← eVTOL产品
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。
资料覆盖与状态依据
可用性能指标 1/3 · 概念设计 · 目录依据 · 目录阶段,尚未核实批准状态
查看状态依据 ↗概念参数,尚不代表已实现性能
订阅本机型报道 RSS →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.
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。