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UASystems SA · Switzerland
eZELOS 300 POC
UASystems eZELOS 300 POC
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
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote
- 航程（按来源口径）
- 750 km (466 miles)
- 巡航速度
- 未公开／未录入
- 最大速度
- 250 km/h (155 mph)
- 最大起飞重量
- 未公开／未录入
- 载荷
- 50 kg (110 lb)
- 空重
- 250 kg (551 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
- Hybrid-electric or all-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
- 30 minutes full electrical, up to 4 hours hybrid-electric
- 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.
全部原始参数
Specifications:
- Aircraft type
- Hybrid-electric or all-electric proof of concept defunct concept design helicopter
- Piloting
- Remote
- Maximum speed
- 250 km/h (155 mph)
- Range
- 750 km (466 miles)
- Flight Time
- 30 minutes full electrical, up to 4 hours hybrid-electric
- Maximum payload
- 50 kg (110 lb)
- Empty weight
- 250 kg (551 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
- Hybrid-electric or all-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
- 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.