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Trek Aerospace, Inc. · USA
DuoTrek 2.0
Trek Aerospace DuoTrek 2.0
多旋翼 · 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
- 1 passenger
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 345 miles (555 km), or more
- 巡航速度
- 115 mph (185 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- ~400 lb (181 kg)
- 空重
- ~800 lb (363 kg)
- 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
- In 2003, the concept design originally had a conventional petroleum engine to power the aircraft with gears and mechanical linkages to drive the propellers. However, in 2011, the propulsion system was redesigned and became a hybrid-electric aircraft. It uses a 200 hp engine to create all the electricity for the aircraft and uses electric motors to turn the propellers.
- 电机
- 2 or 4 electric motors
- 旋翼／螺旋桨
- 2 or 4 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. The aircraft could be outfitted with a whole aircraft ballistic parachute.
全部原始参数
Specifications:
- Aircraft type
- Passenger hybrid-electric VTOL concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 1 passenger
- Cruise speed
- 115 mph (185 km/h)
- Range
- 345 miles (555 km), or more
- Empty weight
- ~800 lb (363 kg)
- Maximum payload
- ~400 lb (181 kg)
- Propellers
- 2 or 4 propellers
- Electric Motors
- 2 or 4 electric motors
- Power source
- In 2003, the concept design originally had a conventional petroleum engine to power the aircraft with gears and mechanical linkages to drive the propellers. However, in 2011, the propulsion system was redesigned and became a hybrid-electric aircraft. It uses a 200 hp engine to create all the electricity for the aircraft and uses electric motors to turn the propellers.
- Fuselage
- Carbon fiber composite
- Windows
- Canopy over cockpit
- Wings
- Front stub wings
- Tail
- Tailplane mounted tail
- Landing gear
- Fixed skid type landing gear
- 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. The aircraft could be outfitted with a whole aircraft ballistic parachute.