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Trek Aerospace, Inc. · USA
DuoTrek 1.0
Trek Aerospace DuoTrek 1.0
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 (with side-by-side seating)
- 航程（按来源口径）
- 218 m (350 km)
- 巡航速度
- 100 mph (160 km/h)
- 最大速度
- 150 mph (240 km/h)
- 最大起飞重量
- 1,177 lb (534 kg)
- 载荷
- 未公开／未录入
- 空重
- 675 lb (306 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
- 8 electric motors (20 kW electric motors)
- 旋翼／螺旋桨
- 8 ducted propellers, 42" (1,067 mm)
- 续航时间
- 1-1/2 hours
- 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 has a whole aircraft ballistic parachute.
全部原始参数
Specifications:
- Aircraft type
- Passenger hybrid-electric VTOL concept design aircraft
- Piloting
- 1 pilot (with side-by-side seating)
- Capacity
- 1 passenger
- Cruise speed
- 100 mph (160 km/h)
- Maximum speed
- 150 mph (240 km/h)
- Range
- 218 m (350 km)
- Flight time
- 1-1/2 hours
- Empty weight
- 675 lb (306 kg)
- Maximum payload weight
- 360 lb (163 kg)
- Maximum fuel weight
- 142 lb (64 kg)
- Maximum takeoff weight
- 1,177 lb (534 kg)
- Propellers
- 8 ducted propellers, 42" (1,067 mm)
- Electric Motors
- 8 electric motors (20 kW 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
- Stub wings
- Tail
- T-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 has a whole aircraft ballistic parachute.