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HIEN Aero Technologies Co., LTD. · Japan
HIEN 6
Hien Aero Technologies HIEN 6
升力+巡航 · 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
- 6 passengers and luggage
- 乘客
- 未公开/未录入
- 驾驶方式
- Remote, autopilot, autonomous piloting or artificial intelligence (AI) piloting
- 航程(按来源口径)
- Over 180 km (112 m)
- 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
- 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
- Gas turbine(s) using kerosene (Jet-A1/B). It is unknown how many gas turbine engines are on this aircraft. Future models have the possibility of being designed and sold with an all-electric power source, such as battery packs or hydrogen fuel cells.)
- 电机
- 8 electric motors
- 旋翼/螺旋桨
- 8 propellers (4 propellers for forward flight mounted on booms, 4 propellers for VTOL flight mounted on booms)
- 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) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also 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
- Passenger hybrid-electric VTOL concept design aircraft (that company plans to also future models with an all-electric power source)
- Pilot
- Remote, autopilot, autonomous piloting or artificial intelligence (AI) piloting
- Capacity
- 6 passengers and luggage
- Maximum cruise speed
- ~180 km/h or more (112 mph or more)
- Range
- Over 180 km (112 m)
- Maximum payload weight
- 500 kg (1,102 lb)
- Propellers
- 8 propellers (4 propellers for forward flight mounted on booms, 4 propellers for VTOL flight mounted on booms)
- Electric motors
- 8 electric motors
- Power source
- Gas turbine(s) using kerosene (Jet-A1/B). It is unknown how many gas turbine engines are on this aircraft. Future models have the possibility of being designed and sold with an all-electric power source, such as battery packs or hydrogen fuel cells.)
- Power supply capacity
- 400 kWh
- Fuselage
- Carbon fiber composite
- Size
- 1,000 x 1,600 x 320 cm (~33 X ~52-1/2 X ~10-1/2 ft)
- Windows
- Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above the passenger compartment
- Wings
- 1 high main gull-wing
- Tail
- 1 H-tail
- Landing gear
- Fixed tricycle wheeled landing gear
- Safety features
- Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for its passengers or cargo. There are also 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.