MITIGATION TECHNIQUES FOR PHOTOVOLTAIC (PV) MODULE INSTALLATION SURFACE ABRASION
    66.
    发明申请
    MITIGATION TECHNIQUES FOR PHOTOVOLTAIC (PV) MODULE INSTALLATION SURFACE ABRASION 审中-公开
    用于光伏(PV)模块安装表面磨损的减缓技术

    公开(公告)号:US20150318426A1

    公开(公告)日:2015-11-05

    申请号:US14266670

    申请日:2014-04-30

    Abstract: Mitigation techniques for photovoltaic (PV) module installation surface abrasion are described. According to one embodiment, a photovoltaic system includes first and second photovoltaic modules, each including a first coupling element (e.g., mounting leg) on a first end and a second coupling element on a second end opposite of the first end. The system also includes a connector assembly including a fastener adapted to engage the first coupling element of the first photovoltaic module with the second coupling element of the second photovoltaic module. The fastener is configured to provide an engagement state that enables movement of the second coupling element of the second photovoltaic module independent of the first photovoltaic module.

    Abstract translation: 描述了光伏(PV)模块安装表面磨损的缓解技术。 根据一个实施例,光伏系统包括第一和第二光伏模块,每个光伏模块包括在第一端上的第一耦合元件(例如,安装支腿)和与第一端相对的第二端上的第二耦合元件。 该系统还包括连接器组件,其包括适于将第一光伏模块的第一耦合元件与第二光伏模块的第二耦合元件接合的紧固件。 紧固件被配置成提供能够独立于第一光伏模块移动第二光伏模块的第二耦合元件的接合状态。

    Landing gear
    67.
    发明授权
    Landing gear 有权
    起落架

    公开(公告)号:US08998129B2

    公开(公告)日:2015-04-07

    申请号:US13574357

    申请日:2011-01-19

    Applicant: Ian Bennett

    Inventor: Ian Bennett

    CPC classification number: B64C25/34 B64C2025/345

    Abstract: Aircraft landing gear including an axle pivotally connected to a bogie beam and a locking device. The locking couples the axle to the bogie beam, and has a movable member and a follower. The movable member is movable between first and second configurations. Movement of the movable member towards the second configuration causes corresponding movement of the follower so as to transfer a steering force to the axle through the follower which causes the axle to rotate in a first direction. With the movable member in the first configuration, the follower is in a first configuration that inhibits the movable member being moved by an external force applied to the axle. With the movable member in the second configuration, the follower in a second configuration that permits the movable member to be moved by an external force applied to the axle.

    Abstract translation: 飞机起落架包括枢转地连接到转向架梁的轴和锁定装置。 锁定将车轴连接到转向架梁,并具有可动构件和从动件。 可移动部件可在第一和第二构造之间移动。 可移动构件朝向第二构造的运动导致从动件的相应运动,以便通过从动件将转向力传递到轴,这使得轴沿第一方向旋转。 在可动构件处于第一构造的情况下,从动件处于第一构造,其阻止可移动构件被施加到车轴的外力移动。 利用第二构造中的可动构件,第二构造中的从动件允许可移动构件通过施加到车轴的外力而移动。

    Bogie stop block
    68.
    发明授权
    Bogie stop block 有权
    转向架停车

    公开(公告)号:US08651417B2

    公开(公告)日:2014-02-18

    申请号:US13503265

    申请日:2010-04-30

    CPC classification number: B64C25/34

    Abstract: An aircraft landing gear assembly includes a bogie beam, a landing gear strut and a stop. The landing gear strut has a first end arranged to be pivotally coupled to an aircraft and a second end pivotally coupled to the bogie beam. The stop is arranged to limit pivotal movement of the bogie beam relative to the landing gear strut The stop includes an elongate member arranged to be deflectable in bending when the bogie beam reaches a pivotal limit.

    Abstract translation: 飞机起落架组件包括转向架梁,起落架支柱和挡块。 起落架支柱具有被布置成枢转地联接到飞行器的第一端和枢转地联接到转向架梁的第二端。 挡块被布置成限制转向架梁相对于起落架支柱的枢转运动。止挡件包括细长构件,其布置成当转向架梁达到枢转极限时可弯曲弯曲。

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