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Alaka'i Technologies · USA

Skai

Alaka'i Technologies Skai

多旋翼 · 概念设计 · 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
4 passengers (In autonomous mode, 5 passengers)
驾驶方式
1 pilot (The aircraft can be manually piloted, remote controlled or provide fully autonomous flight)
航程(按来源口径)
150 miles (241 km)
巡航速度
115 mph (185 km/h)
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
A hybrid-electric power source using hydrogen fuel cells
电机
6 electric motors
旋翼/螺旋桨
6 propellers
续航时间
未公开/未录入
飞行高度
Less than 10,000 ft (3,048 m)
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 its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure. The avionics system is protected against electromagnetic interference. There is a triple-redundant autopilot system that will maintain smooth stable flight. The aircraft has next-generation Automatic Dependent Surveillance Broadcast (ADS-B) system providing tracking, weather data, increased air traffic awareness and reduces the risk of collisions with other aircraft. Key systems include a combination of LIDAR (Light Detection and Ranging) and camera sensors that can detect large and small objects in the vehicle’s path. FAA certified impact-absorbing seats have a 4-point seat belt system to keep passengers as safe and secure as possible. The carbon composite airframe and landing skids are built to flex and reduce the effects of a hard 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
Hybrid-electric passenger VTOL multicopter concept design aircraft
Pilot
1 pilot (The aircraft can be manually piloted, remote controlled or provide fully autonomous flight)
Passengers
4 passengers (In autonomous mode, 5 passengers)
Cruise speed
115 mph (185 km/h)
Range
150 miles (241 km)
Maximum flight time
4 hours
Flight altitude
Less than 10,000 ft (3,048 m)
Propellers
6 propellers
Electric motors
6 electric motors
Power source
A hybrid-electric power source using hydrogen fuel cells
Refueling time
Less than 10 minutes
Windows
Large windows provide spectacular views for the passengers
Landing gear
Fixed skid landing gear
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 its passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy for its passengers or cargo. Having multiple redundant systems on any aircraft decreases having any single point of failure. The avionics system is protected against electromagnetic interference. There is a triple-redundant autopilot system that will maintain smooth stable flight. The aircraft has next-generation Automatic Dependent Surveillance Broadcast (ADS-B) system providing tracking, weather data, increased air traffic awareness and reduces the risk of collisions with other aircraft. Key systems include a combination of LIDAR (Light Detection and Ranging) and camera sensors that can detect large and small objects in the vehicle’s path. FAA certified impact-absorbing seats have a 4-point seat belt system to keep passengers as safe and secure as possible. The carbon composite airframe and landing skids are built to flex and reduce the effects of a hard landing. There is also a whole aircraft emergency ballistic parachute in case of an unexpected inflight emergency.