Quick-release wing structure and an unmanned aerial vehicle using the same
A quick-release wing structure includes a lock cylinder assembly and a lock head. The lock cylinder assembly is installed in the fuselage. The lock cylinder assembly includes a shell and a lock plate. An installation slot is opened inside the shell. The side wall of the installation slot is provided with a clamping hole connected with the installation slot. The lock plate is sliding and arranged in the installation slot. The lock head is installed in the wing. A locking slot is set on the periphery of the lock head. The lock head can pass through the clamping hole and drive the lock plate to move. When the locking slot is facing the lock plate, the lock head is clamped onto the locking slot and fixed. The UAV includes the quick-release wing structure described above.
1. A quick-release wing structure, comprising:
a lock cylinder assembly ( 1 ) installed in a body ( 100 ), and the lock cylinder assembly ( 1 ) comprises a shell ( 11 ) and a lock plate ( 12 );
the shell ( 11 ) is internally provided with an installation slot ( 10 );
a side wall of the shell is provided with a clamping hole ( 20 ) which is connected with the installation slot ( 10 ), and the lock plate ( 12 ) is set in the installation slot ( 10 ) in a sliding manner;
a lock head ( 2 ) installed in a wing ( 200 );
the lock head ( 2 ) is provided with a locking slot ( 30 ) on a periphery of the lock head;
wherein the lock head ( 2 ) passes through the clamping hole ( 20 ) to drive the lock plate ( 12 ) to move;
a bolt ( 13 ), which slides along the installation slot and is arranged in the installation slot ( 10 );
an elastic part ( 14 ) having two ends;
wherein the lock plate ( 12 ) is fixedly connected to the bolt ( 13 ); and
wherein the shell ( 11 ) further comprises a plurality of sliding holes ( 40 ), each sliding hole provided on two opposite sides of the shell, the sliding holes ( 40 ) are connected with the installation slot ( 10 ), wherein the bolt ( 13 ) has two opposite sides that are respectively provided with clips ( 131 ), and the said clips ( 131 ) are respectively connected with the two sliding holes ( 40 ).
2. The quick-release wing structure of claim 1 , wherein the lock plate ( 12 ) is provided with a locking hole ( 50 ).
3. A unmanned aerial vehicle comprising the quick-release wing structure as recited in claim 2 .
4. The quick-release wing structure of claim 1 , wherein one of said two ends of the elastic part ( 14 ) is embedded in the limit slot ( 70 ).
5. A unmanned aerial vehicle comprising the quick-release wing structure as recited in claim 4 .
6. The quick-release wing structure of claim 1 , wherein an end of the bolt ( 13 ) extends out of the installation slot ( 10 ) and protrudes from the body ( 100 ).
7. A unmanned aerial vehicle comprising the quick-release wing structure as recited in claim 6 .
8. The quick-release wing structure of claim 1 , wherein a front end of the lock head ( 2 ) is cone-shaped.
9. A unmanned aerial vehicle comprising the quick-release wing structure as recited in claim 8 .
10. A unmanned aerial vehicle comprising the quick-release wing structure as recited in claim 1 .