US 12,129,057 B2
UAV structural elements quick release fastening system
Maksym Makarchuk, Uman (UA); Roman Franchuk, Shepetivka (UA); Yevhen Sedochenko, Obukhiv (UA); Yevhenii Doroshenko, Kyiv (UA); Hryhorii Yehoshyn, Kyiv (UA); and Dmytro Vrachynskyi, Kyiv (UA)
Appl. No. 17/925,621
Filed by Maksym Makarchuk, Uman (UA); Roman Franchuk, Shepetivka (UA); Yevhen Sedochenko, Obukhiv (UA); Yevhenii Doroshenko, Kyiv (UA); Hryhorii Yehoshyn, Kyiv (UA); and Dmytro Vrachynskyi, Kyiv (UA)
PCT Filed Mar. 25, 2021, PCT No. PCT/UA2021/000027
§ 371(c)(1), (2) Date Nov. 16, 2022,
PCT Pub. No. WO2021/236047, PCT Pub. Date Nov. 25, 2021.
Claims priority of application No. u 2020 03090 (UA), filed on May 22, 2020.
Prior Publication US 2023/0166828 A1, Jun. 1, 2023
Int. Cl. B64U 20/70 (2023.01); B64U 10/25 (2023.01); B64U 20/40 (2023.01); F16B 21/04 (2006.01); B64U 20/80 (2023.01)
CPC B64U 20/70 (2023.01) [B64U 10/25 (2023.01); B64U 20/40 (2023.01); F16B 21/04 (2013.01); B64U 20/80 (2023.01)] 2 Claims
OG exemplary drawing
 
1. An unmanned serial vehicle (UAV) comprising:
a tail assembly comprising:
a tail assembly docking chuck; and
a male part of a bayonet mount;
a fuselage and a wing, wherein at least one of the fuselage and the wing comprises:
a center wing section docking chuck; and
a center wing section fixing pin; and
at least two tail booms; wherein each of the at least two tail booms comprise:
a female part of the bayonet mount configured to mate with the male part of the bayonet mount; and
an electrical wire bundle;
wherein the male part of the bayonet mount comprises a tail assembly fixing pin, wherein the female part of the bayonet mount comprises an L-shaped cutout; and
wherein the tail assembly further comprises a first UAV wiring bundles connector, wherein the at least one of the fuselage and the wing further comprises a second UAV wiring bundles connector, wherein the electrical wire bundle comprises a third UAV winging bundle connector configured to mate with each of the first UAV wiring bundles connector and the second UAV wiring bundles connector in order to provide electrical connection; and
wherein the tail assembly further comprises a horizontal stabilizer, wherein the horizontal stabilizer comprises two horizontal stabilizer halves, wherein each of the two horizontal stablilzer halves comprises a docking chuck, wherein the electrical wire bundle further comprises a docking plate, wherein the docking plate is configured to mate with the docking chuck;
wherein electrical wire bundle further comprises a quick release fastener.