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UASystems SA · Switzerland

eZELOS 300 POC

UASystems eZELOS 300 POC

直升机 · 停研/历史型号 · 核查 2026-10-01

飞行构型与公司名称

直升机

Aircraft type: Hybrid-electric or all-electric proof of concept defunct concept design helicopter

核对构型依据 ↗

原始目录分组:电动旋翼机

中文名称:待核实 · 原名:UASystems SA

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 · 停研/历史型号 · 目录阶段,尚未核实批准状态

查看状态依据 ↗订阅本机型报道 RSS →

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.

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。