Sichuan Xunfei Aviation Engineering Technology Co., Ltd. · China

Wenyao

Sichuan Xunfei Aviation Engineering Technology Wenyao

矢量推力 · 原型机 · 核查 2026-10-01

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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: 4 passengers and their luggage or can be used for an all air cargo aircraft
乘客: 未公开／未录入
驾驶方式: Remote or piloted. If piloted, the aircraft would hold 3 passengers.
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: 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
电机: 6 electric motors
旋翼／螺旋桨: 6 propellers (4 coaxial contra-rotating tilt-propellers, 2 contra-rotating VTOL-only 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 (for the planned full-scale production aircraft for estimated 2030 production year):

Aircraft type: Passenger eVTOL full-scale concept design aircraft (to eventually made into their production aircraft)
Piloting: Remote or piloted. If piloted, the aircraft would hold 3 passengers.
Capacity: 4 passengers and their luggage or can be used for an all air cargo aircraft
Cruise speed (estimated): 250 km/h (155 mph)
Range (estimated): 300 km (186 miles)
Flight time (estimated): 70 minutes
Empty weight (estimated): 1,200 kg (2,645 lb)
Maximum payload weight (estimated): 400 kg (882 lb)
Maximum takeoff weight (estimated): 1,600 kg (3,527 lb)
Propellers: 6 propellers (4 coaxial contra-rotating tilt-propellers, 2 contra-rotating VTOL-only propellers)
Electric motors: 6 electric motors
Power source: Battery packs
Fuselage: Carbon fiber composite
Windows: Larger than conventional general aviation aircraft for forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
Wings: Tandem wings
Tail: 2 vertical stabilizers
Landing gear: Retractable 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.

Specifications (subscale prototype):

Aircraft type: Passenger eVTOL subscale prototype
Piloting: Remote
Capacity: None. This is a subscale prototype.
Cruise speed: Unknown
Propellers: 6 propellers (4 coaxial contra-rotating tilt-propellers, 2 contra-rotating VTOL-only propellers)
Electric motors: 6 electric motors
Power source: Battery packs
Fuselage: Carbon fiber composite
Windows: The prototype does have windows
Wings: Tandem wings
Tail: 2 vertical stabilizers
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.