Aircraft wing folding and unfolding mechanism
The invention provides an aircraft wing folding and unfolding mechanism which comprises a machine shell and two wings and further comprises a turnover mechanism, a release assembly and two wing unfolding mechanisms, and the two wings are both arranged on the machine shell and folded to the two sides...
Gespeichert in:
| Hauptverfasser: | , , , , , |
|---|---|
| Format: | Patent |
| Sprache: | chi ; eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| Zusammenfassung: | The invention provides an aircraft wing folding and unfolding mechanism which comprises a machine shell and two wings and further comprises a turnover mechanism, a release assembly and two wing unfolding mechanisms, and the two wings are both arranged on the machine shell and folded to the two sides of the machine shell respectively; the turnover mechanism is arranged in the machine shell and comprises a rotating shaft, the two ends of the rotating shaft extend to the outside of the machine shell, and the rotating shaft tends to rotate around the axis of the rotating shaft. The release assembly is arranged in the machine shell and selectively fixes the rotating shaft. The two wing unfolding mechanisms are fixed to the two ends of the rotating shaft correspondingly and located on the outer side of the machine shell, and the two wing unfolding mechanisms are fixed to the two wings correspondingly and used for pushing the wings to be unfolded on the outer side of the machine shell. According to the aircraft wing |
|---|