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DreamFly Aerotech · China
DF600 Jinghong
Dreamfly Aerotech DF600 Jinghong
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
- Air cargo
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote, autopilot, autonomous or a combination of the three
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- Unknown
- 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
- Hybrid-electric power source
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 propellers (2 tilt-propellers, 4 VTOL-only 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:
- Aircraft type
- Long-range heavy-lift air cargo hybrid-electric or electric VTOL prototype aircraft
- Piloting
- Remote, autopilot, autonomous or a combination of the three
- Capacity
- Air cargo
- Cruise speed
- Unknown
- Range (electric)
- 150-200 km (62-124 m)
- Range (hybrid-electric)
- 1,000 km (621 m)
- Maximum payload weight
- 1,000 kg (2,205 lb)
- Propellers
- 6 propellers (2 tilt-propellers, 4 VTOL-only propellers)
- Electric motors
- 6 electric motors
- Power source
- Hybrid-electric power source
- Fuselage
- Carbon fiber composite
- Wings
- 1 main high wing
- Tail
- 1 V-tail with a downward vertical stabilizer
- Landing gear
- Fixed skid 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.