VERTICAL TAKE-OFF AND LANDING AIRCRAFT

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 rot...

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Bibliographische Detailangaben
Hauptverfasser:	UCHIDA, Kenta, AIZAWA, Bon, TSUKAMOTO, Toshinori, YOSHIMURA, Kaisaku, KATO, Masashi
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	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.