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Limosa Inc. · Canada

LimoConnect V1

Limosa LimoConnect V1

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
6 passengers
乘客
未公开/未录入
驾驶方式
1 pilot (The aircraft will be piloted at first and in the future will be autonomous)
航程(按来源口径)
150 miles (241 km)
巡航速度
200 mph (322 km/h)
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
Batteries
电机
8 electric motors
旋翼/螺旋桨
8 tilt-propellers
续航时间
1 hour
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 in the sub-systems of the aircraft.

全部原始参数

Specifications:

Aircraft type
eVTOL passenger aircraft
Piloting
1 pilot (The aircraft will be piloted at first and in the future will be autonomous)
Capacity
6 passengers
Cruise speed
200 mph (322 km/h)
Range
150 miles (241 km)
Flight Time
1 hour
Maximum payload weight
1,100 lbs (499 kg)
Propellers
8 tilt-propellers
Electric Motors
8 electric motors
Power source
Batteries
Fuselage
Carbon fiber composite
Windows
Larger than standard aircraft panoramic wrap around windows allowing forward, left, right visibility for spectacular views with a solid roof above the passenger compartment
Wings
1 high main gull-wing type wing with winglets
Tail
1 high rear gull-wing type tail
Landing gear
Retractable tricycle wheeled landing gear
Stub wings
2 stub wings are located on the lower portion of each side of the fuselage which hold the rear 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 in the sub-systems of the aircraft.