跳到正文
← eVTOL产品

Bell · USA

Nexus 6HX

Bell Nexus 6HX

矢量推力 · 阶段未核实 · 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。

资料覆盖与状态依据

可用性能指标 1/3 · 阶段未核实 · 目录依据 · 目录阶段,尚未核实批准状态

查看状态依据 ↗订阅本机型报道 RSS →

主要参数

座位/载员
4 passengers and luggage
乘客
未公开/未录入
驾驶方式
Piloted until autonomous flying is available
航程(按来源口径)
150 miles (241 km)
巡航速度
未公开/未录入
最大速度
179 mph (288 km/h)
最大起飞重量
6,000 lb (2,720 kg)
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 or all batteries
电机
6 electric motors
旋翼/螺旋桨
6 ducted fans
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.

全部原始参数

Specifications:

Aircraft type
Hybrid-electric VTOL or eVTOL passenger concept design
Piloting
Piloted until autonomous flying is available
Capacity
4 passengers and luggage
Maximum speed
179 mph (288 km/h)
Range
150 miles (241 km)
Maximum takeoff weight
6,000 lb (2,720 kg)
Aircraft footprint
40 ft X 40 ft (12 m X 12 m)
Propellers
6 ducted fans
Electric motors
6 electric motors
Power source
Hybrid-electric or all batteries
Fuselage
Carbon fiber composite
Windows
Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
Wings
2 high stub wings, 8 ft (2.4 m)
Tail
1 T-tail
Landing gear
Fixed quadricycle 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.

明确提及本机型的报道

暂无明确匹配的公开报道;通用或重名型号不会自动关联。

目录参数变化记录

从保存的目录刷新快照比较,资料修改不等于实机性能发生变化。

暂无已保存的版本变化,后续目录刷新将保留快照。