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Aibot US Inc. · USA
aiEVTOL
Aibot US Inc. aiEVTOL
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
- 6 passengers
- 乘客
- 未公开/未录入
- 驾驶方式
- 1 pilot (at first), then AI using compact fly-by-wire (cFBW)
- 航程(按来源口径)
- 250 miles (402 km) (range will vary with speed and payload)
- 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
- 7,000 lb (3,175 kg)
- 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
- 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) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.
全部原始参数
Specifications:
- Aircraft type
- Long-range hyper-performance passenger and cargo eVTOL concept design aircraft
- Piloting
- 1 pilot (at first), then AI using compact fly-by-wire (cFBW)
- Capacity
- 6 passengers
- Maximum cruise speed
- 250 mph (402 km/h)
- Range
- 250 miles (402 km) (range will vary with speed and payload)
- Maximum payload weight
- 1,000 lb (454 kg)
- Maximum takeoff weight
- 7,000 lb (3,175 kg)
- Propellers
- 8 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
- Window
- Canopy over cockpit
- Wings
- 1 wing, 47 ft (14.3 m) (1 wing possibly)
- Tail
- Unknown
- Landing gear
- Unknown (possibly retractable tricycle wheeled landing gear)
- Safety features
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.