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Winged Tiger Aviation · China
Tianyi-Ti
Winged Tiger Aviation Tianyi-Ti
多旋翼 · 原型机 · 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
- Autonomous driving and flying
- 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
- 300 kg (661 lb)
- 载荷
- 未公开／未录入
- 空重
- 220 kg (485 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
- 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
- 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
- Air-ground passenger eVTOL multicopter module prototype vehicle
- Piloting
- Autonomous driving and flying
- Capacity
- 2 people and their luggage
- Cruise speed (flight or ground)
- Unknown
- Empty weight
- 220 kg (485 lb)
- Maximum payload weight
- 80 kg (176 lb)
- Maximum takeoff weight
- 300 kg (661 lb)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- Battery packs
- 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
- Landing gear
- Fixed skid landing gear
- Ground module
- No information is available for the ground module
- 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.