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Vehicle Systems, Dynamics and Design Laboratory · USA

Hexa-Chakra Personal Air Vehicle

Auburn University Hexa-Chakra Personal Air Vehicle

多旋翼 · 概念设计 · 核查 2026-10-01

飞行构型与公司名称

多旋翼

VFS 原始目录分组:个人飞行器。按目录所述推进方式归类。

核对构型依据 ↗

原始目录分组:个人飞行器 · 个人飞行器属于产品形态,构型另行识别。

中文名称:待核实 · 原名:Vehicle Systems, Dynamics and Design Laboratory

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 1/3 · 概念设计 · 目录依据 · 目录阶段,尚未核实批准状态

查看状态依据 ↗

概念参数,尚不代表已实现性能

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主要参数

座位/载员
未公开/未录入
乘客
未公开/未录入
驾驶方式
1 pilot
航程(按来源口径)
未公开/未录入
巡航速度
60 mph (97 km/h)
最大速度
未公开/未录入
最大起飞重量
547 lb (249 kg)
载荷
未公开/未录入
空重
347 lb (158 kg)
长度
5.54 ft (1.69 m)
翼展
未公开/未录入
高度
4.87 ft (1.48 m)
动力来源
Lithium polymer batteries (3 of these batteries)
电机
6 electric motors
旋翼/螺旋桨
6 ducted propellers
续航时间
24 minutes plus a 10 minute reserve
飞行高度
未公开/未录入
安全设计
Distributed electric propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. 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. The racing seat has safety harnesses and an interface for a head and neck safety (HANS) device. There is a roll bar to protect the pilot in case the multicopter rolls over during takeoff or landing. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.

全部原始参数

Specifications:

Aircraft type
Passenger eVTOL multicopter concept design aircraft
Piloting
1 pilot
Cruise speed
60 mph (97 km/h)
Flight time
24 minutes plus a 10 minute reserve
Empty weight
347 lb (158 kg)
Maximum payload weight
200 lb (91 kg)
Maximum takeoff weight
547 lb (249 kg)
Propellers
6 ducted propellers
Electric motors
6 electric motors
Power source
Lithium polymer batteries (3 of these batteries)
Fuselage
Aircraft aluminum and other materials
Length
5.54 ft (1.69 m)
Width
4.64 ft (1.41 m)
Height
4.87 ft (1.48 m)
Cockpit
Open cockpit with a Tillett B7 racing seat with safety harnesses and an interface for a Head and Neck Safety (HANS) device
Landing gear
Fixed tricycle wheeled landing gear. The nose gear is steerable and the rear wheels have brakes.
Safety features
Distributed electric propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. 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. The racing seat has safety harnesses and an interface for a head and neck safety (HANS) device. There is a roll bar to protect the pilot in case the multicopter rolls over during takeoff or landing. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.

明确提及本机型的报道

暂无明确匹配的公开报道;通用或重名型号不会自动关联。

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。