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Vehicle Systems, Dynamics and Design Laboratory · USA
TW-01 Minokawa
Auburn University TW-01
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
- 3 passengers
- 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
- 230 mph (370 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 6,000 lb (2,721 kg)
- 载荷
- 未公开／未录入
- 空重
- 3,300 lb (1,497 kg) for all-electric variant, 3,882 lb (1,761 kg) for hybrid-electric variant
- 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 (all-electric) or battery packs + turbo-generator (hybrid-electric)
- 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
- 3,000 ft (914.4 m)
- 安全设计
- Distributed electric propulsion (DEP) means having multiple propulsors (propellers + drive motors) so that if one or more propulsors fail, the other working propulsors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. 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. The lift-plus-cruise aircraft has no tilting components when transitioning between vertical and forward flight which increases safety by reducing complexity. The tricycle gear also allow the aircraft to land conventionally on a runway or road in emergencies.
全部原始参数
Specifications:
- Aircraft type
- Passenger eVTOL and hybrid-electric VTOL concept design tiltwing aircraft
- Piloting
- 1 pilot
- Capacity
- 3 passengers
- Cruise speed
- 230 mph (370 km/h)
- Cruise altitude
- 3,000 ft (914.4 m)
- Range (all-electric)
- two back-to-back 75 mile (121 km) trips
- Range (hybrid-electric)
- two back-to-back 155 mile (250 km) trips
- Empty weight
- 3,300 lb (1,497 kg) for all-electric variant, 3,882 lb (1,761 kg) for hybrid-electric variant
- Maximum payload weight
- 882 lb (400 kg)
- Maximum takeoff weight
- 6,000 lb (2,721 kg)
- Propellers
- 8 propellers
- Electric motors
- 8 electric motors
- Power source
- battery packs (all-electric) or battery packs + turbo-generator (hybrid-electric)
- Fuselage
- Carbon fiber composite
- Wings
- 1 high main tiltwing (34.65 ft or 10.56 m)
- Tail
- 1 tilting-horizontal stabilizer mounted on two fixed vertical stabilizers, one tilting canard
- Windows
- The windows are similar in size to a general aviation airplane
- Landing gear
- Fixed landing gear, two wheels in the front and one wheel in the rear of the aircraft.
- Safety features
- Distributed electric propulsion (DEP) means having multiple propulsors (propellers + drive motors) so that if one or more propulsors fail, the other working propulsors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. 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. The lift-plus-cruise aircraft has no tilting components when transitioning between vertical and forward flight which increases safety by reducing complexity. The tricycle gear also allow the aircraft to land conventionally on a runway or road in emergencies.