reinforcing vertical strip The outer walls of 31 are all provided with semicircular grooves 32 .

[0040] refer to figure 2 , Figure 4 , Figure 5 , the thickness of the reinforcing vertical strip 31 is smaller than the thickness of the inclined surface strip 30, the bottom outer wall of the piston plate 3 is welded with the attachment plate 23, and the cross-section of the attachment plate 23 is composed of a plurality of trapezoidal structures superimposed on each other, and the bottom outer wall of the attachment plate 23 is formed. Both are welded with bottom round blocks 2...

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Abstract

The invention belongs to the technical field of satellite transportation, in particular to a satellite transportation box, which includes a box body, a bottom plate is fixed at an end of the inner wall of the box close to the inner bottom by bolts, and a top cavity cover is connected to the top of the box body through a hinge. The top outer wall of the bottom platform is equipped with a supporting mechanism, and both sides of the top outer wall of the bottom platform are vertically welded with fixed side plates, and the opposite side of the fixed side plate is equipped with a follow-up clamping mechanism. A pressing mechanism is installed on the top chamber cover, and the supporting mechanism includes a main box body fixed to the top outer wall of the bottom platform by bolts. In the present invention, through the follow-up clamping mechanism provided, when the main body of the satellite is put in, the piston plate can be squeezed to the bottom of the main box body under the action of gravity, and then the hydraulic oil in the main box body can be passed through the L-shaped connecting pipe Squeeze into the cylinder, and then use hydraulic pressure to push the piston push rod and the clamping plate to move towards each other until they are closely attached to the surface of the satellite main body.

Description

technical field [0001] The invention relates to the technical field of satellite transportation, in particular to a satellite transportation box. Background technique [0002] Artificial satellites refer to unmanned spacecraft orbiting the earth in space orbits. Artificial satellites basically move around the earth according to the laws of celestial mechanics, but due to the influence of the non-spherical earth's gravitational field, atmospheric resistance, solar gravitational, lunar gravitational and light pressure in different orbits, the actual motion situation is very complicated. Artificial satellites are the most launched, most widely used and fastest-growing spacecraft. The number of satellite launches accounts for more than 90% of the total number of spacecraft launches. Artificial satellites can be divided into three categories: scientific satellites, technical test satellites and application satellites. [0003] The shapes of satellites are cylindrical, spherica...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B65D25/10B65D25/02B65D85/68
CPCB65D25/02B65D25/10B65D85/68
Inventor 朱少静
Owner 烟台海上航天科技有限公司
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