Eve Air Mobility, LLC · USA

Eve

Eve Air Mobility Eve

升力＋巡航 · 原型机 · 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。

资料覆盖与状态依据

可用性能指标 0/3 · 原型机 · 目录依据 · 目录阶段，尚未核实批准状态

巡航速度未纳入：单位或条件未能一致解析

座位／载员: No passengers
乘客: 未公开／未录入
驾驶方式: Remotely operated
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 (2 electric motors are used for the pusher propeller)
旋翼／螺旋桨: 8 VTOL-only propellers, 1 pusher propeller
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) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. 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. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.

Aircraft type: Full scale eVTOL prototype aircraft
Piloting: Remotely operated
Capacity: No passengers
Cruise speed: Unknown
Propellers: 8 VTOL-only propellers, 1 pusher propeller
Electric motors: 10 electric motors (2 electric motors are used for the pusher propeller)
Power source: Batteries
Fuselage: Carbon fiber composite
Wings: 1 high main wing
Tail: 1 U tail
Landing gear: Fixed skid landing gear
Safety features: Distributed Electric Propulsion (DEP) uses multiple propellers or electric ducted fans, each powered by electric motors, to increase safety through redundancy. If one or more components fail, the remaining ones can still ensure a safe landing. 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. The aircraft has no moving surfaces or tilting parts when transitioning from vertical to forward flight and the reverse which increases safety by reducing complexity.

暂无明确匹配的公开报道；通用或重名型号不会自动关联。

从保存的目录刷新快照比较，资料修改不等于实机性能发生变化。

暂无已保存的版本变化，后续目录刷新将保留快照。

包括公司融资及其他机型进展，请查看原文确认涉及的具体型号。