UNMANNED AERIAL VEHICLE, CHARGING SYSTEM OF THE SAME AND METHOD OF CHARGING THE SAME

An unmanned aerial vehicle comprises a central body, a plurality of driving units, a plurality of arms, and first and second landing members. The central body comprises a top surface, a bottom surface, and an inner space which is defined by a plurality of support shafts connecting the top surface an...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	CHO, YEON JE, KIM, JOUNG HO
Format:	Patent
Sprache:	eng ; kor
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PARACHUTES PERFORMING OPERATIONS SYSTEMS FOR STORING ELECTRIC ENERGY TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	An unmanned aerial vehicle comprises a central body, a plurality of driving units, a plurality of arms, and first and second landing members. The central body comprises a top surface, a bottom surface, and an inner space which is defined by a plurality of support shafts connecting the top surface and the bottom surface each other. The plurality of driving units generates thrust for aviation. The one end of the plurality of arms is connected to the central body and the other end thereof is connected to one among the plurality of driving units. The first and second landing members are connected to a bottom surface of the central body, are installed to face each other, and support the central body so that the unmanned aerial vehicle can be landed to a certain height apart from the ground. Circular receiving coils are installed above the plurality of arms not to be overlapped with the central body and charge a rechargeable battery installed in the inner space. 무인 비행체는 중앙의 몸체부, 복수의 구동부들, 복수의 암들 및 제1 및 제2 착지부재를 포함한다. 상기 중앙의 몸체부는 상면, 하면 및 상기 상면과 상기 하면을 서로 연결하는 복수의 지지축들에 의하여 정의되는 내부 공간을 구비한다. 상기 복수의 구동부들은 비행을 위한 추력을 발생시킨다. 상기 복수의 암들은 일단은 상기 몸체부에 연결되고, 타단에는 상기 구동부들 중 하나가 장착된다. 상기 제1 및 제2 착지 부재들은 상기 몸체부의 하면에 연결되고, 상기 무인 비행체가 지면에서 일정 높이로 이격되어 착지하도록 상기 몸체부를 지지하며 서로 대향하도록 설치된다. 상기 복수의 암들 상부에는 상기 몸체부와 중첩되지 않도록 환형의 수신 코일들이 설치되어 상기 내부 공간에 설치되는 재충전가능 배터리를 충전한다.