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ERC System GmbH · Germany

Charlie

ERC System Charlie

复合翼(升力+巡航) · 概念设计 · 核查 2026-10-01

飞行构型与公司名称

复合翼(升力+巡航)

VFS 原始目录分组:升力+巡航。按目录所述推进方式归类。

核对构型依据 ↗

原始目录分组:升力+巡航

中文名称:待核实 · 原名:ERC System GmbH

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
1 doctor, 1 patient and medical equipment The aircraft can hold two patients if there is less medical equipment on board.
乘客
未公开/未录入
驾驶方式
1 pilot
航程(按来源口径)
190 km (118 m)
巡航速度
200 km/h (124 mph)
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 (will be located in the wings)
电机
10 electric motors
旋翼/螺旋桨
10 propellers (8 VTOL-only propellers on two booms and 2 tractor propellers, for forward flight)
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) 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 passengers or cargo. 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
Emergency medical services (EMS) passenger eVTOL aircraft (concept design)
Piloting
1 pilot
Capacity
1 doctor, 1 patient and medical equipment The aircraft can hold two patients if there is less medical equipment on board.
Cruise speed
200 km/h (124 mph)
Range
190 km (118 m)
Maximum payload weight
450 kg (990 lb)
Propellers
10 propellers (8 VTOL-only propellers on two booms and 2 tractor propellers, for forward flight)
Electric motors
10 electric motors
Power source
Batteries (will be located in the wings)
Fuselage
Carbon fiber composite, cabin volume of 5.2 cubic meters (184 cubic feet), the rear door will have dimensions of 1.4 meters by 1.4 meters (4 feet 7 inches)
Windows
Panoramic wrap around windows allowing forward, left and right visibility for excellent views for the pilot with a solid roof above the passenger compartment
Doors
2 doors for the cockpit and 1 rear door for the patient
Wings
1 high main wing and 2 booms for propellers
Tail
1 high boom tail
Landing gear
Tricycle wheeled landing gear
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 passengers or cargo. 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

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。