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Thibault Chatillon (inventor) · France
Le Colibri
Chatillon Le Colibri
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
- 3 persons or air cargo
- 乘客
- 未公开／未录入
- 驾驶方式
- Piloted or autonomous
- 航程（按来源口径）
- 300 km (186 miles)
- 巡航速度
- 250 km/h (155 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 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
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 propellers
- 续航时间
- 未公开／未录入
- 飞行高度
- According to the rules of each country
- 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 passenger concept aircraft
- Piloting
- Piloted or autonomous
- Capacity
- 3 persons or air cargo
- Cruise speed
- 250 km/h (155 mph)
- Range
- 300 km (186 miles)
- Cruise altitude
- According to the rules of each country
- Propellers
- 6 propellers
- Electric motors
- 6 electric motors
- Power source
- Hybrid-electric
- Fuselage
- Carbon fiber composite
- Windows
- Large windows allowing forward, left, right visibility with a solid roof above the passenger compartment
- Wings
- 1 main high wing with winglets
- Tail
- 1 horizontal stabilizer
- 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.