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Coflow Jet, LLC. · USA
CFJ-VTOL
Coflow Jet CFJ-VTOL
矢量推力 · 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 seats
- 乘客
- 未公开／未录入
- 驾驶方式
- Unknown
- 航程（按来源口径）
- 318 miles (512 km)
- 巡航速度
- 115 mph (186 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
- 未公开／未录入
- 空重
- 4,678 lb (2,122 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
- Batteries
- 电机
- 10 electric motors
- 旋翼／螺旋桨
- 10 propellers (stationary forward 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), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft. Can land conventionally if the VTOL systems are not working.
全部原始参数
Specifications:
- Aircraft type
- eVTOL passenger concept design aircraft
- Piloting
- Unknown
- Capacity
- 4 seats
- Cruise speed
- 115 mph (186 km/h)
- Range
- 318 miles (512 km)
- Empty weight
- 4,678 lb (2,122 kg)
- Propellers
- 10 propellers (stationary forward propellers)
- Electric motors
- 10 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- The windows are larger than conventional aircraft allowing forward, left and right views with a solid roof above the passenger compartment
- Wings
- Tandem wings (with coflow technology inside the wings), the wing flaps turn down and uses the coflow technology to provide lift for VTOL flight, flaps return to the horizontal position for forward flight
- Landing gear
- Fixed tricycle wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft. Can land conventionally if the VTOL systems are not working.