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CycloTech GmbH · Austria
CCY-01
CycloTech CCY-01
矢量推力 · 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
- Air cargo
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote or autonomous
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 120 km/h (75 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 280 kg (617 lb)
- 载荷
- 未公开／未录入
- 空重
- 235 kg (518 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
- Battery packs
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 CycloRotors
- 续航时间
- 未公开／未录入
- 飞行高度
- 1,500 m (4,921 ft)
- 安全设计
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- Air cargo eVTOL concept design drone
- Piloting
- Remote or autonomous
- Capacity
- Air cargo
- Cruise speed
- 120 km/h (75 mph)
- Maximum cruise speed
- 130 km/h (81 mph)
- Range (with the maximum payload weight)
- 40 km (25 m)
- Maximum altitude
- 1,500 m (4,921 ft)
- Wind condition flight capabilities
- Can fly in windy conditions of up to 68 km/h (42 mph)
- Empty weight
- 235 kg (518 lb)
- Maximum payload weight
- 45 kg (99 lb)
- Maximum takeoff weight
- 280 kg (617 lb)
- Propellers
- 6 CycloRotors
- Electric motors
- 6 electric motors
- Power source
- Battery packs
- Rotor RPM
- 2,600 rpm
- Overall hover thrust
- 2,750 N
- Maximum overall thrust
- 4,395 N
- Overall hover drive power
- 118 kW
- Maximum overall drive power
- 210 kW
- Fuselage
- Carbon fiber composite
- Size of aircraft
- 2.7 m x 2.5 m (8 ft, 10 in X 8 ft, 2.5 in)
- Landing gear
- Fixed quadricycle strut landing gear
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies of critical components in the sub-systems of the aircraft.