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1. WO2018128287 - UNMANNED AERIAL VEHICLE KIT AND SYSTEM

Publication Number WO/2018/128287
Publication Date 12.07.2018
International Application No. PCT/KR2017/014415
International Filing Date 08.12.2017
IPC
B64C 39/02 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
B64C 27/08 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
08with two or more rotors
B64C 27/12 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
12Rotor drives
CPC
B64C 2201/024
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
02characterized by type of aircraft
024Helicopters, or autogiros
B64C 2201/042
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
04characterised by type of power plant
042by electric motors; Electric power sources therefor, e.g. fuel cells, solar panels or batteries
B64C 2201/108
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
10characterised by the lift producing means
108using rotors, or propellers
B64C 2201/12
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
12adapted for particular use
B64C 2201/165
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
16characterised by type of propulsion unit
165using unducted propellers
B64C 2211/00
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2211Modular constructions of airplanes or helicopters
Applicants
  • 삼성전자 주식회사 SAMSUNG ELECTRONICS CO., LTD. [KR]/[KR]
Inventors
  • 윤영규 YOON, Yeonggyu
  • 이민성 LEE, Minsung
  • 유민우 YOO, Minwoo
  • 최종철 CHOI, Jongchul
Agents
  • 윤앤리특허법인(유한) YOON & LEE INTERNATIONAL PATENT & LAW FIRM
Priority Data
10-2017-000080603.01.2017KR
Publication Language Korean (KO)
Filing Language Korean (KO)
Designated States
Title
(EN) UNMANNED AERIAL VEHICLE KIT AND SYSTEM
(FR) KIT ET SYSTÈME POUR VÉHICULE AÉRIEN SANS PILOTE
(KO) 무인 비행 장치 키트 및 시스템
Abstract
(EN)
An unmanned aerial vehicle kit and a system according to various embodiments of the present invention comprise a first assembly and a second assembly. The first assembly comprises: a housing comprising a processor and a navigation system; at least one first propeller which is connected to or mounted on the housing, and which has a direction set such that the same rotates about a first axis extending in a first direction; at least one first motor which drives the at least one first propeller, and which is configured to be controlled by at least one of the processor and the navigation system; and at least one first electric contact electrically connected to the processor. The second assembly comprises: a frame that can be connected to the first assembly in an attachable/detachable manner; at least one second electric contact that can be electrically connected to the at least one first electric contact when the frame is connected to the first assembly; at least one second propeller which is connected to or mounted on the frame, and which has a direction set such that the same rotates about a second axis that is different from the first axis; and at least one second motor which drives the at least one second propeller, and which is configured to be controlled by at least one of the processor and the navigation system. At least one of the processor and the navigation system is configured to selectively drive the first motor or the second motor according to whether the second assembly has been connected to the first assembly or not, and the first assembly can accordingly transfer a control signal corresponding to the type of the second assembly to the second assembly. Various embodiments other than the embodiments disclosed in the present specification are also possible.
(FR)
Un kit de véhicule aérien sans pilote et un système selon divers modes de réalisation de la présente invention comprennent un premier ensemble et un deuxième ensemble. Le premier ensemble comprend : un boîtier comprenant un processeur et un système de navigation ; au moins une première hélice qui est reliée au boîtier ou montée sur celui-ci et qui a une direction définie de telle sorte que celle-ci tourne autour d'un premier axe s'étendant dans une première direction ; au moins un premier moteur qui entraîne l'au moins une première hélice et qui est configuré pour être commandé par au moins l'un parmi le processeur et le système de navigation ; et au moins un premier contact électrique relié électriquement au processeur. Le deuxième ensemble comprend : un cadre qui peut être relié au premier ensemble d'une manière amovible ; au moins un deuxième contact électrique qui peut être relié électriquement à l'au moins un premier contact électrique lorsque le cadre est relié au premier ensemble ; au moins une deuxième hélice qui est reliée au cadre ou montée sur celui-ci et qui a une direction définie de telle sorte que celle-ci tourne autour d'un deuxième axe qui est différent du premier axe ; et au moins un deuxième moteur qui entraîne l'au moins une deuxième hélice et qui est configuré pour être commandé par au moins l'un parmi le processeur et le système de navigation. Au moins l'un parmi le processeur et le système de navigation est configuré pour entraîner sélectivement le premier moteur ou le deuxième moteur selon que le deuxième ensemble a été connecté ou non au premier ensemble, et le premier ensemble peut en conséquence transférer au deuxième ensemble un signal de commande correspondant au type du deuxième ensemble. Divers modes de réalisation autres que les modes de réalisation décrits ici sont également possibles.
(KO)
본 발명의 다양한 실시예에 따른 무인 비행 장치 키트 및 시스템은, 제 1 어셈블리(assembly)로서, 프로세서 및 내비게이션 시스템을 포함하는 하우징; 상기 하우징에 연결되거나 장착되며, 제 1 방향으로 연장된 제 1 축을 중심으로 회전하도록 방향이 설정된 적어도 하나의 제 1 프로펠러; 상기 적어도 하나의 제 1 프로펠러를 구동하며, 상기 프로세서 또는 내비게이션 시스템 중의 적어도 하나에 의해 제어되도록 구성된 적어도 하나의 제 1 모터; 및 상기 프로세서에 전기적으로 연결된 적어도 하나의 제 1 전기 컨택트를 포함하는 제 1 어셈블리; 및, 상기 제 1 어셈블리에 탈착 가능하게 연결가능한 프레임; 상기 프레임이 상기 제 1 어셈블리에 연결될 때 상기 적어도 하나의 제 1 전기 컨택트에 전기적으로 연결가능한 적어도 하나의 제 2 전기 컨택트; 상기 프레임에 연결되거나 장착되며, 상기 제 1 축과 상이한 제 2 축을 중심으로 회전하도록 방향이 설정된 적어도 하나의 제 2 프로펠러; 및 상기 적어도 하나의 제 2 프로펠러를 구동하며, 상기 프로세서 또는 내비게이션 시스템 중의 적어도 하나에 의해 제어되도록 구성된 적어도 하나의 제 2 모터를 포함하는 제 2 어셈블리를 포함하되, 상기 프로세서 또는 내비게이션 시스템 중의 적어도 하나는, 상기 제 2 어셈블리가 상기 제 1 어셈블리에 연결되었는지의 여부에 따라, 상기 제 1 모터 또는 상기 제 2 모터를 선택적으로 구동하도록 구성되어, 제 1 어셈블리가 상기 제 2 어셈블리의 종류에 대응하는 제어 신호를 제 2 어셈블리에 전달할 수 있다. 본 명세서에 개시된 실시예들 이외의 다양한 실시예가 가능하다.
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