← eVTOL产品
Commercial Aircraft Corporation of China, Ltd. (COMAC) · China
CE-4VT
Commercial Aircraft Corporation of China (COMAC) CE4VT
升力＋巡航 · 概念设计 · 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
- 3 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- Unknown but this is a long-range aircraft
- 巡航速度
- Unknown
- 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
- Battery packs
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 propellers (4 for forward flight, 4 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 concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 3 passengers
- Cruise speed
- Unknown
- Range
- Unknown but this is a long-range aircraft
- Maximum payload weight
- ~450 kg (~992 lb)
- Propellers
- 8 propellers (4 for forward flight, 4 VTOL only propellers)
- Electric motors
- 8 electric motors
- Power source
- Battery packs
- Fuselage
- Carbon fiber composite
- Windows
- Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
- Wings
- 1 main high wing
- Tail
- 1 boom 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.