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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。

资料覆盖与状态依据

可用性能指标 1/3 · 原型机 · 目录依据 · 目录阶段,尚未核实批准状态

查看状态依据 ↗订阅本机型报道 RSS →

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.

明确提及本机型的报道

暂无明确匹配的公开报道;通用或重名型号不会自动关联。

目录参数变化记录

从保存的目录刷新快照比较,资料修改不等于实机性能发生变化。

暂无已保存的版本变化,后续目录刷新将保留快照。