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CycloTech GmbH · Austria
Air Taxi V2
CycloTech Air Taxi V2
其他推力转向（待细分） · 概念设计 · 核查 2026-10-01
飞行构型与公司名称
其他推力转向（待细分）
VFS 原始目录分组：矢量推力。尚无足够资料确定具体布局。
核对构型依据 ↗原始目录分组：矢量推力
中文名称：待核实 · 原名：CycloTech GmbH
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。
资料覆盖与状态依据
可用性能指标 1/3 · 概念设计 · 目录依据 · 目录阶段，尚未核实批准状态
查看状态依据 ↗概念参数，尚不代表已实现性能
订阅本机型报道 RSS →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.
明确提及本机型的报道
暂无明确匹配的公开报道；通用或重名型号不会自动关联。
目录参数变化记录
从保存的目录刷新快照比较，资料修改不等于实机性能发生变化。
暂无已保存的版本变化，后续目录刷新将保留快照。