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Guangdong Pengcheng Wanli Aviation Technology · China

PC-500

Guangdong Pengcheng Wanli Aviation Technology PC-500

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
5 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)
未公开/未录入
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
2,700 kg (5,950 lb)
载荷
未公开/未录入
空重
2,200 kg (4,850 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 or hybrid-electric (for extended range version)
电机
6 electric motors
旋翼/螺旋桨
6 tilt-props
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 and air cargo eVTOL and hyrbid-electric VTOL concept design aircraft
Piloting
1 pilot
Capacity
5 passengers and their luggage
Cruise speed (all-electric)
240 km/h (150 mph)
Maximum speed (all-electric)
300 km/h (186 mph)
Range (all-electric)
200 km (125 miles)
Flight time (all-electric)
1 hour
Cruise speed (extended range)
300 km/h (186 mph)
Maximum speed (extrended range)
360 km/h (224 mph)
Range (extended range)
600 km (373 miles)
Flight time (extened range)
2 hours
Empty weight
2,200 kg (4,850 lb)
Maximum payload weight
500 kg (1,100 lb)
Maximum takeoff weight
2,700 kg (5,950 lb)
Propellers
6 tilt-props
Electric motors
6 electric motors
Power source
Battery packs or hybrid-electric (for extended range version)
Fuselage
Carbon fiber composite
Windows
Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
Wings
1 high wing
Tail
1 V tail
Landing gear
Fixed tricycle 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.