Tilt-Rotor eVTOL

Specifications:

Aircraft type

Tilt-rotor autonomous passenger eVTOL concept design aircraft

Piloting

Autonomous

Capacity

Unknown

Cruise speed

Unknown

Maximum payload weight

1,202 kg (2,650 lb)

Maximum takeoff weight

2,585 kg (5,700 lb)

Propellers

Tilt-rotors (the number of tilt-rotors is unknown)

Electric motors

The number of electric motors will be the same as the number of propellers

Power source

The power source might be a conventional turboshaft engine or it can be fitted with an all battery power source, a hybrid system or a hybrid-hydrogen power source

Fuselage

Carbon fiber composite

Windows

Most new eVTOL aircraft have larger windows than conventional aircraft and the design will most likely follow this pattern

Wings

At least one tilt-wing

Tail

Unknown

Landing gear

Unknown

Safety features

Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure. There is the possibility there will be a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.