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Guangdong Yufei Aviation Investment Co., Ltd · China
Yutu A100
Guangdong Yufei Aviation Investment Yutu A100
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 person
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 72 km/h (45 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 225 kg (497 lb)
- 载荷
- 未公开／未录入
- 空重
- 115 kg (254 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
- Batteries
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 propellers
- 续航时间
- 20 minutes
- 飞行高度
- <10 meters (32.8 ft)
- 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 eVTOL prototype aircraft
- Piloting
- 1 person
- Cruise speed
- 72 km/h (45 mph)
- Flight time
- 20 minutes
- Cruise altitude
- <10 meters (32.8 ft)
- Empty weight
- 115 kg (254 lb)
- Maximum payload weight
- 110 kg (243 lb)
- Maximum takeoff weight
- 225 kg (497 lb)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- Batteries
- Charging time
- About 50 minutes
- Fuselage
- EPP foam exterior and race-grade frame
- Window
- Open cockpit with roll bars
- Landing gear
- Lands on the bottom of the fuselage
- 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.