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Delft University of Technology · Netherlands
Aether
Delft University of Technology Aether
倾转旋翼 · 概念设计 · 核查 2026-10-01
飞行构型与公司名称
倾转旋翼
Propellers: 6 tilt-propellers
核对构型依据 ↗原始目录分组：矢量推力
中文名称：待核实 · 原名：Delft University of Technology
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 · 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
- 4 mobile passengers, 2 passengers (with one helper)
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 160 km (100 mph)
- 巡航速度
- 176 km/h (109 mph)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 未公开／未录入
- 载荷
- 未公开／未录入
- 空重
- 未公开／未录入
- 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
- Batteries
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 tilt-propellers
- 续航时间
- 56 minutes
- 飞行高度
- 1,219 m (4,000 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 in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- eVTOL passenger aircraft
- Piloting
- 1 pilot
- Capacity
- 4 mobile passengers, 2 passengers (with one helper)
- Cruise speed
- 176 km/h (109 mph)
- Range
- 160 km (100 mph)
- Flight time
- 56 minutes
- Cruise altitude
- 1,219 m (4,000 ft)
- Propellers
- 6 tilt-propellers
- Electric motors
- 6 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- The aircraft has larger windows, than convention aircraft, for a better passenger experience.
- Wings
- 1 main high wing
- Tail
- Rear T-tail
- Landing gear
- Fixed skid 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 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。