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Volocopter GmbH · Germany
e-volo uVC400 cargo
Volocopter e-volo uVC400 cargo
多旋翼 · 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
- Cargo only, no passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote or autonomous
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 未公开／未录入
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- 275 kg (606 lb)
- 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
- Battery or hybrid-electric power source
- 电机
- 18 electric motors
- 旋翼／螺旋桨
- 18 propellers
- 续航时间
- 2 hours with a hybrid-electric power source
- 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. There is also an aircraft parachute. Has automatic altitude control, automatic gentle landing, crosswinds and turbulence is automatically compensated for. Redundancy has been built into the aircraft so if one critical system breaks, there are other same exact systems so the aircraft can continue flying and safely land.
全部原始参数
Specifications:
- Aircraft type
- eVTOL or hybrid-electric VTOL cargo design concept
- Piloting
- Remote or autonomous
- Capacity
- Cargo only, no passengers
- Flight time
- 2 hours with a hybrid-electric power source
- Maximum payload
- 275 kg (606 lb)
- Propellers
- 18 propellers
- Electric Motors
- 18 electric motors
- Propeller frame diameter
- 10.8 meter (over 35 feet)
- Power source
- Battery or hybrid-electric power source
- Fuselage
- Based on the e-volo VC400 single passenger eVTOL aircraft
- Landing gear
- Fixed skid landing gear
- 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. There is also an aircraft parachute. Has automatic altitude control, automatic gentle landing, crosswinds and turbulence is automatically compensated for. Redundancy has been built into the aircraft so if one critical system breaks, there are other same exact systems so the aircraft can continue flying and safely land.