DUAL FUNCTON AIRCRAFT

DUAL FUNCTON AIRCRAFT

An aircraft 10 includes an electric power source 40 having a combustion engine 94 and an electric generator 96. The electric generator 96 is powered by the combustion engine 94. The aircraft 10 also includes a propulsion assembly 38 including a propulsor and an electric motor 86, the electric motor...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: VONDRELL, Randy M, CRABTREE, Glenn David, BARONE, Dominic
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES
ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL
HELICOPTERS
MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:An aircraft 10 includes an electric power source 40 having a combustion engine 94 and an electric generator 96. The electric generator 96 is powered by the combustion engine 94. The aircraft 10 also includes a propulsion assembly 38 including a propulsor and an electric motor 86, the electric motor 86 configured for rotating the propulsor. The aircraft 10 also includes an electrical outlet 92 configured for connection with an outside power sink. The electrical outlet 92 and the propulsion assembly 38 are selectively in electrical communication with the electric power source 40 such that the electric power source 40 selectively provides electrical power to one of the electrical outlet 92 or the propulsion assembly 38.