Prime Design Consultancy Services · India

Haricopter X1-Q

Prime Design Consultancy Services Haricopter X1-Q

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: 4 passengers
乘客: 未公开／未录入
驾驶方式: Autonomous
航程（按来源口径）: Long distance
巡航速度: Unknown
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 power source
电机: 5 electric motors
旋翼／螺旋桨: 4 VTOL propellers and 1 front 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) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.

Aircraft type: Hybrid-electric VTOL concept design aircraft car carrier
Piloting: Autonomous
Capacity: 4 passengers
Cruise speed: Unknown
Range: Long distance
Propellers: 4 VTOL propellers and 1 front propeller
Electric Motors: 5 electric motors
Power source: Hybrid-electric power source
Cabin: An all clear cabin, with an entry way for a small car to enter in the rear of the aircraft
Fuselage: Carbon fiber composite
Landing gear: Skid type landing gear
Safety features: Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.