Brake buffering device of suspending device of solar wing plates

Abstract

The invention discloses a brake buffering device of a suspending device of solar wing plates. The brake buffering device is used for buffering braking of the suspending device which is erected on a linear rail and does linear motion along the linear rail, and the suspending device is provided with an attraction iron block. The brake buffering device comprises a double-output rod air cylinder, an air cylinder fixing base, an electromagnet, a buffering pad and a buffering spring, wherein an air inlet of the double-output rod air cylinder is connected to an air inlet pipeline, an air outlet of the double-output rod air cylinder is connected to an air outlet pipeline, the air inlet pipeline is provided with a first throttling valve, and the air outlet pipeline is provided with a second throttling valve. The brake buffering device can effectively absorb the energy generated by inertia in the braking process of the suspending device, and the phenomenon that the suspending device influences the solar wing plates due to inertial motion can be prevented; and inner walls, located on two sides of a piston rod of the double-output rod air cylinder, of a cylinder barrel can communicate with each other, a pipeline used for communicating the two inner walls is provided with two throttling valves, gas is prevented from being transferred too fast, and therefore the buffering effect is better.

Description

technical field [0001] The invention relates to the technical field of a solar wing ground simulation suspension device, and more specifically, relates to a brake buffer cylinder used for a solar wing panel suspension 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 i...

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 buffer cylinder for the hanging device of the solar wing. The device 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

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