← eVTOL产品
Pan Jiazhi, Zhu Wenxi and Lai Zexin · China
Yee Flying Car
Yee Flying Car
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
- 未公开／未录入
- 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
- 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
- Batteries
- 电机
- 2 electric motors (possibly 4 more electric motors for the wings and propellers to fold in and out from the fuselage)
- 旋翼／螺旋桨
- 2 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), 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 of critical components in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Roadable eVTOL passenger vehicle concept design
- Piloting
- 1 pilot
- Propellers
- 2 propellers
- Electric motors
- 2 electric motors (possibly 4 more electric motors for the wings and propellers to fold in and out from the fuselage)
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Wings
- 1 main high forward-swept wing
- Tail
- 2 horizontal stabilizers
- Landing gear
- Retractable wheeled landing gear.
- Road travel
- For road travel, the high forward-swept wing folds down and small wheels are located on the road edge of the wing. The rear two propellers fold parallel to the fuselage and the outside rim of the propellers is the tire tread.
- 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 of critical components in the sub-systems of the aircraft.