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Transcend Air Corporation · USA
Vy 400R
Transcend Air Vy 400R
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
- 5 passengers and luggage
- 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
- 410 mph (660 km/h)
- 最大速度
- 未公开／未录入
- 最大起飞重量
- 6,900 lb (3,130 kg)
- 载荷
- 2,190 lb (993 kg)
- 空重
- 4,800 lb (2,177 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
- Hybrid-electric power source, using one GE Aviation CT7-8 turboshaft engine (2,500 shp)
- 电机
- 3 electric motors
- 旋翼／螺旋桨
- 3 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
- The aircraft has redundant systems, HUMS (health and usage monitoring), flight into known icing (FIKI) mission protection, fly by wire dual channel, triple modular redundant control system, advanced avionics, autopilot, envelope protection geofencing plus sensors (no flight into terrain or obstacles) and an emergency whole aircraft parachute. The aircraft has been simplified and has no cables, no hydraulics and no fuel lines.
全部原始参数
Specifications:
- Aircraft type
- Long-range hybrid-electric VTOL passenger concept design aircraft
- Piloting
- 1 pilot
- Capacity
- 5 passengers and luggage
- Cruise speed
- 410 mph (660 km/h)
- Range with comfort interior
- 500 m (805 km), with 4 passengers; 370 m (595 km), with 5 passengers
- Range with super light interior
- 610 m (982 km) with 4 passengers; 485 m (781 km), with 5 passengers
- Maximum cruise altitude
- 8,000 ft (2,438 km)
- Maximum operating altitude
- 20,000 ft (6,096 km)
- Empty weight
- 4,800 lb (2,177 kg)
- Maximum payload
- 2,190 lb (993 kg)
- Maximum takeoff weight
- 6,900 lb (3,130 kg)
- Propellers
- 3 propellers
- Electric motors
- 3 electric motors
- Power source
- Hybrid-electric power source, using one GE Aviation CT7-8 turboshaft engine (2,500 shp)
- Fuselage
- Carbon fiber composite
- Windows
- Typical round windows found on conventional small passenger jet aircraft
- Wings
- 1 high main tilt-wing
- Tail
- 1 H-tail
- Landing gear
- Retractable tricycle strut landing gear
- Safety features
- The aircraft has redundant systems, HUMS (health and usage monitoring), flight into known icing (FIKI) mission protection, fly by wire dual channel, triple modular redundant control system, advanced avionics, autopilot, envelope protection geofencing plus sensors (no flight into terrain or obstacles) and an emergency whole aircraft parachute. The aircraft has been simplified and has no cables, no hydraulics and no fuel lines.