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海鸥飞行汽车 · Guangdong Seagull Flying Car Group · China

Eagle-350-HQ

Guangdong Seagull Flying Car Group Eagle-350-HQ

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:海鸥飞行汽车 · 原名:Guangdong Seagull Flying Car Group

核对中文名称 ↗

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 0/3 · 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 ↗

巡航速度未纳入:单位或条件未能一致解析

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
Heavy-lift air cargo
乘客
未公开/未录入
驾驶方式
Autonomous piloting
航程(按来源口径)
未公开/未录入
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
Battery packs
电机
12 electric motors
旋翼/螺旋桨
12 propellers (stacked)
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. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.

全部原始参数

Specifications:

Aircraft type
Heavy-lift autonomous air cargo eVTOL concept design drone
Piloting
Autonomous piloting
Capacity
Heavy-lift air cargo
Cruise speed
Unknown
Maximum payload weight
~200 kg (441 lb) or more
Propellers
12 propellers (stacked)
Electric motors
12 electric motors
Power source
Battery packs
Fuselage
Carbon fiber composite
Landing gear
Lands on the bottom of its air cargo container or its fuselage
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. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.

明确提及本机型的报道

2025年1月6日周一

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。