Captive balloon main node posture adjusting mechanism
Captive balloon main node posture adjusting mechanism
- Neue Suche nach: QIAO TAO
- Neue Suche nach: ZHANG TAIHUA
- Neue Suche nach: FU QIANG
- Neue Suche nach: QIN YUMEI
- Neue Suche nach: WANG ZIHAO
- Neue Suche nach: QIAO TAO
- Neue Suche nach: ZHANG TAIHUA
- Neue Suche nach: FU QIANG
- Neue Suche nach: QIN YUMEI
- Neue Suche nach: WANG ZIHAO
The invention provides a captive balloon main node posture adjusting mechanism which comprises at least two mooring rope length adjusting device groups, at least two pitch angle indicating devices corresponding to the at least two mooring rope length adjusting device groups, a centralized node device and a photoelectric slip ring connecting piece, each mooring rope length adjusting device group comprises at least four mooring rope length adjusting structures of the same structure, and the mooring rope length adjusting structures are used for adjusting the length of four-in-one mooring ropes onthe two sides of a captive balloon. The pitch angle indicating devices are used for indicating pitch angles in the posture adjusting process; the concentrated node device is used for concentrating the pitch angle indicating device at one point to be stressed, can achieve the deflection freedom degree of the two sides of the pitch angle indicating device, and can adapt to deflection of the captiveballoon during air parking. The length of the tying rope can be rapidly and accurately adjusted.
本发明提供了一种系留气球主节点调姿机构，包括：至少两个系缆长度调节装置组、与至少两个系缆长度调节装置组对应的至少两个俯仰角度指示装置、集中节点装置和光电滑环连接件，每个系缆长度调节装置组包括至少四个结构相同的系缆长度调节结构，系缆长度调节结构用于对系留气球的两侧4合1的系索的长度进行调节；俯仰角度指示装置用于调节姿态过程中的俯仰角指示；集中节点装置用于将俯仰角度指示装置集中于一点受力，且可实现俯仰角度指示装置的两侧偏摆自由度，可适应驻空时系留气球偏摆。本发明能够实现系索长度的快速准确调节。
Dokumentinformationen
Captive balloon main node posture adjusting mechanism
一种系留气球主节点调姿机构
2020-10-16
Patent
Elektronische Ressource
Chinesisch
| IPC: | B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft |
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