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Vehicle Systems, Dynamics and Design Laboratory · USA
LPC-02 DUeVTOL
Auburn University LPC-02 DUeVTOL
升力＋巡航 · 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 or air cargo pod
- 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
- 5,525 lb (2,506 kg)
- 载荷
- 未公开／未录入
- 空重
- 3,128 lb (1,419 kg) for the all-electric variant and 3,673 lb (1,666 kg) for the 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
- The aircraft can be powered by batteries alone or it can be outfitted with a hybrid-electric system using a turbine engine. There are 5 battery packs in both designs. The batteries are sized for a minimum 20% power reserve at the end of the design mission.
- 电机
- 8 electric motors
- 旋翼／螺旋桨
- 8 propellers. 6 VTOL-only propellers and 2 tractor propellers for forward flight.
- 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
- Modular passenger and air cargo eVTOL and hybrid-electric VTOL concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 4 passengers or air cargo pod
- Cruise speed
- 230 mph (370 km/h)
- Cruise altitude
- 3,000 ft (914.4 m)
- Range (batteries only)
- 63 m (101 km)
- Range (hybrid-electric)
- 149 m (240 km)
- Empty weight
- 3,128 lb (1,419 kg) for the all-electric variant and 3,673 lb (1,666 kg) for the hybrid-electric variant
- Maximum payload weight
- 882 lb (400 kg)
- Maximum takeoff weight
- 5,525 lb (2,506 kg)
- Propellers
- 8 propellers. 6 VTOL-only propellers and 2 tractor propellers for forward flight.
- Electric motors
- 8 electric motors
- Power source
- The aircraft can be powered by batteries alone or it can be outfitted with a hybrid-electric system using a turbine engine. There are 5 battery packs in both designs. The batteries are sized for a minimum 20% power reserve at the end of the design mission.
- Fuselage
- Material unknown
- Wing
- 1 canard, 1 high main wing, 33.23 ft (10.13 m) in span
- Tail
- 1 canard (fore), 1 horizontal stabilizer (aft), two vertical stabilizers
- Windows
- Larger windows than a general aviation airplane
- Landing gear
- Fixed quadricycle wheeled landing gear
- 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.