|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-039/02 B64D-047/08 H05K-007/14|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 87|
Disclosed herein are unmanned aerial vehicles (UAVs). Some UAVs include a vertically-mounted printed circuit board (PCB). The UAVs have yaw, pitch, and roll axes. The UAVs comprise a plurality of propellers, each of the plurality of propellers configured to rotate about a respective one of a plurality of axes of rotation; a base assembly coupled to each of the plurality of propellers; and a PCB coupled to the base assembly. A surface of the PCB lies in a plane defined by the yaw axis and the roll axis, and no portion of the PCB intersects any axis of rot...
1. An unmanned aerial vehicle having a yaw axis, a pitch axis, and a roll axis, the unmanned aerial vehicle comprising: a plurality of propeller assemblies, each of the plurality of propeller assemblies configured to rotate about a respective one of a plurality of axes of rotation;a base assembly coupled to each of the plurality of propeller assemblies; anda vertically-mounted printed circuit board coupled to the base assembly, the vertically-mounted printed circuit board comprising a populated surface and an edge substantially perpendicular to the popul...