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Gravity discharge device for ground-spreading flexible solar wing

A gravity unloading and flexible technology, applied in the field of solar wing ground deployment, can solve the problems of inability to complete the flexible solar wing ground deployment test, reduce thickness, etc., and achieve the effects of increasing rigidity, improving load capacity, and ensuring accuracy and accuracy

Inactive Publication Date: 2016-08-10
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the thickness of the flexible solar wing is relatively thin, and the thickness of the single plate is about 1mm, and the number of folds is large when it is folded in the effective space of the spacecraft. Under the condition of ensuring the structural strength, reduce the thickness to 1mm, and the hanging device exceeds the distance between the solar panels when the flexible solar wing is folded, so the ground deployment test of the flexible solar wing cannot be completed

Method used

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  • Gravity discharge device for ground-spreading flexible solar wing
  • Gravity discharge device for ground-spreading flexible solar wing

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Embodiment Construction

[0014] The present invention will be described in detail below with reference to the drawings and embodiments.

[0015] The present invention provides a gravity unloading device for deploying a flexible solar wing on the ground, such as figure 1 As shown, it includes a first limit roller device 1, a column 2, a beam 3, a roller device 4, a cantilever 5, an adjuster 6, a reinforcing rib 7, a second limit roller device 8 and a suspension rope 10. Among them, the column 2 is divided into upper and lower sections, and the angle between the two sections is an obtuse angle; the first limit roller device 1 is fixedly installed at one end of the column 2, and the cantilever 5 is fixedly installed at the other end of the column 2. And it forms a "Z" shape with the column 2; the cantilever 5 is provided with a through hole on the end surface of the suspended end, the cantilever 5 is provided with an adjuster 6, and the suspension rope 10 passes through the through hole on the end surface of...

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Abstract

The invention discloses a gravity unloading device for a ground-deployed flexible solar wing. Using the present invention can be applied to the extremely small spacing when the solar panels of the flexible solar wing are folded, can realize the gravitational unloading of the flexible solar wing, and can passively follow the movement of the flexible solar wing in the deployment direction of the solar wing, effectively ensuring the accuracy of the ground test precision and accuracy. The present invention includes a first limit roller device, a column, a beam, a roller device, a cantilever, an adjuster, a second limit roller device and a sling, wherein the cantilever is vertically fixedly connected to one end of the column and forms a "Z" shape with the column ;The beam is fixedly connected to the bending part of the column, and through the three roller devices, it can effectively reduce the excessive additional force and additional moment introduced by the unloading tooling. The first limit roller device and the second limit roller device are on the contact surface with the guide rail. There is a limit chute on the top to avoid vibration and shock.

Description

Technical field [0001] The invention relates to the technical field of ground deployment of solar wings, in particular to a gravity unloading device for ground deployment of flexible solar wings. Background technique [0002] With the continuous development of aerospace technology, the application of large-scale solar wings and other deployment mechanisms has become more and more extensive. At present, the domestic ground-based solar wing test device is mainly aimed at the zero-gravity deployment of ordinary solar panels. Each solar panel is connected to a hanging device, and the tension of the hanging device is adjusted to be equal to that of the solar panel connected to it. Gravity, so as to complete the gravity unloading of the solar wing deployed on the ground. As spacecraft's demand for space and energy increases, the application of flexible solar wings has attracted more and more attention in the aerospace field. However, the thickness of the flexible solar wing is relati...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/00
Inventor 宋晓东杨巧龙沈晓鹏于洋任守志王举马静雅闫泽红
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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