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Chery Automobile · China
Land and Air Vehicle
Chery Automobile (Chery Group) Land and Air Vehicle
升力＋巡航 · 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
- 2 people and their luggage
- 乘客
- 未公开／未录入
- 驾驶方式
- 未公开／未录入
- 航程（按来源口径）
- 70–80 km (43– 50 miles)
- 巡航速度
- 未公开／未录入
- 最大速度
- 120 km/h (75 mph)
- 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
- Unknown
- 电机
- 9 electric motors
- 旋翼／螺旋桨
- 9 propellers (8 VTOL-only propellers, 1 pusher propeller)
- 续航时间
- 40 minutes
- 飞行高度
- 1,000 m (3,300 ft)
- 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
- Modular passenger eVTOL prototype aircraft and ground vehicle
- Piloting and driving
- Autonomous piloting and ground driving with an intelligent cockpit
- Capacity
- 2 people and their luggage
- Maximum speed
- 120 km/h (75 mph)
- Range
- 70–80 km (43– 50 miles)
- Flight time
- 40 minutes
- Maximum altitude
- 1,000 m (3,300 ft)
- Propellers
- 9 propellers (8 VTOL-only propellers, 1 pusher propeller)
- Electric motors
- 9 electric motors
- Power source
- Unknown
- 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 high main wing
- Tail
- 1 inverted U tail
- 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.