公开(公告)号：EP4311770A1

公开(公告)日：2024-01-31

申请号：EP23188288.7

申请日：2023-07-28

申请人： HONDA MOTOR CO., LTD.

发明人： AIZAWA, Bon ,  TSUKAMOTO, Toshinori ,  KATO, Masashi ,  UCHIDA, Kenta ,  YOSHIMURA, Kaisaku

IPC分类号： B64C29/00 ,  B64C39/04 ,  B64C39/08 ,  B64D27/24 ,  B64D31/06 ,  B64C27/30

摘要： In a vertical take-off and landing aircraft (10), a plurality of VTOL rotors (20) are divided into a plurality of groups, and each VTOL rotor (20) is included in any one of the groups. After lift is generated by wings (a front wing (14) and a rear wing (16)), a controller (46) sequentially stops rotation of the plurality of VTOL rotors (20) on a group-by-group basis.