Steuervorrichtung für Flugzeuge

Details

Veröffentlichungs-Nr.

EP4345002

Aktenzeichen

EP23199792

Anmeldetag

26. September 2023

Veröffentlichung

17. September 2025

Erteilung

17. September 2025

Rechtsraum

EP

IPC

B64C27/26B64C27/30B64C29/00B64U10/20

Abstract

A control device (48) for an vertical take-off and landing (VTOL) aircraft (10) with at least a fixed wing (18, 20) and a plurality of rotors (12) is provided. In a state where lift is generated in the wing (18, 20), said control device (48) controls the pitch of each blade (26) and the stopped state rotation angle of each VTOL rotor (12) to control the force generated in each VTOL rotor (12) in a state where rotation of the VTOL rotor (12) is stopped, thereby applying a force to a fuselage (16).

Anmelder

Firma

HONDA MOTOR CO., LTD.

Land

🇯🇵 Japan

Fachgebiete