← eVTOL产品
Blue Space Aircraft Co., Ltd. · China
Yunfan-2
Blue Space Aircraft Company (Weilan Space Flight Technology) Yunfan-2
矢量推力 · 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
- 5.6 cubic meters for air cargo. Possibly 4-5 passengers and their luggage.
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous
- 航程（按来源口径）
- 300 km (186 m)
- 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
- 2,000 kg (4,409 lb)
- 载荷
- 未公开／未录入
- 空重
- 1,500 kg (3,307 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
- Battery packs or hybrid-electric
- 电机
- 12 electric motors
- 旋翼／螺旋桨
- 12 tilt-propellers
- 续航时间
- 未公开／未录入
- 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.
全部原始参数
Specifications:
- Aircraft type
- Air cargo and passenger eVTOL prototype aircraft
- Piloting
- Autonomous
- Capacity
- 5.6 cubic meters for air cargo. Possibly 4-5 passengers and their luggage.
- Maximum flight speed
- 450 km/h (280 mph)
- Range
- 300 km (186 m)
- Empty weight
- 1,500 kg (3,307 lb)
- Maximum payload weight
- 500 kg (1,102 lb)
- Maximum takeoff weight
- 2,000 kg (4,409 lb)
- Propellers
- 12 tilt-propellers
- Electric motors
- 12 electric motors
- Power source
- Battery packs or hybrid-electric
- Fuselage
- Carbon fiber composite
- Windows (passenger model)
- Panoramic wrap around windows allowing forward, left and right visibility for spectacular views for the passengers
- Wings
- Tandem wings. 1 front low wing, 1 high main wing with winglets.
- Landing gear
- 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.