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快轮科技(RICTOR) · Rictor, KuickWheel · China

Skyrider X1

Rictor, KuickWheel Skyrider X1

构型待核实 · 生产型设计 · 核查 2026-10-01

飞行构型与公司名称

构型待核实

VFS 原始目录分组:个人飞行器。尚无足够资料确定具体布局。

核对构型依据 ↗

原始目录分组:个人飞行器 · 个人飞行器属于产品形态,构型另行识别。

中文名称:快轮科技(RICTOR) · 原名:Rictor, KuickWheel

核对中文名称 ↗

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 0/3 · 生产型设计 · 目录依据 · 目录阶段,尚未核实批准状态

查看状态依据 ↗订阅本机型报道 RSS →

主要参数

座位/载员
未公开/未录入
乘客
未公开/未录入
驾驶方式
1 pilot with an AI automatic route planning function and automated takeoff and landing capability. The company's avionics adjusts flight altitude, speed and direction in real-time according to weather and environmental changes, for an efficient and safe flight experience. The aircraft can be flown manually with a joystick control. Displays real-time data, weather updates, and system status for full situational awareness.
航程(按来源口径)
未公开/未录入
巡航速度
未公开/未录入
最大速度
未公开/未录入
最大起飞重量
200 kg (440 lb)
载荷
未公开/未录入
空重
80 kg (176 lb)
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
Hybrid-electric power source
电机
8 electric motors
旋翼/螺旋桨
8 stacked propellers (with automatic folding and unfolding system)
续航时间
25-40 minutes
飞行高度
未公开/未录入
安全设计
Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Specifically, the aircraft has a triple-redundant flight control system. Having multiple redundant systems on any aircraft decreases having any single point of failure. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.

全部原始参数

Specifications:

Aircraft type
Passenger hybrid-electric VTOL sea-land-air motorcycle-aircraft
Piloting
1 pilot with an AI automatic route planning function and automated takeoff and landing capability. The company's avionics adjusts flight altitude, speed and direction in real-time according to weather and environmental changes, for an efficient and safe flight experience. The aircraft can be flown manually with a joystick control. Displays real-time data, weather updates, and system status for full situational awareness.
Maximum cruise speed
100 km/h (62 mph)
Range (air)
300 km (186 miles)
Flight time
25-40 minutes
Maximum cruise altitude
200 m (656 ft)
Empty weight
80 kg (176 lb)
Maximum payload weight
120 kg (264 lb)
Maximum takeoff weight
200 kg (440 lb)
Propellers
8 stacked propellers (with automatic folding and unfolding system)
Electric motors
8 electric motors
Power source
Hybrid-electric power source
Fuselage
Carbon fiber composite and aerospace-grade aluminum
Window
Canopy over cockpit
Landing gear
Retractable 1 front and 1 rear motorcycle tires, with retractable rear training wheels to keep the flying motorcycle upright without having to use a kickstand
Safety features
Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Specifically, the aircraft has a triple-redundant flight control system. Having multiple redundant systems on any aircraft decreases having any single point of failure. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.

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。