US 12,378,015 B2
Flight device with end parts displaceable along front end parts of wing parts
Yoichi Suzuki, Tokyo (JP)
Assigned to AERONEXT INC., Tokyo (JP)
Appl. No. 18/550,257
Filed by AERONEXT INC., Tokyo (JP)
PCT Filed Mar. 17, 2021, PCT No. PCT/JP2021/010734
§ 371(c)(1), (2) Date Sep. 12, 2023,
PCT Pub. No. WO2022/195747, PCT Pub. Date Sep. 22, 2022.
Prior Publication US 2024/0208643 A1, Jun. 27, 2024
Int. Cl. B64U 30/12 (2023.01); B64C 3/40 (2006.01); B64C 29/02 (2006.01); B64D 9/00 (2006.01); B64U 10/20 (2023.01); B64U 50/13 (2023.01); B64U 101/31 (2023.01); B64U 101/55 (2023.01); B64U 101/60 (2023.01)
CPC B64U 30/12 (2023.01) [B64C 3/40 (2013.01); B64C 29/02 (2013.01); B64D 9/00 (2013.01); B64U 10/20 (2023.01); B64U 50/13 (2023.01); B64U 2101/31 (2023.01); B64U 2101/55 (2023.01); B64U 2101/60 (2023.01)] 4 Claims
OG exemplary drawing
 
1. A flight vehicle, comprising:
a main body part;
end parts connected to the main body part;
a propulsion part on each of the end parts;
a connection part connecting the main body part and the end parts; and
a wing part on the main body part, the wing part comprising wing parts, each wing part comprising a front end part sloping backwardly,
wherein
the connection part is configured to displace the end parts, in a predetermined range, from the front end parts while the end parts remain connected to the main body part, the end parts displaceable along the front end parts starting from the connection part,
the connection part configured to pivot each of the end parts from a first state to a second state.