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Delft University of Technology · Netherlands

Wigeon

Delft University of Technology Wigeon

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
4 passengers
乘客
未公开/未录入
驾驶方式
1 pilot
航程(按来源口径)
400 km (249 m)
巡航速度
Unknown
最大速度
未公开/未录入
最大起飞重量
Unknown
载荷
Unknown
空重
Unknown
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
24 solid-state lithium battery packs
电机
12 electric motors
旋翼/螺旋桨
12 propellers
续航时间
Unknown
飞行高度
Unknown
安全设计
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft. The aircraft can also glide and land like a conventional airplane on a runway or road, in an emergency.

全部原始参数

Specifications:

Aircraft type
eVTOL long-range passenger aircraft
Piloting
1 pilot
Capacity
4 passengers
Cruise speed
Unknown
Range
400 km (249 m)
Flight time
Unknown
Cruise altitude
Unknown
Empty weight
Unknown
Maximum payload
Unknown
Maximum takeoff weight
Unknown
Propellers
12 propellers
Electric motors
12 electric motors
Power source
24 solid-state lithium battery packs
Fuselage
Unknown (possibly carbon fiber composite)
Windows
Panoramic wrap around windows allowing forward, left, right visibility, for spectacular views with a solid roof above the passenger compartment
Wings
Tandem wings with winglets, the front wings have downward facing winglets and the rear wings have upward facing winglets
Tail
1 vertical stabilizer
Landing gear
Unknown (most likely retractable tricycle wheeled landing gear)
Safety features
Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft. The aircraft can also glide and land like a conventional airplane on a runway or road, in an emergency.