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Overair, Inc. · USA
Butterfly V2
Overair (Karem) Butterfly
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
- 未公开／未录入
- 乘客
- 5 passengers with luggage
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 100 miles (161 km)
- 巡航速度
- 180 mph (290 km/h)'
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- 1,100 lb (499 kg)
- 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
- Batteries
- 电机
- 4 electric motors
- 旋翼／螺旋桨
- 4 propellers. A quad tilt-rotor with Optimum Speed Tiltrotor (OSTR) technology (a large rotor, slow turning). propeller.
- 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 in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL concept design aircraft
- Pilot
- 1 pilot
- Passengers
- 5 passengers with luggage
- Cruise speed
- 180 mph (290 km/h)'
- Maximum cruise speed
- 200 mph (322 km/h)
- Range
- 100 miles (161 km)
- Payload
- 1,100 lb (499 kg)
- Propellers
- 4 propellers. A quad tilt-rotor with Optimum Speed Tiltrotor (OSTR) technology (a large rotor, slow turning). propeller.
- Electric Motors
- 4 electric motors
- Power source
- Batteries
- Windows
- The windows are larger than conventional aircraft providing better views for the passengers
- Wing
- Tandem wings with winglets
- Tail
- 1 vertical stabilizer
- Landing gear
- Retractable tricycle wheeled landing gear
- 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 in the sub-systems of the aircraft.