US 12,420,920 B2
Aerial vehicle such as high speed drone
Yoshiro NakaMats, Tokyo (JP)
Assigned to DR. NAKAMATS INNOVATION INSTITUTE, Tokyo (JP)
Filed by Dr. NakaMats Innovation Institute, Tokyo (JP)
Filed on Sep. 26, 2024, as Appl. No. 18/898,113.
Application 18/898,113 is a continuation of application No. 17/043,899, granted, now 12,129,022, previously published as PCT/JP2019/012261, filed on Mar. 22, 2019.
Claims priority of application No. 2018-070484 (JP), filed on Mar. 31, 2018.
Prior Publication US 2025/0033766 A1, Jan. 30, 2025
Int. Cl. B64C 27/26 (2006.01); B64C 29/00 (2006.01); B64U 10/25 (2023.01); B64U 30/12 (2023.01); B64U 30/299 (2023.01); B64U 50/13 (2023.01); B64U 50/31 (2023.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 70/80 (2023.01)
CPC B64C 27/26 (2013.01) [B64C 29/0025 (2013.01); B64U 10/25 (2023.01); B64U 30/12 (2023.01); B64U 30/299 (2023.01); B64U 50/13 (2023.01); B64U 50/31 (2023.01); B64U 30/20 (2023.01); B64U 50/19 (2023.01); B64U 70/80 (2023.01)] 11 Claims
OG exemplary drawing
 
1. A flying machine comprising:
a main flight wing configured for horizonal flight;
a plurality of propeller guards coupled together to form an integrated single unit and attached to the main flight wing, the plurality of propeller guards being arranged at a center of the flying machine;
a main wing girder attached to and running along a center line of the main flight wing in a lengthwise direction of the main flight wing; and
a plurality of propellers enclosed within the plurality of propeller guards operable for ascending and descending for vertical flight,
wherein the main flight wing includes (i) a left-side main flight wing that extends from a left-side of the plurality of propeller guards and (ii) a right-side main flight wing that extends from a right-side of the plurality of propeller guards,
wherein the main wing girder includes (i) a left-side main wing girder attached to and running along the center line of the left-side main flight wing in the lengthwise direction of the left-side main flight wing and (ii) a right-side main wing girder attached to and running along the center line of the right-side main flight wing in the lengthwise direction of the right-side main flight wing,
wherein the left-side main wing girder is attached to a point at which two adjacent left-side propeller guards from among the plurality of propeller guards are coupled together, and
wherein the right-side main wing girder is attached to a point at which two adjacent right-side propeller guards from among the plurality of propeller guards are coupled together.