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Technoplane · France

Mini-Bee TR2

Technoplane Mini-Bee TR2

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
1 person who needs an emergency recuse
乘客
未公开/未录入
驾驶方式
1 pilot, 1 crew member
航程(按来源口径)
850 km (528 miles)
巡航速度
200 km/h (124 mph)
最大速度
未公开/未录入
最大起飞重量
1,200 kg (2,646 lb)
载荷
未公开/未录入
空重
850 kg (1,874 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
Hybrid-electric power source, 2 Rotax 915 iS engines and 4 compact axial flux permanent magnet synchronous Emrax 188 twin hexaphase high-voltage electric motors
电机
12 electric motors (according to the team's paper)
旋翼/螺旋桨
10 propellers (4 tilt-wing propellers, 6 VTOL-only propellers)
续航时间
未公开/未录入
飞行高度
1,500 m (4,921 ft)
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.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric VTOL EMS tandem tilt-wing concept design aircraft
Piloting
1 pilot, 1 crew member
Capacity
1 person who needs an emergency recuse
Cruise speed
200 km/h (124 mph)
Maximum cruise speed
240 km/h (149 mph)
Range
850 km (528 miles)
Maximum altitude
1,500 m (4,921 ft)
Empty weight
850 kg (1,874 lb)
Maximum payload weight
350 kg (772 lb)
Maximum takeoff weight
1,200 kg (2,646 lb)
Propellers
10 propellers (4 tilt-wing propellers, 6 VTOL-only propellers)
Electric motors
12 electric motors (according to the team's paper)
Power source
Hybrid-electric power source, 2 Rotax 915 iS engines and 4 compact axial flux permanent magnet synchronous Emrax 188 twin hexaphase high-voltage electric motors
Fuselage
Carbon fiber composite
Window
Canopy over cockpit for excellent views
Wings
Tandem tilt-wings
Landing gear
Retractable 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 of critical components in the sub-systems of the aircraft.