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PteroDynamics Inc. · USA
Transwing
PteroDynamics Transwing
矢量推力 · 阶段未核实 · 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
- The aircraft is scalable and passenger capacity can vary
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- 未公开／未录入
- 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
- Scalable weighing between 3 lb (1.36 kg) to 75,000 lb (34,019 kg)
- 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
- 4 or 6 electric motors
- 旋翼／螺旋桨
- 4 or 6 propellers
- 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
- Long range hybrid-electric VTOL or eVTOL passenger concept design aircraft
- Piloting
- 1 pilot
- Capacity
- The aircraft is scalable and passenger capacity can vary
- Empty weight
- Scalable weighing between 3 lb (1.36 kg) to 75,000 lb (34,019 kg)
- Propellers
- 4 or 6 propellers
- Electric motors
- 4 or 6 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Wings
- Scalable from 4 ft (1.21 m) to 34 ft (10.36 m)
- Tail
- 1 inverted angled vertical stabilizer
- Landing gear
- Retractable wheeled landing gear (located on the ends of the propeller nacelles)
- 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.