← eVTOL产品
Guangdong Pengcheng Wanli Aviation Technology · China
PC-200
Guangdong Pengcheng Wanli Aviation Technology PC-200
升力＋巡航 · 阶段未核实 · 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
- 2 people and their luggage
- 乘客
- 未公开／未录入
- 驾驶方式
- Pilot or autonomous
- 航程（按来源口径）
- 150 km (93 miles)
- 巡航速度
- 120 km/h (75 mph)
- 最大速度
- 150 km/h (93 mph)
- 最大起飞重量
- 1,200 kg (2,645 lb)
- 载荷
- 未公开／未录入
- 空重
- 980 kg (2,160 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 motors
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 propellers
- 续航时间
- 未公开／未录入
- 飞行高度
- 1,500 m (4,920 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 mock-up aircraft
- Piloting
- Pilot or autonomous
- Capacity
- 2 people and their luggage
- Cruise speed
- 120 km/h (75 mph)
- Maximum speed
- 150 km/h (93 mph)
- Range
- 150 km (93 miles)
- Cruise altitude
- 1,500 m (4,920 ft)
- Maximum altitude
- 6,000 m (19,685 ft)
- Empty weight
- 980 kg (2,160 lb)
- Maximum payload weight
- 220 kg (485 lb)
- Maximum takeoff weight
- 1,200 kg (2,645 lb)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- Battery motors
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Wings
- 1 main high wing
- Tail
- 2 vertical stabilizers and 1 horizontal stabilizer
- Landing gear
- Fixed quadricycle wheeled 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.