跳到正文
← eVTOL产品

Doroni Aerospace · USA

H1-X

Doroni Aerospace H1-X

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。

资料覆盖与状态依据

可用性能指标 2/3 · 概念设计 · 目录依据 · 目录阶段,尚未核实批准状态

查看状态依据 ↗

概念参数,尚不代表已实现性能

订阅本机型报道 RSS →

主要参数

座位/载员
1 passenger
乘客
未公开/未录入
驾驶方式
1 pilot, intuitive joystick, takeoff and land push button feature, autonomous navigation system with 360 degree anti-collision capability, is capable of remotely piloted flight,
航程(按来源口径)
60 m (97 km)
巡航速度
95 mph (153 km/h)
最大速度
未公开/未录入
最大起飞重量
2,350 lb (1,066 kg)
载荷
未公开/未录入
空重
1,850 lb (839 kg)
长度
未公开/未录入
翼展
18.2 ft (5.5 m)
高度
未公开/未录入
动力来源
Battery packs
电机
10 electric motors
旋翼/螺旋桨
8 VTOL-only ducted propellers, 2 electric ducted fans for forward flight
续航时间
45 minutes
飞行高度
未公开/未录入
安全设计
Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.

全部原始参数

Specifications:

Aircraft type
Passenger eVTOL aircraft (concept design)
Piloting
1 pilot, intuitive joystick, takeoff and land push button feature, autonomous navigation system with 360 degree anti-collision capability, is capable of remotely piloted flight,
Capacity
1 passenger
Cruise speed
95 mph (153 km/h)
Maximum cruise speed
120 mph (193 km/h)
Range
60 m (97 km)
Flight time
45 minutes
Empty weight
1,850 lb (839 kg)
Maximum payload weight
500 lb (227 kg)
Maximum takeoff weight
2,350 lb (1,066 kg)
Propellers
8 VTOL-only ducted propellers, 2 electric ducted fans for forward flight
Electric motors
10 electric motors
Power source
Battery packs
Fuselage
Carbon fiber composite
Window
Canopy over cockpit
Wings
Tandem wings
Wing span
18.2 ft (5.5 m)
Landing gear
Fixed tricycle wheeled landing gear with the rear struts
Safety features
Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.

明确提及本机型的报道

8月8日周六
6月11日周四
6月9日周二
4月9日周四
4月1日周三
2024年3月5日周二
2024年3月2日周六

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。