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SeaHorse Air Limited · United Kingdom

SeaHorse H5

SeaHorse Air SeaHorse H5

多旋翼 · 概念设计 · 核查 2026-10-01

飞行构型与公司名称

多旋翼

VFS 原始目录分组:多旋翼。按目录所述推进方式归类。

核对构型依据 ↗

原始目录分组:多旋翼

中文名称:待核实 · 原名:SeaHorse Air Limited

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

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主要参数

座位/载员
4 passengers and luggage
乘客
未公开/未录入
驾驶方式
1 pilot
航程(按来源口径)
360 km (224 m)
巡航速度
80 km/h (50 mph)
最大速度
120 km/h (75 mph)
最大起飞重量
1,200 kg (2,645 lb)
载荷
未公开/未录入
空重
550 kg (1,212 lb)
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
Ethanol (in the future, hydrogen fuel cells or battery packs)
电机
Digital displacement hydraulic transmission technology (in the future, 8 electric motors)
旋翼/螺旋桨
8 propellers (rotor cluster tilt system)
续航时间
3 hours
飞行高度
15 m (49 ft) over water
安全设计
There are redundancies of critical components and 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.

全部原始参数

Specifications:

Aircraft type
Passenger VTOL land and amphibious concept design multicopter
Piloting
1 pilot
Capacity
4 passengers and luggage
Cruise speed
80 km/h (50 mph)
Maximum speed
120 km/h (75 mph)
Range
360 km (224 m)
Flight time
3 hours
Cruise altitude
15 m (49 ft) over water
Empty weight
550 kg (1,212 lb)
Maximum payload weight
650 kg (1,433 lb)
Maximum takeoff weight
1,200 kg (2,645 lb)
Propellers
8 propellers (rotor cluster tilt system)
Electric motors
Digital displacement hydraulic transmission technology (in the future, 8 electric motors)
Power source
Ethanol (in the future, hydrogen fuel cells or battery packs)
Fuselage
Carbon fiber composite, bottom of fuselage is a boat hull shape
Windows
Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
Doors
Gull-wing doors
Landing gear
Fixed tricycle wheeled landing gear. The aircraft can land on the ground or water. The water landing portion of the aircraft has a a boat hull with two sponsons so the aircraft is stable in the water. When landed on the ground, airstairs open from the sponsons allowing passengers to enter and exit the aircraft easily. When in the water, the sponson can deploy a gangway (or boarding ramp) allowing passengers to walk from the aircraft to a dock and back.
Safety features
There are redundancies of critical components and 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.

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。