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CycloTech GmbH · Austria

Air Taxi V1

CycloTech Air Taxi V1

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 2/3 · 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
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.

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。