Sikorsky · USA

HEX 2-Rotor Tiltwing

Sikorsky HEX 2-Rotor Tiltwing

倾转机翼 · 技术验证机 · 核查 2026-10-01

飞行构型与公司名称

倾转机翼

Aircraft type: HEX 2-Rotor Tiltwing autonomous hybrid-electric passenger VTOL technology demonstrator aircraft

原始目录分组：矢量推力

中文名称：待核实 · 原名：Sikorsky

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。

可用性能指标 1/3 · 技术验证机 · 目录依据 · 目录阶段，尚未核实批准状态

巡航速度未纳入：单位或条件未能一致解析

座位／载员: Unknown
乘客: 未公开／未录入
驾驶方式: Autonomous (has no pilot optional controls inside the cockpit)
航程（按来源口径）: Over 575 miles (925 km)
巡航速度: Unknown
最大速度: 未公开／未录入
最大起飞重量: 9,000 lb (4,082 kg)
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: 2 electric motors
旋翼／螺旋桨: 2 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.

Aircraft type: HEX 2-Rotor Tiltwing autonomous hybrid-electric passenger VTOL technology demonstrator aircraft
Piloting: Autonomous (has no pilot optional controls inside the cockpit)
Capacity: Unknown
Cruise speed: Unknown
Range: Over 575 miles (925 km)
Maximum takeoff weight: 9,000 lb (4,082 kg)
Propellers: 2 rotors
Electric motors: 2 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.

暂无明确匹配的公开报道；通用或重名型号不会自动关联。

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。