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Joby Aviation · USA
SHy4
Joby Aviation SHy4
矢量推力 · 技术验证机 · 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
- 未公开／未录入
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot
- 航程（按来源口径）
- >500 miles (>804 km) plus reserve power
- 巡航速度
- 未公开／未录入
- 最大速度
- 200 mph (322 km/h)
- 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
- Has a hybrid-electric power source using batteries, liquid hydrogen, fuel cells and has a heat exchanger to cool the fuel cell assembly
- 电机
- 6 high performance electric motors
- 旋翼／螺旋桨
- 6 tilt-props, 4 tilt-propellers tilt vertically including the entire motor nacelle, 2 propellers tilt vertically with a linkage mechanism
- 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 passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.
全部原始参数
Specifications:
- Aircraft type
- Hydrogen eVTOL technology demonstrator aircraft
- Piloting
- 1 pilot
- Maximum speed
- 200 mph (322 km/h)
- Range
- >500 miles (>804 km) plus reserve power
- Maximum payload weight
- 1,000 lb (454 kg)
- Propellers
- 6 tilt-props, 4 tilt-propellers tilt vertically including the entire motor nacelle, 2 propellers tilt vertically with a linkage mechanism
- Motors
- 6 high performance electric motors
- Power source
- Has a hybrid-electric power source using batteries, liquid hydrogen, fuel cells and has a heat exchanger to cool the fuel cell assembly
- Fuselage
- Carbon fiber composite
- Windows
- Large windows allowing forward, left and right visibility
- Wings
- 1 main high gull wing
- Tail
- 1 V tail
- Landing gear
- 1 front fixed landing strut and 2 rear fixed 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 passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.