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CarryAll V2000CG
AutoFlight CarryAll V2000CG
升力＋巡航 · 生产型设计 · 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
- Air cargo only
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous
- 航程（按来源口径）
- 250 km (155 m)
- 巡航速度
- 200 km/h (124 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 2,000 kg (4,409 lb)
- 载荷
- 未公开／未录入
- 空重
- 1,600 kg (3,527 lb)
- 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 packs
- 电机
- 13 electric motors
- 旋翼／螺旋桨
- 13 propellers (10 VTOL only propellers, 3 pusher 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) 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. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.
全部原始参数
Specifications:
- Aircraft type
- Passenger air cargo eVTOL production aircraft
- Piloting
- Autonomous
- Capacity
- Air cargo only
- Cruise speed
- 200 km/h (124 mph)
- Range
- 250 km (155 m)
- Empty weight
- 1,600 kg (3,527 lb)
- Maximum payload weight
- 400 kg (882 lb)
- Maximum takeoff weight
- 2,000 kg (4,409 lb)
- Propellers
- 13 propellers (10 VTOL only propellers, 3 pusher propellers)
- Electric motors
- 13 electric motors
- Power source
- Battery packs
- Fuselage
- Carbon fiber composite
- Wings
- 1 canard. 1 high gull wing. 4 booms for VTOL propellers.
- Tail
- 2 downward vertical stabilizers
- Landing gear
- Fixed skid landing gear
- 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. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.