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Odonata GmbH · Germany
Heliplane
Odonata Heliplane
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
- 8 passengers and luggage
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 1,000 km (621 miles)
- 巡航速度
- 280 km/h (174 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
- 1,000 kg (2,205 lb)
- 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
- Hybrid-electric power source using hydrogen fuel cells and hydrogen gas burning turbine engines
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 propellers (4 tilt-prop propellers for forward and VTOL flight and 2 VTOL-only propellers located inside the main high wing with shutters that open during VTOL flight and close during forward flight)
- 续航时间
- 未公开／未录入
- 飞行高度
- 未公开／未录入
- 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
- Hybrid-electric hydrogen fuel cell, gas turbine engine long-range passenger VTOL concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 8 passengers and luggage
- Cruise speed
- 280 km/h (174 mph)
- Range
- 1,000 km (621 miles)
- Maximum cruise altitude
- 3,062 meters (13,000 ft)
- Maximum payload
- 1,000 kg (2,205 lb)
- Propellers
- 6 propellers (4 tilt-prop propellers for forward and VTOL flight and 2 VTOL-only propellers located inside the main high wing with shutters that open during VTOL flight and close during forward flight)
- Electric motors
- 6 electric motors
- Power source
- Hybrid-electric power source using hydrogen fuel cells and hydrogen gas burning turbine engines
- Fuselage
- Carbon fiber composite
- Windows
- Large window over the cockpit with conventional windows for the passengers
- Wings
- 1 main high wing with winglets
- Tail
- 1 inverted V tail
- Landing gear
- 4 retractable landing struts
- 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.