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A Vibration Absorbing Bracket for Flywheel Tuning Liquid Damper

A technology for tuning liquid damping and flywheels, applied in liquid shock absorbers and other directions, can solve problems such as affecting the accuracy of load imaging, and achieve the effects of light weight, rapid vibration attenuation, and simple structure

Active Publication Date: 2017-11-10
SHANGHAI XINYUE METER FACTORY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

During the process of sensitive payload imaging, satellite attitude changes affect the accuracy of payload imaging. The existing technology is still unable to guarantee the normal operation of some high-precision and high-stability devices on the satellite. Therefore, the vibration reduction is carried out for the high-frequency micro-vibration of the typical actuators of the satellite. technology research

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  • A Vibration Absorbing Bracket for Flywheel Tuning Liquid Damper
  • A Vibration Absorbing Bracket for Flywheel Tuning Liquid Damper
  • A Vibration Absorbing Bracket for Flywheel Tuning Liquid Damper

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Embodiment Construction

[0018] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0019] Such as Figure 1-7 As shown, the embodiment of the present invention provides a damping support for a flywheel tuning liquid damper, comprising an upper arched door part 1, the lower end of the upper arched door part 1 is threaded with a cylindrical base 3, and the cylindrical base 3 is provided with The liquid-filled chamber 2 is provided with a liquid-filled hole 4 at the upper end of the liquid-filled chamber 2, and a nut 5 with a sealing ring is arranged on the liquid-filled hole, and ...

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Abstract

The invention discloses a damping bracket for a flywheel tuning liquid damper. The damping bracket comprises an upwards-arched door part, wherein the lower end of the upwards-arched door part is in threaded connection with a cylindrical base, a liquid filled cavity is formed in the cylindrical base, a liquid filling hole is formed in the upper end of the liquid filled cavity and is provided with a screw cap with a sealing ring, and the liquid filled cavity is filled with internal-filled liquid. According to the damping bracket for the flywheel tuning liquid damper, the flywheel damping bracket for the tuning liquid damper is applied to a spacecraft domestically for the first time; due to simple structure and integrated design, high-precision machining process flows are not required; due to light weight, a high-frequency micro-vibrating part of a flywheel is effectively damped in case of guaranteeing effective rigidity; high-frequency micro-vibration part of the flywheel is subjected to effective attenuation; by using a liquid sloshing phenomenon, high-frequency micro-vibration of the flywheel is subjected to energy attenuation. The damping bracket is safe and effective and can achieve the rapid attenuation of vibration resulting from the rotation of the flywheel.

Description

technical field [0001] The invention relates to a vibration-damping support, in particular to a vibration-damping support for a flywheel tuning liquid damper. Background technique [0002] With the development of high-resolution satellites, improving the resolution of high-resolution satellites is the future direction of satellite system design and development. In order to make the spacecraft and the precision equipment it carries require a mechanical environment in the sense of ultra-static, to ensure the measurement accuracy of the instrument. Therefore, it is necessary to isolate, damp and suppress the high-frequency micro-vibration generated during the working process of the typical actuators of the spacecraft. During the process of sensitive payload imaging, satellite attitude changes affect the accuracy of payload imaging. The existing technology is still unable to guarantee the normal operation of some high-precision and high-stability devices on the satellite. There...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16F9/10
Inventor 孙宏丽李结冻张少伟贺亮阳光
Owner SHANGHAI XINYUE METER FACTORY