US 12,286,250 B2
Flying vehicle
Yoichi Suzuki, Shibuya-ku (JP)
Assigned to AERONEXT INC., Shibuya-ku (JP)
Appl. No. 18/042,446
Filed by AERONEXT INC., Shibuya-ku (JP)
PCT Filed Sep. 7, 2020, PCT No. PCT/JP2020/033761
§ 371(c)(1), (2) Date Feb. 21, 2023,
PCT Pub. No. WO2022/049764, PCT Pub. Date Mar. 10, 2022.
Prior Publication US 2023/0331407 A1, Oct. 19, 2023
Int. Cl. B64U 10/20 (2023.01); B64C 3/42 (2006.01); B64C 27/26 (2006.01); B64C 29/00 (2006.01); B64C 39/02 (2023.01); B64D 45/04 (2006.01); B64U 50/13 (2023.01)
CPC B64U 10/20 (2023.01) [B64C 3/42 (2013.01); B64C 27/26 (2013.01); B64C 29/0033 (2013.01); B64C 39/02 (2013.01); B64D 45/04 (2013.01); B64U 50/13 (2023.01)] 5 Claims
OG exemplary drawing
 
1. A flying vehicle, comprising:
a flying part including a plurality of rotary wing parts and a main body part, each of the rotary wing parts including a motor and a rotary wing;
a main wing connected to the flying part; and
wherein the main wing is configured so that a lift generated by the main wing during landing is reduced compared to the lift generated by the main wing during cruise,
wherein the main wing is connected to the flying part via a rotary shaft,
wherein the main wing is configured to tilt forward about the rotary shaft at an angle relative to the flying part when landing more than when cruising,
wherein the main wing is further connected to the flying part via a support member and a spring,
wherein the spring is configured to cause the main wing to tilt forward about the rotary shaft at an angle relative to the flying part when landing more than when cruising, by releasing the support member.