公开(公告)号：US10577098B2

公开(公告)日：2020-03-03

申请号：US15503252

申请日：2014-12-30

Applicant: KOREA AEROSPACE RESEARCH INSTITUTE

Inventor： Sungho Chang

IPC: B64C39/00 ,  B64C39/02 ,  B64C37/02 ,  B64D47/08

Abstract: Provided is a drone having a reconfigurable shape, more specifically, a drone having a reconfigurable shape that is capable of being horizontally flown without a rotation motion of the drone by configuring unit module drones having a rectangular parallelepiped shape that may apply thrusts in six directions and is capable of being flown singly or flown in various shapes by forming an assembly drone by coupling between the unit module drones.

公开(公告)号：US20230286645A1

公开(公告)日：2023-09-14

申请号：US18061042

申请日：2022-12-02

Applicant: Korea Aerospace Research Institute

Inventor： Youngshin Kang ,  Bumjin Park ,  Seongwook Choi ,  Yushin Kim ,  Jongmin Bae ,  Joowon Choi ,  Sungho Chang

IPC: B64C13/04 ,  B64D43/00

CPC classification number: B64C13/0421 ,  B64D43/00 ,  B64C29/0008

Abstract: The present invention relates to a control input device applicable to an eVTOL aircraft, which is an electric-powered vertical take-off and landing aircraft, and more particularly, to an aircraft control input device that may replace a cyclic control stick, a tail rotor control pedal, and a collective control stick used for flight control of a conventional aircraft, which is simpler in configuration and easier to operate than conventional control devices and may improve pilot convenience and stability of flight operation through simple and accurate flight manipulation, and a command input method using the same.