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AeroMech Incorporated · USA
AM-20
AeroMech Incorporated AM-20
升力＋巡航 · 阶段未核实 · 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
- None. (The full-scale prototype will hold 1 pilot, 1 passenger and their luggage.)
- 乘客
- 未公开／未录入
- 驾驶方式
- Computer controlled. Prototypes will be flown remotely, piloted or have autonomous piloting.
- 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
- 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
- Battery packs. The design assumes a battery energy density of 250 Wh/kg for performance modeling.
- 电机
- 6 electric motors
- 旋翼／螺旋桨
- 6 propellers. (4 ducted propellers for VTOL flight, 2 pusher tilt-propellers (the pusher propellers tilt for both VTOL and forward flight)
- 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), 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
- Virtual research eVTOL aircraft
- Piloting
- Computer controlled. Prototypes will be flown remotely, piloted or have autonomous piloting.
- Capacity
- None. (The full-scale prototype will hold 1 pilot, 1 passenger and their luggage.)
- Cruise speed (estimated)
- 185 km/h (115 mph)
- Range (estimated)
- 100 km (62 m)
- Flight time (estimated)
- 30 minutes, plus 30 minutes reserve (CTOL mode)
- Maximum altitude (estimated)
- 3,048 m (10,000 ft)
- Empty weight (estimated)
- 680 kg (1,499 lb)
- Maximum payload weight (estimated)
- 200 kg (441 lb)
- Maximum takeoff weight (estimated)
- 880 kg (1940 lb)
- Propellers
- 6 propellers. (4 ducted propellers for VTOL flight, 2 pusher tilt-propellers (the pusher propellers tilt for both VTOL and forward flight)
- Electric motors
- 6 electric motors
- Power source
- Battery packs. The design assumes a battery energy density of 250 Wh/kg for performance modeling.
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Wing
- 1 main high wing
- Tail
- Combination V-tail with a horizontal stabilizer
- Landing gear
- Fixed tricycle wheeled 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.