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Aliptera · Canada
APV-1
Aliptera APV-1
矢量推力 · 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
- 未公开／未录入
- 乘客
- 2
- 驾驶方式
- 未公开／未录入
- 航程（按来源口径）
- 480 miles (772 km)
- 巡航速度
- 未公开／未录入
- 最大速度
- (242 mph (210 kts, 389 km/h)
- 最大起飞重量
- 未公开／未录入
- 载荷
- 1,400 lb (635 kg)
- 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
- 未公开／未录入
- 电机
- 未公开／未录入
- 旋翼／螺旋桨
- 1 front horizontal propeller mounted in the fuselage for VTOL flight with shutters which close during forward flight. 1 ducted movable propeller in the rear of the aircraft which tilts horizontally for VTOL flight and then tilts vertically for 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
- 未公开／未录入
全部原始参数
Specifications:
- Aircraft type
- eVTOL and hybrid-electric VTOL
- Passengers
- 2
- Maximum speed
- (242 mph (210 kts, 389 km/h)
- Range
- 480 miles (772 km)
- Maximum payload
- 1,400 lb (635 kg)
- Canopy
- Has a clear canopy allowing the pilot and passenger to see in all directions for spectacular views when flying
- Propellers
- 1 front horizontal propeller mounted in the fuselage for VTOL flight with shutters which close during forward flight. 1 ducted movable propeller in the rear of the aircraft which tilts horizontally for VTOL flight and then tilts vertically for forward flight.
- Wing
- Small canard wing with rear high main wing. The rear wing protrudes from the back of the fuselage with an angled-type wing, with the final horizontal wing above the fuselage.
- Fuselage
- Composite
- Landing gear
- Either skids or wheeled landing gear