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A brake cylinder for brake buffering of a solar wing panel suspension device

A suspension device and buffer cylinder technology, which is applied in the field of brake cylinders, can solve problems such as the influence of inertial motion, achieve the effects of low production cost, simple and compact structure, and avoid transfer

Active Publication Date: 2018-01-05
ZHEJIANG UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to solve the problem that the inertial motion of the solar wing will be affected by the forward rush or rebound of the hanging device, and provide a brake cylinder that uses a brake buffer for the hanging device of the solar wing. The special buffer cylinder absorbs the energy of the hanging device, so as to avoid the influence of the inertial motion of the hanging device on the inertial motion of the solar panel itself

Method used

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  • A brake cylinder for brake buffering of a solar wing panel suspension device
  • A brake cylinder for brake buffering of a solar wing panel suspension device

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Embodiment Construction

[0014] The present invention will be further described below in conjunction with accompanying drawing:

[0015] Such as Figure 1~2 As shown, a brake cylinder for braking and buffering the hanging device of the solar wing is used for braking and buffering the hanging device which is erected on the linear track and can move linearly along the linear track. The hanging device is equipped with The absorption iron block includes a buffer cylinder 1, a cylinder fixing seat, an electromagnet 2, a cushion pad 3 and a buffer spring 4. The buffer cylinder 1 is fixed on the cylinder fixing seat, and the cylinder fixing seat is fixed on a linear track. The end of the piston rod is fixed with an electromagnet 2, and the piston rod of the buffer cylinder 1 is also set with a buffer pad 3 and a buffer spring 4. The position of the electromagnet 2 corresponds to the position of the adsorption iron block, and the hanging device When moving to the braking position, the electromagnet 2 is in c...

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Abstract

The invention discloses a brake cylinder for braking and buffering a solar wing board hanging device, comprising a buffer cylinder, a cylinder fixing seat, an electromagnet, a buffer pad and a buffer spring, the buffer cylinder is fixed on the cylinder fixing seat, and the piston of the buffer cylinder A buffer pad and a buffer spring are also set on the rod. An air inlet is provided at the end of the buffer cylinder away from the electromagnet. The air outlet pipe is provided with a one-way pressure regulating valve; the cylinder inner wall of the brake cylinder is provided with a microporous material groove along the radial direction of the cylinder inner wall. The invention can effectively absorb the energy generated by the inertia of the suspension device when braking, and prevent the suspension device from affecting the solar wing due to inertial motion; The air cavity is connected to prevent the piston from rebounding directly under the action of the spring, so that the cushioning effect is better.

Description

technical field [0001] The invention relates to the technical field of a solar wing ground simulation hanging device, and more specifically, relates to a brake cylinder for braking and buffering a solar wing hanging device. Background technique [0002] The solar wing is the energy source of the satellite. The solar panel is a device that collects solar energy. It is usually used to supply energy for satellites and spacecraft, and can also be used to install on the top of environmentally friendly cars. The solar wing is the energy source of the satellite. When the satellite is launched, the solar wing is in a folded state. After the star rocket is separated, it is opened and the direction is constantly adjusted during the flight of the satellite, so that the solar cells are aligned with the sun to provide energy for the entire star. The solar wing monitoring camera can capture the deployment process and working status of the solar wing, and judge whether the solar wing is ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16F13/00F16F9/02F16F9/43
CPCF16F9/0218F16F9/43F16F13/002F16F13/007
Inventor 叶必卿袁智敏陈俊超
Owner ZHEJIANG UNIV OF TECH
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