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Dufour Aerospace · Switzerland

aEro 2

Dufour Aerospace aEro 2

矢量推力 · 停研/历史型号 · 核查 2026-10-01

下列为 VFS 目录披露的参数,包含设计目标及历史版本信息。目录阶段不等于适航或量产状态;不同任务条件的航程与载荷不能直接当作同一条件下的性能。

主要参数

座位/载员
2 people total
乘客
未公开/未录入
驾驶方式
Piloted or autonomous
航程(按来源口径)
800 km (497 miles)
巡航速度
320 km/h (199 mph)
最大速度
未公开/未录入
最大起飞重量
未公开/未录入
载荷
未公开/未录入
空重
未公开/未录入
长度
未公开/未录入
翼展
未公开/未录入
高度
未公开/未录入
动力来源
未公开/未录入
电机
4 electric motors (there are two electric motors for each propeller, for redundancy)
旋翼/螺旋桨
2 propellers
续航时间
未公开/未录入
飞行高度
未公开/未录入
安全设计
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. In case of total power failure to the propellers, the aircraft can also land like an airplane.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric or eVTOL two passenger concept design aircraft
Piloting
Piloted or autonomous
Capacity
2 people total
Cruise speed
320 km/h (199 mph)
Range
800 km (497 miles)
Propellers
2 propellers
Electric motors
4 electric motors (there are two electric motors for each propeller, for redundancy)
Window
Panoramic wrap around windows with forward, left and right visibility for spectacular views by the passengers
Wing
High tilt-wing with flaps and winglets
Tail
Has a conventional tail plus a downward ventral fin
Landing gear
Tail dragger fixed landing gear, with small rear wheel
Noise
Low noise and low downwash profile
Safety Features
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers and motors on the aircraft so if one or more motors or propellers fail, the other working motors and propellers can safely land the aircraft. In case of total power failure to the propellers, the aircraft can also land like an airplane.