SYSTEM FOR DETACHABLY COUPLING AN UNMANNED AERIAL VEHICLE WITHIN A LAUNCH TUBE
First Claim
Patent Images
1. An unmanned aerial vehicle (UAV) launch tube apparatus, comprising:
- at least one layer of prepeg substrate disposed about an aperture to form a tube;
a sabot disposed in an interior of said tube, said sabot having a first clasp tab; and
a clasp detachably coupled to said first clasp tab and contacting an inner circumferential wall of said tube;
wherein said clasp is rotationally constrained by said inner circumferential wall and said first clasp tab.
2 Assignments
0 Petitions
Accused Products
Abstract
An unmanned aerial vehicle launch tube that has at least one layer of prepeg substrate disposed about an aperture to form a tube, a sabot disposed in an interior of said tube, said sabot having a first clasp tab, and a clasp detachably coupled to said first clasp tab and contacting an inner circumferential wall of said tube so that said clasp is rotationally constrained by the inner circumferential wall and said first clasp tab.
-
Citations
34 Claims
-
1. An unmanned aerial vehicle (UAV) launch tube apparatus, comprising:
-
at least one layer of prepeg substrate disposed about an aperture to form a tube; a sabot disposed in an interior of said tube, said sabot having a first clasp tab; and a clasp detachably coupled to said first clasp tab and contacting an inner circumferential wall of said tube; wherein said clasp is rotationally constrained by said inner circumferential wall and said first clasp tab. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
-
-
12. A method of launching an unmanned aerial vehicle (UAV) launch, comprising:
-
generating gas in a gas generator; introducing said generated gas to a high-pressure volume between an expandable sabot skirt of a sabot and said gas generator to break an adhesive coupling that restrains said sabot in a launch tube; pushing said expandable sabot skirt against an inner circumferential wall of said launch tube using said generated gas; and driving said sabot up said launch tube using said generated gas. - View Dependent Claims (13, 14, 15, 16)
-
-
17. A method of launching an unmanned aerial vehicle (UAV) launch, comprising:
-
restraining a sabot in a launch tube; introducing gas to a high-pressure side of an expandable sabot skirt of a sabot to break said restraint of said sabot in said launch tube; and driving said sabot up said launch tube using said gas. - View Dependent Claims (18, 19, 20, 21, 22, 23, 24)
-
-
25. An unmanned aerial vehicle (UAV) launch tube apparatus, comprising:
-
a first aperture portion, wherein said first aperture portion comprises a constant cross-sectional area; a second aperture portion, wherein said second aperture portion comprises an enlarged cross-sectional area relative to said first aperture portion, and wherein said first aperture portion and said second aperture portion form a launch tube; a sabot disposed in said first aperture portion and configured to detachably couple to a UAV; wherein said sabot is configured to decouple from said UAV upon movement of said sabot from said first aperture portion to said second aperture portion. - View Dependent Claims (26, 27, 28, 29, 30, 31, 32, 33, 34)
-
Specification