Folding beam structure-based multi-degree of freedom passive vibration isolation device for spacecraft flywheel
A technology for a spacecraft and a folding beam, which is applied in the field of multi-degree-of-freedom passive vibration isolation devices for spacecraft flywheels, can solve problems such as output disturbance force, and achieve the effects of small additional impact, easy implementation, and low quality.
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[0032] The accompanying drawings constituting a part of this application are used to provide further understanding of the present invention, and the schematic embodiments and descriptions of the present invention are used to explain the present invention, and do not constitute an improper limitation of the present invention.
[0033] see figure 1 The multi-degree-of-freedom passive vibration isolation device for a spacecraft flywheel based on a folded beam structure provided by the present invention is arranged between the spacecraft flywheel 100 and the spacecraft cabin. The flywheel is installed on the vibration isolation device, and the vibration isolation device is connected with the spacecraft cabin, so that the disturbance force generated by the flywheel during high-speed rotation will not be directly transmitted to the spacecraft. Therefore, the interference effect of the disturbance on other devices on the spacecraft during the use of the flywheel is reduced. Improved...
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