UASystems SA · Switzerland

eZELOS 300 Air Taxi

UASystems eZELOS 300 Air Taxi

电动旋翼机 · 停研／历史型号 · 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: 2 passengers
乘客: 未公开／未录入
驾驶方式: 1 pilot
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: 300 kg (661 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: All-electric or hybrid-electric
电机: Possibly 3 electric motors, all 3 used during flight. 2 for the coaxial rotorblades and 1 for the pusher propeller (If one of the electric motors for the rotorblades fail, the other electric motor is built in 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 or all-electric defunct concept design helicopter air taxi
Piloting: 1 pilot
Capacity: 2 passengers
Cruise speed: Unknown
Maximum payload: 300 kg (661 lb)
Rotorblades: 2 coaxial rotorblades (3 blades per rotorblade)
Pusher propeller: 1 pusher propeller
Electric Motors: Possibly 3 electric motors, all 3 used during flight. 2 for the coaxial rotorblades and 1 for the pusher propeller (If one of the electric motors for the rotorblades fail, the other electric motor is built in for redundancy and will help the helicopter land safely.)
Power source: All-electric or hybrid-electric
Fuselage: Carbon fiber composite
Windows: Standard helicopter windows
Tail boom type: Has rear horizontal stabilizer, on each end of stabilizer has a wingtip fence
Landing gear: Fixed tricycle wheeled landing gear, the rear wheel aerostructure provides lift during forward flight
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.