Abstract An unmanned aerial vehicle (UAV) launch tube (100) that has at least one layer of prepeg substrate disposed about an aperture (106) to form a tube, a sabot (110) disposed in an interior of said tube (100), said sabot (110) having a first clasp tab (126), and a clasp (124) detachably coupled to said first clasp tab and contacting an inner circumferential wall (102) of said tube (100) so that said clasp (124) is rotationally constrained by the inner circumferential wall (102) and said first clasp tab (126). 120 -1.22 0e130 124 -126 140 ----- 128 -114 102 2010220 ---- 136 FIG. 2 FIG. 3
System for detachably coupling an unmanned aerial vehicle within a launch tube
2017-06-15
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
SYSTEM FOR DETACHABLY COUPLING UNMANNED AERIAL VEHICLE WITHIN LAUNCH TUBE
Europäisches Patentamt | 2019
|SYSTEM FOR DETACHABLY COUPLING UNMANNED AERIAL VEHICLE WITHIN LAUNCH TUBE
Europäisches Patentamt | 2020
|SYSTEM FOR DETACHABLY COUPLING UNMANNED AERIAL VEHICLE WITHIN LAUNCH TUBE
Europäisches Patentamt | 2018
|SYSTEM FOR DETACHABLY COUPLING AN UNMANNED AERIAL VEHICLE WITHIN A LAUNCH TUBE
Europäisches Patentamt | 2022
|System for detachably coupling an unmanned aerial vehicle within a launch tube
Europäisches Patentamt | 2018
|