A platform for research: civil engineering, architecture and urbanism
A platform for research: civil engineering, architecture and urbanism
A drone takeoff and landing system according to an embodiment comprises: a drone including a through-hole; and a landing pad including an extension member which can pass through the through-hole, wherein, when the extension member of the landing pad passes through the through-hole of the drone, an eddy current may occur between the through-hole and the extension member to cause magnetic braking of the drone.
La présente invention concerne, selon un mode de réalisation, un système de décollage et d'atterrissage de drone comprenant : un drone doté d'un orifice traversant ; et une plateforme d'atterrissage comprenant un élément d'extension qui peut passer à travers ledit orifice traversant. Lorsque l'élément d'extension de la plateforme d'atterrissage passe à travers l'orifice traversant du drone, un courant de Foucault peut se produire entre l'orifice traversant et l'élément d'extension afin de provoquer un freinage magnétique du drone.
일 실시예에 따른 드론 이착륙 시스템은, 관통홀을 구비하는 드론 및 상기 관통홀을 통과할 수 있는 연장부재를 구비하는 착륙대를 포함하고, 상기 착륙대의 상기 연장부재가 상기 드론의 관통홀을 통과하는 경우 상기 관통홀과 상기 연장부재 사이에 와전류(Eddy Current)가 발생하여 상기 드론에 자기 제동(magnetic braking)이 발생될 수 있다.
A drone takeoff and landing system according to an embodiment comprises: a drone including a through-hole; and a landing pad including an extension member which can pass through the through-hole, wherein, when the extension member of the landing pad passes through the through-hole of the drone, an eddy current may occur between the through-hole and the extension member to cause magnetic braking of the drone.
La présente invention concerne, selon un mode de réalisation, un système de décollage et d'atterrissage de drone comprenant : un drone doté d'un orifice traversant ; et une plateforme d'atterrissage comprenant un élément d'extension qui peut passer à travers ledit orifice traversant. Lorsque l'élément d'extension de la plateforme d'atterrissage passe à travers l'orifice traversant du drone, un courant de Foucault peut se produire entre l'orifice traversant et l'élément d'extension afin de provoquer un freinage magnétique du drone.
일 실시예에 따른 드론 이착륙 시스템은, 관통홀을 구비하는 드론 및 상기 관통홀을 통과할 수 있는 연장부재를 구비하는 착륙대를 포함하고, 상기 착륙대의 상기 연장부재가 상기 드론의 관통홀을 통과하는 경우 상기 관통홀과 상기 연장부재 사이에 와전류(Eddy Current)가 발생하여 상기 드론에 자기 제동(magnetic braking)이 발생될 수 있다.
DRONE TAKEOFF AND LANDING SYSTEM
SYSTÈME DE DÉCOLLAGE ET D'ATTERRISSAGE DE DRONE
드론 이착륙 시스템
LEE SEON HO (author)
2018-06-21
Patent
Electronic Resource
Korean
IPC:
E01F
ADDITIONAL WORK, SUCH AS EQUIPPING ROADS OR THE CONSTRUCTION OF PLATFORMS, HELICOPTER LANDING STAGES, SIGNS, SNOW FENCES, OR THE LIKE
,
Zusätzliche Baumaßnahmen, wie die Ausstattung von Straßen oder die bauliche Ausbildung von Bahnsteigen, Landeplätzen für Hubschrauber, Wegweisern, Schneezäunen oder dgl.
/
B64C
AEROPLANES
,
Flugzeuge
A drone takeoff and landing system with a landing permission module
| European Patent Office | 2017
| European Patent Office | 2022