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FlyNow Aviation GmbH · Austria
eCopter P1B
FlyNow Aviation eCopter P1B
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
- 1 person plus luggage
- 乘客
- 未公开／未录入
- 驾驶方式
- Automatic flying
- 航程（按来源口径）
- 50 km (31 m)
- 巡航速度
- 未公开／未录入
- 最大速度
- 130 km/h (81 mph)
- 最大起飞重量
- 360 kg (794 lb)
- 载荷
- 未公开／未录入
- 空重
- 240 kg (529 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
- Lithium-ion batteries
- 电机
- 4 electric motors
- 旋翼／螺旋桨
- 未公开／未录入
- 续航时间
- 30 minutes
- 飞行高度
- 150-300 m (492-984 ft)
- 安全设计
- 未公开／未录入
全部原始参数
Specifications:
- Aircraft type
- Passenger all-electric concept design helicopter
- Piloting
- Automatic flying
- Capacity
- 1 person plus luggage
- Maximum speed
- 130 km/h (81 mph)
- Range
- 50 km (31 m)
- Flight time
- 30 minutes
- Cruise altitude
- 150-300 m (492-984 ft)
- Empty weight
- 240 kg (529 lb)
- Maximum payload weight
- 120 kg (265 lb)
- Maximum takeoff weight
- 360 kg (794 lb)
- Rotorblades
- Two coaxial rotor blades
- Electric Motors
- 4 electric motors
- Power source
- Lithium-ion batteries
- Fuselage
- Carbon fiber composite
- Windows
- Large vertical front window allowing forward, left, right, up and down views
- Landing gear
- Fixed skid landing gear
- Safety feature
- The helicopter uses the redundancy of four electric motors, so if one or two fail, it can still safely land. The helicopter will also have collision avoidance systems on board. All critical systems of the helicopter are redundant.