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Hangzhou Zhiyuan Research Institute · China
Wearable Flying Device
Hangzhou Zhiyuan Research Institute Wearable Flying Device
个人飞行器 · 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 with a ground station-assisted control system, with an augmented reality (AR) helmet and joystick controls for intuitive operation
- 航程(按来源口径)
- 8 km (5 miles)
- 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
- 未公开/未录入
- 载荷
- 未公开/未录入
- 空重
- 未公开/未录入
- 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 (maybe?)
- 电机
- 3 electric motors
- 旋翼/螺旋桨
- 3 ducted fans
- 续航时间
- 20 minutes
- 飞行高度
- 1,000 m (3,280 feet)
- 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. According to the institute, one of the safety features of the flying device is a one-click pilot-aircraft separation, deploying a low-altitude parachute to ensure a safe forced landing for the pilot.
全部原始参数
Specifications:
- Aircraft type
- One person eVTOL wearable aircraft
- Piloting
- 1 pilot with a ground station-assisted control system, with an augmented reality (AR) helmet and joystick controls for intuitive operation
- Maximum cruise speed
- 60 km/h (37 mph)
- Range
- 8 km (5 miles)
- Flight time
- 20 minutes
- Maximum altitude
- 1,000 m (3,280 feet)
- Maximum payload weight
- ~91 kg (~200 lb)
- Propellers
- 3 ducted fans
- Electric motors
- 3 electric motors
- Power source
- Battery packs (maybe?)
- Frame material
- Unknown
- Landing gear
- Fixed tricycle strut 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. According to the institute, one of the safety features of the flying device is a one-click pilot-aircraft separation, deploying a low-altitude parachute to ensure a safe forced landing for the pilot.