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Sikorsky · USA
HEX 4-Rotor Tiltwing
Sikorsky HEX 4-Rotor Tiltwing
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
- Unknown
- 乘客
- 未公开／未录入
- 驾驶方式
- Autonomous
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- Unknown
- 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
- Hybrid-electric power source
- 电机
- 4 electric motors
- 旋翼／螺旋桨
- 4 rotors
- 续航时间
- 未公开／未录入
- 飞行高度
- 未公开／未录入
- 安全设计
- There are redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure.
全部原始参数
Specifications:
- Aircraft type
- Autonomous hybrid-electric passenger VTOL 4-rotor tiltwing concept design aircraft
- Piloting
- Autonomous
- Capacity
- Unknown
- Cruise speed
- Unknown
- Propellers
- 4 rotors
- Electric motors
- 4 electric motors
- Power source
- Hybrid-electric power source
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Wings
- 1 high main tiltwing
- Tail
- 1 conventional T-tail
- Landing gear
- Retractable tricycle wheeled landing gear
- Safety features
- There are redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure.