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EHang · China
EH216-F
EHang EH216-F
多旋翼 · 生产型设计 · 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
- 100 L (26.4 gallons) firefighting material (foam or microbial water-based liquid). 6 fire projectiles filled with ABC superfine dry powder. The casing of the projectile is made from an aluminum alloy.
- 乘客
- 未公开／未录入
- 驾驶方式
- Remote control piloting (no pilots or passengers onboard)
- 航程（按来源口径）
- 未公开／未录入
- 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
- 7.33 m (24 ft, 1/2 in)
- 翼展
- 未公开／未录入
- 高度
- 2.2 m (7 ft, 5/8 in)
- 动力来源
- Battery packs
- 电机
- 16 electric motors
- 旋翼／螺旋桨
- 16 propellers
- 续航时间
- 21 minutes
- 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. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.
全部原始参数
Specifications:
- Aircraft type
- Uncrewed firefighting eVTOL multicopter drone production model
- Piloting
- Remote control piloting (no pilots or passengers onboard)
- Capacity
- 100 L (26.4 gallons) firefighting material (foam or microbial water-based liquid). 6 fire projectiles filled with ABC superfine dry powder. The casing of the projectile is made from an aluminum alloy.
- Maximum cruise speed
- 130 km/h (81 mph)
- Flight time
- 21 minutes
- Maximum payload weight
- 220 kg (485 lb)
- Propellers
- 16 propellers
- Electric motors
- 16 electric motors
- Power source
- Battery packs
- Time to charge batteries
- <120 minutes
- Fuselage
- Epoxy carbon fiber composite and aluminum alloy
- Length
- 7.33 m (24 ft, 1/2 in)
- Width
- 5.61 m (18 ft, 2/3 in)
- Height
- 2.2 m (7 ft, 5/8 in)
- Windows
- Helicopter type windows allowing forward, left, right and visibility for excellent views
- Landing gear
- Fixed skid 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. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.