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Yixiang UAV Team · China
eVTOL
Yixiang UAV Team eVTOL, Harbin Institute of Technology
矢量推力 · 概念设计 · 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
- 3 passengers and their luggage
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- >1,000 km (>621 miles)
- 巡航速度
- Unknown
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 2,100 kg (4,630 lb)
- 载荷
- 未公开／未录入
- 空重
- 1,700 kg (3,748 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
- High-energy-density hydrogen fuel cells
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 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
- Passenger hydrogen fueled eVTOL concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 3 passengers and their luggage
- Cruise speed
- Unknown
- Range
- >1,000 km (>621 miles)
- Empty weight
- 1,700 kg (3,748 lb)
- Maximum payload weight
- 400 kg (882 lb)
- Maximum takeoff weight
- 2,100 kg (4,630 lb)
- Propellers
- 6 propellers
- Electric motors
- 6 electric motors
- Power source
- High-energy-density hydrogen fuel cells
- Fuselage
- Carbon fiber composite
- Windows
- Standard commercial airliner windows
- Wings
- 1 high canard wing, 1 main high wing (on the top center of the fuselage)
- Tail
- 1 V-tail
- 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.