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Satellite-borne load linear motion system

A linear motion, space-borne technology, applied in the direction of motor vehicles, artificial satellites, electric components, etc., can solve the problems of short service life, the drive mechanism cannot meet the use requirements, and cannot meet the long-distance and long-term reciprocating linear motion, etc., to achieve The effect of improving stability and reliability

Active Publication Date: 2020-08-07
SHANGHAI SPACEFLIGHT INST OF TT&C & TELECOMM
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

With the continuous increase of the load system, the required drive mechanism is also getting larger and larger, and the existing drive mechanism cannot meet the use requirements. In order to better cooperate with the satellite load system, it is urgent to break through the inherent mode of the drive mechanism and study a Applicable to space-borne linear motion system
[0003] Existing space-borne linear motion systems are generally small in size, one-time expansion or closing motion, short service life, unable to meet long-distance and long-term reciprocating linear motion, and unable to meet the use requirements of complex load systems

Method used

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  • Satellite-borne load linear motion system
  • Satellite-borne load linear motion system
  • Satellite-borne load linear motion system

Examples

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Embodiment 1

[0035] A starborne load linear motion system, including a load assembly 2 and a linear track 1 fixed on a star body 100; the linear track 1 is a foldable structure, and the load assembly 2 includes a moving mechanism 3, a driving mechanism 4, and a load carrying a corresponding load The mechanism 5 and the moving mechanism 3 are assembled on the linear track 1, and the linear track 1 provides a force for the moving mechanism 3 to limit its detachment from the linear track 1, so that the moving mechanism 3 can move on the linear track 1 under the drive of the driving mechanism 4 , in order to realize the high-precision, long-distance and long-distance reciprocating motion of the load in the foldable track.

[0036] After the satellite is launched and flies away from the earth, the star is in a state of weightlessness, so the drive and linear motion system suitable for the ground are not suitable for spaceborne. The linear track 1 provides the moving mechanism 3 with a force tha...

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Abstract

The invention discloses a satellite-borne load linear motion system which comprises a load assembly and a linear track fixed on a satellite body. The linear rail is a foldable rail; the load assemblycomprises a moving mechanism, a driving mechanism and a load mechanism for bearing a corresponding load; the moving mechanism is assembled on the linear rail, the linear rail provides acting force forlimiting the moving mechanism to be separated from the linear rail, the moving mechanism can be driven by the driving mechanism to move on the linear rail, and therefore the load can complete high-precision long-time reciprocating motion in the foldable rail. By means of the foldable structure, the distance of the linear orbit can be longer after the linear orbit is unfolded, the satellite load envelope requirement can be met, and meanwhile the long-distance reciprocating linear motion of the load can be met; the moving mechanism can move on the linear rail all the time and cannot be separated from the linear rail to fail in the weightless state, and therefore the load linear motion system can still normally move in the weightless state.

Description

technical field [0001] The invention relates to the technical field of linear drive mechanisms, in particular to a linear motion system suitable for spaceborne applications. Background technique [0002] With the continuous development of aerospace technology, in order to obtain better electrical performance of satellite payloads, the payload system is becoming more and more complex, and the requirements are getting higher and higher, and the space occupied by the payload is getting larger and larger. With the continuous increase of the load system, the required drive mechanism is also getting larger and larger, and the existing drive mechanism cannot meet the use requirements. In order to better cooperate with the satellite load system, it is urgent to break through the inherent mode of the drive mechanism and study a Applicable to space-borne linear motion systems. [0003] Existing space-borne linear motion systems are generally small in size, one-time unfolding or closi...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10B64G1/22H02K7/06
CPCB64G1/10B64G1/22H02K7/06Y02E10/50
Inventor 李宁杰刘瑞冯剑锋何子慧翁艺航栾英宏赵锋孙彦龙李丹熊一帆
Owner SHANGHAI SPACEFLIGHT INST OF TT&C & TELECOMM
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