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Technoplane · France

Mini-Bee Octadecacopter

Technoplane Mini-Bee Octadecacopter

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 plus autopilot technology
航程(按来源口径)
387 km (240 miles)
巡航速度
170 km/h (106 mph)
最大速度
未公开/未录入
最大起飞重量
800 kg (1,764 lb)
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, 1 Rotax 915 iS engine without gearbox and 2 compact axial flux permanent magnet synchronous Emrax 208 twin hexaphase high-voltage electric motors
电机
18 electric motors
旋翼/螺旋桨
18 propellers (4 kW each)
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 of critical components in the sub-systems of the aircraft. There is a whole aircraft emergency parachute that can hold 750 kg (1,653 lb), using a Junkers Profly Magnum 601 or 800 model.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric VTOL passenger multicopter concept design aircraft
Piloting
1 pilot plus autopilot technology
Capacity
1 passenger
Cruise speed
170 km/h (106 mph)
Range
387 km (240 miles)
Maximum payload weight
180 kg (397 lb)
Maximum takeoff weight
800 kg (1,764 lb)
Propellers
18 propellers (4 kW each)
Electric motors
18 electric motors
Power source
Hybrid-electric power source, 1 Rotax 915 iS engine without gearbox and 2 compact axial flux permanent magnet synchronous Emrax 208 twin hexaphase high-voltage electric motors
Maximum power
87.6 kW mechanical
Fuselage
Carbon fiber composite tubular structure or aluminum
Windows
Helicopter type windows for forward, left, right excellent views with a roof over your head
Landing gear
Fixed skid 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 of critical components in the sub-systems of the aircraft. There is a whole aircraft emergency parachute that can hold 750 kg (1,653 lb), using a Junkers Profly Magnum 601 or 800 model.