NOVEL WING APPARATUS

The novel wing design disclosed herein has a cambered, swept wing design for aircraft application that can achieve steady state flight via the integration of an electric motor driven lift-thrust system that can provide both vertical thrust for take-off and horizontal thrust for flight propulsion by...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	Bermudez Onopa, Ramon David
Format:	Patent
Sprache:	eng
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:	The novel wing design disclosed herein has a cambered, swept wing design for aircraft application that can achieve steady state flight via the integration of an electric motor driven lift-thrust system that can provide both vertical thrust for take-off and horizontal thrust for flight propulsion by the selective use of fan blades connected to the motor.