Launch tube restraint system for unmanned aerial vehicle (UAV)
View Patent ↗An unmanned aerial launch vehicle (UAV) launch apparatus is disclosed that includes a UAV ( 400 ) having an exterior surface, an aerial vehicle (AV) tab ( 510 ) extending from the exterior surface, a tube ( 440 ) containing the UAV ( 400 ), the tube ( 440 ) including a tab stop ( 515 ) configured to controllably hinder travel of the AV tab ( 510 ) past the tab stop ( 515 ), and a pair of opposing tab guides ( 700, 705 ) configured to position the AV tab ( 510 ) for travel over the tab stop ( 515 ).
1. An unmanned aerial launch vehicle (UAV) launch apparatus, comprising:
a UAV;
a tube containing the UAV, wherein the tube has an open end;
a cap positioned over the open end of the tube; and
a strap extending through at least one strap guide and restraining the cap;
wherein the strap extends around the entire tube.
2. The apparatus of claim 1 , wherein the strap extends over a top of the cap.
3. The apparatus of claim 1 , wherein the strap extends through at least one strap guide.
4. The apparatus of claim 3 , wherein the at least one strap guide includes at least one of: a top strap guide disposed on the cap and a bottom strap guide disposed distal from the open end of the tube.
5. The apparatus of claim 1 , wherein the strap has a first attachment at a first end of the strap and a second attachment at a second end of the strap, and wherein the first attachment is detachably coupled to the second attachment.
6. The apparatus of claim 5 , wherein the first attachment and the second attachment are buckles.
7. The apparatus of claim 5 , wherein the strap, first attachment, and second attachment have sufficient strength to prevent forceful escape of the UAV through the open end of the tube by holding the cap in place over the open end of the tube.
8. The apparatus of claim 1 , wherein the strap remains connected to the at least one strap guide when the cap is removed from the open end of the tube.
9. The apparatus of claim 8 , wherein the cap remains connected to the tube via the strap when the cap is removed from the open end of the tube.
10. The apparatus of claim 1 , wherein the at least one strap guide includes two guides disposed on either side of the strap.
11. The apparatus of claim 10 , wherein the at least one strap guide includes a top portion disposed between the two guides to hold the strap in place.
12. An apparatus, comprising:
a tube having an open end;
a cap positioned over the open end of the tube; and
a strap extending through a top strap guide and restraining the cap, wherein the cap and strap have sufficient strength to forcibly retain an unmanned aerial vehicle (UAV) within the tube upon application of a launch force;
wherein the strap extends around the entire tube.
13. The apparatus of claim 12 , further comprising:
a bottom strap guide disposed distal from the open end of the tube, wherein the strap extends through the bottom strap guide.
14. The apparatus of claim 12 , wherein the strap has a first attachment at a first end of the strap and a second attachment at a second end of the strap, and wherein the first attachment is detachably coupled to the second attachment.
15. The apparatus of claim 12 , wherein the cap comprises a top strap guide.
16. The apparatus of claim 15 , wherein the strap remains connected to the top strap guide when the cap is removed from the open end of the tube.
17. The apparatus of claim 16 , wherein the cap remains connected to the tube via the strap when the cap is removed from the open end of the tube.
18. The apparatus of claim 15 , wherein the top strap guide includes two guides disposed on either side of the strap.
19. The apparatus of claim 16 , wherein the top strap guide includes a top portion disposed between the two guides to hold the strap in place.
20. A method of launching an unmanned aerial launch vehicle (UAV), comprising:
removing a strap detachably coupled to an exterior of a tube, wherein the strap extends around the entire tube;
removing the cap from an open end of the tube; and
providing an axial launch force to the UAV, wherein the launch force is at least sufficient to enable the UAV to translate axially out of the tube.
21. The method of claim 20 , wherein removing the strap further comprises:
decoupling a first attachment at a first end of the strap from a second attachment at a second end of the strap.
22. The method of claim 20 , further comprising:
removing the strap from a bottom strap guide disposed distal from the open end of the tube.
23. The method of claim 22 , wherein the strap extends through a top strap guide of a cap.