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Aridge (A division of XPeng) · China

Land Aircraft Carrier

Aridge (XPeng) Land Aircraft Carrier

多旋翼 · 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
未公开/未录入
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)
未公开/未录入
巡航速度
未公开/未录入
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
未公开/未录入
电机
未公开/未录入
旋翼/螺旋桨
未公开/未录入
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), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft.

全部原始参数

Specifications:

Aircraft type
Passenger eVTOL multicopter production model that fits inside a custom made hybrid-electric off-road van
Piloting (multicopter)
1 pilot flying manually or using automatic piloting
Capacity (multicopter)
2 passengers including the pilot
Van (off-road) capacity
4-5 passengers (including the driver)
Cruise speed (multicopter)
Unknown
Propellers (multicopter)
6 electric VTOL propellers and 2 ducted fans for forward and backwards flight
Electric motors (multicopter)
8 electric motors
Power source (multicopter)
Battery packs (charged using the hybrid-electric power source from the van)
Power source (van)
Hybrid-electric power source
Fuselage (multicopter)
Carbon fiber composite
Windows (multicopter)
Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
Landing gear (multicopter)
4 retractable strut landing gear
Wheels (van)
3-axle 6 wheeled all-wheel drive vehicle with rear wheel steering
Safety features
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft.