An aircraft system includes an aircraft fuselage having at least one coupling point that is configured to connect various mutually exchangeable drive module units detachably and load-transmittingly to the aircraft fuselage. The aircraft system further includes at least one first drive module unit that is detachably, load-transmittingly and with another drive module unit exchangeably attachable to the at least one coupling point to form a first aircraft comprising the aircraft fuselage and the first drive module unit and at least one second drive module unit that is detachably, load-transmittingly and with another drive module unit exchangeably attachable to the at least one coupling point to form a second aircraft comprising the aircraft fuselage and the second drive module unit. In some embodiments, the first aircraft is a rotary wing aircraft and the second aircraft is a fixed-wing aircraft or a convertiplane.
AIRCRAFT SYSTEM WITH INTERCHANGEABLE DRIVE MODULE UNITS
2020-03-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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