VERTICAL TAKE-OFF AND LANDING AIRCRAFT

VERTICAL TAKE-OFF AND LANDING AIRCRAFT

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

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Hauptverfasser: Uchida, Kenta, Yoshimura, Kaisaku, Kato, Masashi, Tsukamoto, Toshinori, Aizawa, Bon
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
CONTROLLING
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
PHYSICS
REGULATING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
TRANSPORTING
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creator Uchida, Kenta
Yoshimura, Kaisaku
Kato, Masashi
Tsukamoto, Toshinori
Aizawa, Bon
description In a vertical take-off and landing aircraft, a plurality of VTOL rotors are divided into a plurality of groups, and each VTOL rotor is included in any one of the groups. After lift is generated by wings (a front wing and a rear wing), a controller sequentially stops rotation of the plurality of VTOL rotors on a group-by-group basis.
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subjects AEROPLANES
AIRCRAFT
AVIATION
CONTROLLING
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
PHYSICS
REGULATING
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
TRANSPORTING
title VERTICAL TAKE-OFF AND LANDING AIRCRAFT
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