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CarryAll V2000CG

AutoFlight CarryAll V2000CG

复合翼(升力+巡航) · 生产型设计 · 核查 2026-10-01

飞行构型与公司名称

复合翼(升力+巡航)

VFS 原始目录分组:升力+巡航。按目录所述推进方式归类。

核对构型依据 ↗

原始目录分组:升力+巡航

中文名称:峰飞航空 · 原名:AutoFlight

核对中文名称 ↗

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 2/3 · 货运型号 TC 已核实 · 已有型号状态依据

查看状态依据(2024-03-22) ↗订阅本机型报道 RSS →

主要参数

座位/载员
Air cargo only
乘客
未公开/未录入
驾驶方式
Autonomous
航程(按来源口径)
250 km (155 m)
巡航速度
200 km/h (124 mph)
最大速度
未公开/未录入
最大起飞重量
2,000 kg (4,409 lb)
载荷
未公开/未录入
空重
1,600 kg (3,527 lb)
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
电机
13 electric motors
旋翼/螺旋桨
13 propellers (10 VTOL only propellers, 3 pusher propellers)
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.

全部原始参数

Specifications:

Aircraft type
Passenger air cargo eVTOL production aircraft
Piloting
Autonomous
Capacity
Air cargo only
Cruise speed
200 km/h (124 mph)
Range
250 km (155 m)
Empty weight
1,600 kg (3,527 lb)
Maximum payload weight
400 kg (882 lb)
Maximum takeoff weight
2,000 kg (4,409 lb)
Propellers
13 propellers (10 VTOL only propellers, 3 pusher propellers)
Electric motors
13 electric motors
Power source
Battery packs
Fuselage
Carbon fiber composite
Wings
1 canard. 1 high gull wing. 4 booms for VTOL propellers.
Tail
2 downward vertical stabilizers
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.

明确提及本机型的报道

6月16日周二
6月13日周六
6月11日周四
2025年1月27日周一
2024年3月23日周六

目录参数变化记录

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。

公司资料与事件

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。

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