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WeFly (Qifei Aviation Technology) · China
WF-01
WeFly (Qifei Aviation Technology) WF-01
升力+巡航 · 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
- Simulated passenger or simulated cargo capability
- 乘客
- 未公开/未录入
- 驾驶方式
- Remote or autonomous
- 航程(按来源口径)
- Long-range, the actual range is unknown
- 巡航速度
- Unknown
- 最大速度
- 未公开/未录入
- 最大起飞重量
- 600 kg (1,320 lb)
- 载荷
- 未公开/未录入
- 空重
- 500 kg (1,100 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
- 电机
- 8 electric motors
- 旋翼/螺旋桨
- 6 VTOL-only propellers, 2 ducted fans for forward flight
- 续航时间
- 未公开/未录入
- 飞行高度
- 未公开/未录入
- 安全设计
- Most likely: Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- eVTOL subscale prototype aircraft
- Piloting
- Remote or autonomous
- Capacity
- Simulated passenger or simulated cargo capability
- Cruise speed
- Unknown
- Range
- Long-range, the actual range is unknown
- Empty weight
- 500 kg (1,100 lb)
- Maximum payload weight
- 100 kg (220 lb)
- Maximum takeoff weight
- 600 kg (1,320 lb)
- Propellers
- 6 VTOL-only propellers, 2 ducted fans for forward flight
- Electric motors
- 8 electric motors
- Power source
- Battery packs
- Fuselage
- Carbon fiber composite
- Windows
- None
- Wings
- 1 main high wing
- Tail
- 1 vertical stabilizer
- Landing gear
- Fixed skid landing gear
- Safety features
- Most likely: Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft.