ELECTRIC VEHICLE POWER DISTRIBUTION SYSTEM
    1.
    发明申请
    ELECTRIC VEHICLE POWER DISTRIBUTION SYSTEM 有权
    电动车配电系统

    公开(公告)号:US20160241028A1

    公开(公告)日:2016-08-18

    申请号:US15046197

    申请日:2016-02-17

    Applicant: Zee.Aero Inc.

    Inventor: Geoffrey A. Long

    Abstract: A power distribution system comprises a plurality of energy storage modules coupled in series. A plurality of electrically isolated power converters are each coupled across one or more of the energy storage modules. When enabled, the power converters provide a low voltage output to an output of the power distribution system. A control system controls the power converters to provide the low voltage output. The control system selectively enables the power converters to balance states of charge of the energy storage modules.

    Abstract translation: 配电系统包括串联耦合的多个能量存储模块。 多个电隔离功率转换器分别耦合在一个或多个能量存储模块上。 当使能时,电源转换器向配电系统的输出端提供低电压输出。 控制系统控制电源转换器提供低电压输出。 控制系统选择性地使能量转换器平衡能量存储模块的充电状态。

    VARIABLE GEOMETRY LIFT FAN MECHANISM
    2.
    发明申请
    VARIABLE GEOMETRY LIFT FAN MECHANISM 有权
    可变几何提升机构

    公开(公告)号:US20150132104A1

    公开(公告)日:2015-05-14

    申请号:US13804527

    申请日:2013-03-14

    Applicant: Zee.Aero Inc.

    Abstract: A vertical takeoff and landing aircraft includes rotors that provide vertical and horizontal thrust. During forward motion, the vertical lift system is inactive. A lift fan mechanism positions the fan blades of the aircraft in a collapsed configuration when the vertical lift system is inactive and positions the fan blades of the aircraft in a deployed configuration when the vertical lift system is active.

    Abstract translation: 垂直起降飞机包括提供垂直和水平推力的转子。 在向前运动期间,垂直升降系统不起作用。 当垂直升降系统处于非活动状态时,升降风扇机构将飞行器的风扇叶片定位在折叠构型中,并且当垂直升降系统处于活动状态时将飞行器的风扇叶片定位在展开配置中。

    Variable geometry lift fan mechanism
    3.
    发明授权
    Variable geometry lift fan mechanism 有权
    可变几何提升风机机构

    公开(公告)号:US09284962B2

    公开(公告)日:2016-03-15

    申请号:US13804527

    申请日:2013-03-14

    Applicant: Zee.Aero Inc.

    Abstract: A vertical takeoff and landing aircraft includes rotors that provide vertical and horizontal thrust. During forward motion, the vertical lift system is inactive. A lift fan mechanism positions the fan blades of the aircraft in a collapsed configuration when the vertical lift system is inactive and positions the fan blades of the aircraft in a deployed configuration when the vertical lift system is active.

    Abstract translation: 垂直起降飞机包括提供垂直和水平推力的转子。 在向前运动期间,垂直升降系统不起作用。 当垂直升降系统处于非活动状态时,升降风扇机构将飞行器的风扇叶片定位在折叠构型中,并且当垂直升降系统处于活动状态时将飞行器的风扇叶片定位在展开配置中。

    PASSIVE DEPLOYMENT MECHANISM FOR LIFT FAN
    4.
    发明申请
    PASSIVE DEPLOYMENT MECHANISM FOR LIFT FAN 有权
    被动部署风机的部署机制

    公开(公告)号:US20150367935A1

    公开(公告)日:2015-12-24

    申请号:US14313680

    申请日:2014-06-24

    Applicant: Zee.Aero Inc.

    Inventor: Geoffrey A. Long

    Abstract: A vertical takeoff and landing aircraft includes rotors that provide vertical and horizontal thrust. During forward motion, the vertical lift system is inactive. A lift fan mechanism positions the fan blades of the aircraft in a collapsed configuration when the vertical lift system is inactive and positions the fan blades of the aircraft in a deployed configuration when the vertical lift system is active.

    Abstract translation: 垂直起降飞机包括提供垂直和水平推力的转子。 在向前运动期间,垂直升降系统不起作用。 当垂直升降系统处于非活动状态时,升降风扇机构将飞行器的风扇叶片定位在折叠构型中,并且当垂直升降系统处于活动状态时将飞行器的风扇叶片定位在展开配置中。

    CENTRIFUGAL DE-CLUTCH
    6.
    发明申请
    CENTRIFUGAL DE-CLUTCH 有权
    离心离合器

    公开(公告)号:US20140318907A1

    公开(公告)日:2014-10-30

    申请号:US14070820

    申请日:2013-11-04

    Applicant: Zee.Aero Inc.

    Inventor: Geoffrey A. Long

    Abstract: A mechanical mechanism is used to prevent a rotor of an aircraft from rotating when the rotor is not in use. The mechanical mechanism disengages when the speed of the rotor exceeds a speed threshold and the mechanism reengages when the speed of the rotor is below the speed threshold.

    Abstract translation: 当转子不使用时,使用机械机构来防止飞行器的转子旋转。 当转子的速度超过速度阈值时,机械机构脱离,并且当转子的速度低于速度阈值时机构重新接通。

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