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Shiyun Aviation Technology Co., Ltd. (Steadywin) · China
SW One
Shiyun Aviation Technology (Steadywin) SW One
多旋翼 · 原型机 · 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
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 50 km (30 m)
- 巡航速度
- ~97 km/h (60 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- 未公开／未录入
- 空重
- 300 kg (660 lb) [or this might be the maximum takeoff weight]
- 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
- 8 lithium-polymer batteries
- 电机
- 12 electric motors
- 旋翼／螺旋桨
- 12 propellers
- 续航时间
- 30 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. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL multicopter prototype aircraft
- Piloting
- 1 pilot
- Cruise speed
- ~97 km/h (60 mph)
- Range
- 50 km (30 m)
- Flight time
- 30 minutes
- Empty weight
- 300 kg (660 lb) [or this might be the maximum takeoff weight]
- Propellers
- 12 propellers
- Electric motors
- 12 electric motors
- Power source
- 8 lithium-polymer batteries
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Landing gear
- Fixed skid landing gear (similar to some types of helicopter fixed skid landing gear)
- 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. Having multiple redundant systems on any aircraft decreases having any single point of failure. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.