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Technoplane · France
Mini-Bee Hexacontacopter
Technoplane Mini-Bee Hexacontacopter
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）
- 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 without gearbox and 2 Emrax 228 twin hexaphase high-voltage motors
- 电机
- 60 electric motors
- 旋翼／螺旋桨
- 60 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 plus autopilot technology
- Capacity
- 1 passenger
- Cruise speed
- 170 km/h (106 mph)
- Range
- 600 km (373 miles)
- Maximum takeoff weight
- 700 kg (1,543 lb)
- Propellers
- 60 propellers
- Electric motors
- 60 electric motors
- Power source
- Hybrid-electric power source, 1 Rotax 915 engine without gearbox and 2 Emrax 228 twin hexaphase high-voltage motors
- Maximum power
- 100 kW mechanical
- Fuselage
- Carbon fiber composite tubular structure
- 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.