US 12,404,016 B2
Aircraft and power device
Yoichi Suzuki, Shibuya-ku (JP)
Assigned to AERONEXT INC., Tokyo (JP)
Appl. No. 18/004,439
Filed by AERONEXT INC., Shibuya-ku (JP)
PCT Filed Jul. 7, 2020, PCT No. PCT/JP2020/026607
§ 371(c)(1), (2) Date Jan. 5, 2023,
PCT Pub. No. WO2022/009319, PCT Pub. Date Jan. 13, 2022.
Prior Publication US 2024/0025574 A1, Jan. 25, 2024
Int. Cl. B64U 30/299 (2023.01); B64U 10/16 (2023.01); B64U 20/94 (2023.01); B64U 50/19 (2023.01); H02K 7/00 (2006.01); H02K 9/22 (2006.01)
CPC B64U 20/94 (2023.01) [B64U 10/16 (2023.01); B64U 30/299 (2023.01); B64U 50/19 (2023.01); H02K 7/006 (2013.01); H02K 9/227 (2021.01)] 16 Claims
OG exemplary drawing
 
1. An aircraft, comprising:
a power unit having a first space open at least on one of an upper surface or a lower surface of the power unit;
a propeller having a first through-space and connected to the power unit;
a pair of holding parts defined by an arm or a frame of the aircraft and holding the power unit and the propeller on one side of the pair of holding parts; and
a functional part having a predetermined function and including a grounding part that is configured to be in contact with a ground when landed,
wherein
the grounding part is coaxially arranged with the power unit and is located at least in part within an internal space formed by the first space and the first through-space, and
the grounding part has an end protruding from the first space of the power unit and mounted to the one side of the pair of holding parts.