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CycloTech GmbH · Austria
Air Taxi V1
CycloTech Air Taxi V1
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
- 3 passengers and luggage
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 85 km (53 m)
- 巡航速度
- 150 km/h (93 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 2,200 kg (4,850 lb)
- 载荷
- 未公开／未录入
- 空重
- 1,800 kg (3,968 lb)
- 长度
- 275.6 in (700 cm)
- 翼展
- 未公开／未录入
- 高度
- 未公开／未录入
- 动力来源
- Conventional, hybrid-electric or all electric power source
- 电机
- 4 electric motors
- 旋翼／螺旋桨
- 4 Cyclogyro rotors
- 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
- Hybrid-electric VTOL or eVTOL passenger concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 3 passengers and luggage
- Cruise speed
- 150 km/h (93 mph)
- Range
- 85 km (53 m)
- Flight time
- 40 minutes
- Empty weight
- 1,800 kg (3,968 lb)
- Maximum payload weight
- 400 kg (882 lb)
- Maximum takeoff weight
- 2,200 kg (4,850 lb)
- Propellers
- 4 Cyclogyro rotors
- Rotor dimension
- 100 x 120 cm (39 in x 47 in)
- Rotation speed
- 1,600 rpm
- Electric motors
- 4 electric motors
- Power source
- Conventional, hybrid-electric or all electric power source
- Battery information
- 760 kg @ 230 Wh/kg (1,676 lb @ 230 Wh/lb)
- Fuselage
- Carbon fiber composite
- Length
- 275.6 in (700 cm)
- Width
- 197 in (500 cm)
- Windows
- Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
- Landing gear
- Fixed skid landing gear
- 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.