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Eve Air Mobility, LLC · USA
Eve
Eve Air Mobility Eve
升力＋巡航 · 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
- 4 passengers and luggage (6 passengers in autonomous configuration)
- 乘客
- 未公开／未录入
- 驾驶方式
- 1 pilot (in the future, autonomous)
- 航程（按来源口径）
- 未公开／未录入
- 巡航速度
- Unknown
- 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
- Batteries
- 电机
- 10 electric motors
- 旋翼／螺旋桨
- 10 propellers (8 VTOL-only propellers, 2 pusher propellers)
- 续航时间
- Unknown
- 飞行高度
- Unknown
- 安全设计
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft.
全部原始参数
Specifications:
- Aircraft type
- eVTOL passenger planned production model aircraft
- Piloting
- 1 pilot (in the future, autonomous)
- Capacity
- 4 passengers and luggage (6 passengers in autonomous configuration)
- Cruise speed
- Unknown
- Range (estimated)
- 100 km (60 miles)
- Flight time
- Unknown
- Cruise altitude
- Unknown
- Propellers
- 10 propellers (8 VTOL-only propellers, 2 pusher propellers)
- Electric motors
- 10 electric motors
- Power source
- Batteries
- Fuselage
- Carbon fiber composite
- Windows
- Large windows allowing forward, left, right views with a solid roof above the passenger compartment
- Window
- Canopy over cockpit
- Wings
- 1 main high wing
- Tail
- 1 U tail
- Landing gear
- Fixed skid landing gear (similar to a helicopter fixed skid landing gear)
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. There are also redundancies in the sub-systems of the aircraft.