UASystems SA · Switzerland

eZELOS C4 Cargo Twin-Hybrid

UASystems eZELOS C4 Cargo Twin-Hybrid

电动旋翼机 · 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: Cargo only
乘客: 未公开／未录入
驾驶方式: Remote or autonomous
航程（按来源口径）: 500+ km (311 m)
巡航速度: 280 km/h (174 mph)
最大速度: 320 km/h (199 mph)
最大起飞重量: 未公开／未录入
载荷: 500+ kg (1,102 lb)
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, piston engines and batteries
电机: 6 electric motors. If one or two of the electric motors for the main rotorblades fail, the other electric motors are built for redundancy and will help the helicopter land safely.
旋翼／螺旋桨: 未公开／未录入
续航时间: 未公开／未录入
飞行高度: 未公开／未录入
安全设计: In case of a power loss, the helicopter can land using autorotation. The company also has redundancy built into the aircraft providing an additional margin of safety.

Aircraft type: Hybrid-electric air cargo concept design helicopter
Piloting: Remote or autonomous
Capacity: Cargo only
Cruise speed: 280 km/h (174 mph)
Maximum speed: 320 km/h (199 mph)
Range: 500+ km (311 m)
Maximum payload: 500+ kg (1,102 lb)
Rotorblades: 2 coaxial rotorblades (4 blades per rotorblade)
Pusher propellers: 2 electric ducted fans (pusher ducted fans)
Electric Motors: 6 electric motors. If one or two of the electric motors for the main rotorblades fail, the other electric motors are built for redundancy and will help the helicopter land safely.
Power source: Hybrid-electric, piston engines and batteries
Fuselage: Carbon fiber composite
Wings: At the lower front of the fuselage, there are stub wings with small winglets
Tail boom type: The helicopter has no tail but there is a small downward facing vertical stabilizer protruding from the rear of the helicopter
Landing gear: Fixed skid landing gear
Safety features: In case of a power loss, the helicopter can land using autorotation. The company also has redundancy built into the aircraft providing an additional margin of safety.