US 12,319,446 B2
Modular flying vehicle
Ryan Joseph Bohm, Logan, UT (US); and Daniel Garrett, Cottage Grove, MN (US)
Filed by Ryan Joseph Bohm, Logan, UT (US); and Daniel Garrett, Cottage Grove, MN (US)
Filed on Oct. 26, 2023, as Appl. No. 18/495,549.
Claims priority of provisional application 63/449,433, filed on Mar. 2, 2023.
Prior Publication US 2024/0294280 A1, Sep. 5, 2024
Int. Cl. B60L 50/60 (2019.01); B64U 10/16 (2023.01); B64U 20/40 (2023.01); B64U 30/29 (2023.01); B64U 50/30 (2023.01); B64U 80/86 (2023.01); B64U 101/61 (2023.01)
CPC B64U 20/40 (2023.01) [B60L 50/60 (2019.02); B64U 10/16 (2023.01); B64U 30/29 (2023.01); B64U 50/30 (2023.01); B64U 80/86 (2023.01); B60L 2200/10 (2013.01); B64U 2101/61 (2023.01)] 13 Claims
OG exemplary drawing
 
1. A flying vehicle comprising:
an upper chassis;
a lower chassis removably mounted to the upper chassis, the lower chassis positioned below the upper chassis;
a plurality of rotors mounted to the upper chassis, wherein the plurality of rotors comprises four upper rotors and four lower rotors, wherein the four lower rotors are mounted below the respective four upper rotors;
a battery pack mounted to the upper chassis;
a control unit mounted to the upper chassis; and
a seat mounted to the lower chassis,
wherein the four upper rotors are connected to a first power supply and the four lower rotors are coupled to a second power supply, the first power supply and the second power supply are different, wherein the first power supply is connected to a first set of batteries of the battery pack and the second power supply is connected to a second set of batteries of the battery pack,
wherein each rotor is removably coupled to the upper chassis.