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Teching Aviation Technologies Co., Ltd. · China
Dragonfly-EV2000
Teching Aviation Technologies Dragonfly-EV2000
矢量推力 · 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
- 3 passengers
- 乘客
- 未公开/未录入
- 驾驶方式
- 1 pilot
- 航程(按来源口径)
- 200 km (124 m)
- 巡航速度
- ~180-250 km/h (~112-155 mph)
- 最大速度
- 未公开/未录入
- 最大起飞重量
- 未公开/未录入
- 载荷
- 未公开/未录入
- 空重
- 未公开/未录入
- 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
- 4 electric motors
- 旋翼/螺旋桨
- 4 tilt-ducted 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 (Estimated specifications for the planned full-scale production model):
- Aircraft type
- Passenger eVTOL full-scale production aircraft
- Piloting
- 1 pilot
- Capacity
- 3 passengers
- Cruise speed
- ~180-250 km/h (~112-155 mph)
- Range
- 200 km (124 m)
- Maximum payload weight
- 360 kg (794 lb)
- Propellers
- 4 tilt-ducted propellers
- Electric motors
- 4 electric motors
- Power source
- Battery packs
- Windows
- Panoramic wrap around windows allowing forward, left and right visibility for spectacular views for the passengers
- Fuselage
- Carbon fiber composite
- Wings
- 1 low canard, 1 high main wing (tandem wings)
- Tail
- 1 V-tail
- Landing gear
- Unknown. (The subscale prototype has fixed quadricycle wheeled 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.
Specifications (for the subscale prototype):
- Aircraft type
- eVTOL subscale prototype
- Piloting
- Remote
- Cruise speed
- Unknown
- Propellers
- 4 tilt-duct propellers
- Electric motors
- 4 electric motors
- Power source
- Battery packs
- Fuselage
- Unknown
- Wings
- Tandem wings
- Tail
- V tail
- Landing gear
- Fixed wheeled quadricycle 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.