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Aerial Rider · China
Six-Seater eVTOL
Aerial Rider Six-seater eVTOL
矢量推力 · 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
- 5 or 6 people depending if the aircraft is pilotless or not
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot (or a pilotless aircraft)
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- Unknown
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 2,585 kg (5,700 lb)
- 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
- The power source might be a conventional turboshaft engine or it can be fitted with an all battery power source, a hybrid system or a hybrid-hydrogen power source
- 电机
- The number of electric motors will be the same as the number of propellers
- 旋翼／螺旋桨
- Unknown
- 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. There is the possibility there will be a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL concept design aircraft
- Piloting
- 1 pilot (or a pilotless aircraft)
- Capacity
- 5 or 6 people depending if the aircraft is pilotless or not
- Cruise speed
- Unknown
- Maximum takeoff weight
- 2,585 kg (5,700 lb)
- Propellers
- Unknown
- Electric motors
- The number of electric motors will be the same as the number of propellers
- Power source
- The power source might be a conventional turboshaft engine or it can be fitted with an all battery power source, a hybrid system or a hybrid-hydrogen power source
- Fuselage
- Carbon fiber composite
- Windows
- Most new eVTOL aircraft have larger windows than conventional aircraft and the design will most likely follow this pattern
- Wings
- Unknown
- Tail
- Unknown
- Landing gear
- Unknown
- 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. There is the possibility there will be a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.