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Thibault Chatillon (inventor) · France
Tritan Jet TQ
Chatillon Tritan Jet TQ
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
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot and can be flown autonomously
- 航程（按来源口径）
- 400 km (248 miles)
- 巡航速度
- 400 km/h (248 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
- 4 electric motors
- 旋翼／螺旋桨
- 4 electric ducted fans
- 续航时间
- 未公开／未录入
- 飞行高度
- The cruise altitude will be determined according to the rules of the 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 design aircraft
- Piloting
- 1 pilot and can be flown autonomously
- Cruise speed
- 400 km/h (248 mph)
- Range
- 400 km (248 miles)
- Cruise altitude
- The cruise altitude will be determined according to the rules of the country
- Propellers
- 4 electric ducted fans
- Electric motors
- 4 electric motors
- Power source
- Hybrid-electric
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Wings
- Two independently tilting tandem wings
- Landing gear
- Retractable 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.