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Horizon Aircraft · Canada
Cavorite X7
Horizon Aircraft Cavorite X7
升力＋巡航 · 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
- 6 passengers
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 805 km (500 m)
- 巡航速度
- 未公开／未录入
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 2,495 kg (5,500 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
- 电机
- 17 electric motors
- 旋翼／螺旋桨
- 16 fans (patented fan in wing system), 1 pusher propeller
- 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. If the engine runs out of fuel or some type of mechanical failure occurs with the engine, there is is a battery pack which can continue to power all the electrical systems on the aircraft to land it safely. Also, the aircraft can land conventionally, if there is not enough power in the battery pack for a vertical landing.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric passenger eVTOL concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 6 passengers
- Maximum cruise speed
- 450 km/h (280 mph)
- Range
- 805 km (500 m)
- Empty weight (with fuel)
- 1,815 kg (4,001 lb)
- Maximum payload weight
- 680 kg (1,500 lb)
- Maximum takeoff weight
- 2,495 kg (5,500 lb)
- Propellers
- 16 fans (patented fan in wing system), 1 pusher propeller
- Electric motors
- 17 electric motors
- Power source
- Hybrid-electric power source
- Fuselage
- Carbon fiber composite
- Windows
- The cockpit has a canopy over the cockpit which slides forward for exit and entry. The passenger cabin has gull-wing doors.
- Wings
- Tandem wings
- Tail
- Modified V tail
- 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. If the engine runs out of fuel or some type of mechanical failure occurs with the engine, there is is a battery pack which can continue to power all the electrical systems on the aircraft to land it safely. Also, the aircraft can land conventionally, if there is not enough power in the battery pack for a vertical landing.