TILT WING AIRCRAFT

A tilt-wing aircraft is provided. The tilt-wing aircraft includes a tail drive and control unit. The control unit is configured to generate a forward thrust. The control unit can also generate an upwardly or downwardly directed thrust component and/or a laterally directed thrust component in hover f...

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Bibliographische Detailangaben
1. Verfasser:	STUHLBERGER, JOHANNES
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:	A tilt-wing aircraft is provided. The tilt-wing aircraft includes a tail drive and control unit. The control unit is configured to generate a forward thrust. The control unit can also generate an upwardly or downwardly directed thrust component and/or a laterally directed thrust component in hover flight and in climb flight of the aircraft.