|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-027/82 G05D-001/00 B64C-039/02 B64F-001/04 B64F-001/06 B64C-029/00 B64C-029/02|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 21|
An improved unmanned aerial vehicular system having a rotor head assembly with any balanced number of rotary wings or blades, a generally tubular body assembly, a gimballed neck connecting the head to the body, and a navigation, communications and control unit such as for military and humanitarian operations, including payload delivery and pickup. The vehicle is generally guided using a global positioning satellite signal, and by pre-programmed or real time targeting. The vehicle is generally electrically powered and may be launched by one of (a) hand-la...
1. An improved unmanned vehicular system for airborne deployment, which comprises: (a) a vehicle fuselage having a top aspect, a lower aspect, and a center of mass, wherein said vehicle fuselage is aerodynamic in shape, having an elongate and generally tubular vehicle body assembly with a center Z-axis, such that said center of mass is partitioned to a lower half of said Z-axis thereof;(b) a dual rotor head having an apical aspect and an inferior aspect, said rotor head comprising an apical rotor assembly and an inferior rotor assembly, wherein said two ...