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CycloTech GmbH · Austria
Air Taxi V2
CycloTech Air Taxi V2
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
- 2 passengers (possibly)
- 乘客
- 未公开／未录入
- 驾驶方式
- Manual, remote or autonomous piloting
- 航程（按来源口径）
- 85 km (53 m)
- 巡航速度
- 未公开／未录入
- 最大速度
- ~124 mph
- 最大起飞重量
- 2,200 kg (4,850 lb)
- 载荷
- 未公开／未录入
- 空重
- 1800 kg (3,970 lb)
- 长度
- 7 m (~23 ft)
- 翼展
- 未公开／未录入
- 高度
- 未公开／未录入
- 动力来源
- Batteries (the aircraft has the option for other power sources)
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 CycloRotors
- 续航时间
- 40 minutes
- 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 in this case, CycloRotors, and motors on the aircraft, so if one or more CycloRotors or motors fail, the other working CyclorRotors 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 concept design aircraft
- Piloting
- Manual, remote or autonomous piloting
- Capacity
- 2 passengers (possibly)
- Maximum speed
- ~124 mph
- Range
- 85 km (53 m)
- Flight time
- 40 minutes
- Empty weight
- 1800 kg (3,970 lb)
- Maximum payload weight
- 400 kg (880 lb)
- Maximum takeoff weight
- 2,200 kg (4,850 lb)
- Propellers
- 8 CycloRotors
- Electric motors
- 8 electric motors
- Power source
- Batteries (the aircraft has the option for other power sources)
- Maximum hover thrust
- 30,000 N (6,744 lb)
- Maximum drive power
- 1,660 kW (2,226 hp)
- Batteries
- 760 kg @ 230 Wh/kg (1,676 lb @ 230 Wh/lb)
- Rotor dimensions
- 100 x 120 cm (39 in x 47 in)
- Rotation speed
- 1,600 rpm
- Fuselage
- Carbon fiber composite
- Length
- 7 m (~23 ft)
- Width
- 5 m (~16.5 ft)
- Window
- Canopy over cockpit
- Tail
- 1 vertical stabilizer
- Landing gear
- Unknown
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers or in this case, CycloRotors, and motors on the aircraft, so if one or more CycloRotors or motors fail, the other working CyclorRotors and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft.