Integrated shock absorbing vibrating isolation device for stellite
Patent Information
- Authority / Receiving Office
- CN ยท China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- ้้ข้
- Publication Date
- 2007-02-14
- Estimated Expiration
- Not applicable ยท inactive patent
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Abstract
Description
technical field
[0001] The invention relates to a vibration damping and isolating device. Background technique
[0002] The dynamic environment in which a satellite is launched is the harshest. Therefore, ensuring that the satellite can not be damaged in the dynamic environment of the launch process is the main research direction of the current satellite structural strength design. Usually, the strength of the satellite itself is improved, but the quality of the spacecraft is increased, which increases the launch cost, and the increased quality is useless in the normal operation of the spacecraft in orbit. The satellite adapter is the connection part between the satellite and the launch vehicle. The existing satellite adapter is a section of conical shell structure with bolt holes at both ends to connect with the satellite connection interface and the vehicle connection interface respectively. The overall satellite vibration reduction and isolation device is a modification...