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Aviation Industry Corporation of China (AVIC) AR-E3000 · China
AR-E3000
Aviation Industry Corporation of China (AVIC) AR-E3000
矢量推力 · 原型机 · 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
- 3 passengers and luggage
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 200 km (124 mph)
- 巡航速度
- Unknown
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 2,600 kg (5,732 lb)
- 载荷
- 未公开／未录入
- 空重
- 2,150 kg (4,740 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
- Batteries
- 电机
- 12 electric motors
- 旋翼／螺旋桨
- 12 propellers (4 tilt-props, 8-VTOL only 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.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL prototype aircraft
- Piloting
- 1 pilot
- Capacity
- 3 passengers and luggage
- Cruise speed
- Unknown
- Range
- 200 km (124 mph)
- Empty weight
- 2,150 kg (4,740 lb)
- Maximum payload weight
- 450 kg (992 lb)
- Maximum takeoff weight
- 2,600 kg (5,732 lb)
- Propellers
- 12 propellers (4 tilt-props, 8-VTOL only propellers)
- Electric motors
- 12 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- Large panoramic wrap around windows
- Wing
- 1 main high wing
- Tail
- 1 V tail
- Landing gear
- Fixed tricycle wheeled 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.