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Banlan Aviation Technology Company · China

ET-C22

Banlan Aviation Technology Company ET-C22

多旋翼 · 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)
34 km (21 m)
巡航速度
Unknown
最大速度
未公开/未录入
最大起飞重量
150 kg (331 lb)
载荷
未公开/未录入
空重
100 kg (220 lb)
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
2 electric motors
旋翼/螺旋桨
2 propellers
续航时间
30 minutes
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
Passenger eVTOL multicopter prototype aircraft
Piloting
Remote, autopilot, autonomous or a combination of the three
Capacity
Air cargo
Cruise speed
Unknown
Range
34 km (21 m)
Flight time
30 minutes
Maximum cruise altitude
3,000 m (9,843 ft)
Empty weight
100 kg (220 lb)
Maximum payload weight
50 kg (110 lb)
Maximum takeoff weight
150 kg (331 lb)
Propellers
2 propellers
Electric motors
2 electric motors
Power source
Batteries
Fuselage
Unknown (A production aircraft would probably be made from carbon fiber composite material)
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.