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Technoplane · France

Mini-Bee Hexatriacontacopter

Technoplane Mini-Bee Hexatriacontacopter

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 and is planned in the future to be an autonomous piloting
航程(按来源口径)
600 km (373 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
700 kg (1,543 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 engine powering a T-Motor engine U12KV120 (or U13)
电机
36 electric motors
旋翼/螺旋桨
36 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 of critical components in the sub-systems of the aircraft. The aircraft has anti-crash seats and an anti-crash superstructure. There is a whole aircraft emergency parachute.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric VTOL passenger multicopter concept design aircraft
Piloting
1 pilot and is planned in the future to be an autonomous piloting
Capacity
1 passenger
Cruise speed
170 km/h (106 mph)
Range
600 km (373 miles)
Maximum takeoff weight
700 kg (1,543 lb)
Propellers
36 propellers
Electric motors
36 electric motors
Power source
Hybrid-electric power source, 1 Rotax 915 engine powering a T-Motor engine U12KV120 (or U13)
Fuselage
Carbon fiber composite tubular structure or aluminum
Windows
Helicopter type windows allowing forward, left and right visibility for spectacular views with a solid roof above the cockpit
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. The aircraft has anti-crash seats and an anti-crash superstructure. There is a whole aircraft emergency parachute.