AIRCRAFT BRAKE ASSEMBLY
    1.
    发明申请
    AIRCRAFT BRAKE ASSEMBLY 有权
    飞机制动总成

    公开(公告)号:US20150136902A1

    公开(公告)日:2015-05-21

    申请号:US14401886

    申请日:2013-04-15

    IPC分类号: B64C25/36 B64C25/62 B64C25/42

    摘要: An aircraft brake assembly comprising a support leg, a main wheel rotatably mounted on the support leg, a brake comprising a first sub-assembly fixed to the main wheel and a second sub-assembly moveably mounted on the support leg and a ground reaction wheel coupled to the second sub-assembly, wherein on application of the brake, the first sub-assembly engages with the second sub-assembly to exert a braking force on the second sub-assembly; and wherein the ground reaction wheel is arranged to transfer the braking force from the second sub-assembly to the ground.

    摘要翻译: 一种飞机制动组件,包括支撑腿,可旋转地安装在支撑腿上的主轮,制动器,其包括固定到主轮的第一子组件和可移动地安装在支撑腿上的第二子组件, 第二子组件,其中在施加制动器时,第一子组件与第二子组件接合以在第二子组件上施加制动力; 并且其中所述接地反作用轮被布置成将所述制动力从所述第二子组件传递到地面。

    Shock Absorber
    2.
    发明申请
    Shock Absorber 审中-公开
    减震器

    公开(公告)号:US20170016502A1

    公开(公告)日:2017-01-19

    申请号:US15200190

    申请日:2016-07-01

    IPC分类号: F16F6/00 B64C25/58

    CPC分类号: F16F6/005 B64C25/58 F16F9/366

    摘要: A magnetic shock absorber having a first body slidably coupled to a second body via a first bearing arranged to move in sliding engagement with a first counter-face portion. A first array of magnets associated with the first body is arranged to magnetically interact with a second array of magnets associated with the second body to absorb compression or extension loads applied to the shock absorber. The first bearing and the first counter-face portion each have a non-circular cross section profile to inhibit axial relative rotation between the bodies.

    摘要翻译: 一种磁性减震器,其具有经由布置成与第一相对面部分滑动接合的第一轴承可滑动地联接到第二主体的第一主体。 与第一主体相关联的第一磁体阵列布置成与与第二主体相关联的第二磁体阵列磁性地相互作用以吸收施加到减震器的压缩或延伸负载。 第一轴承和第一相对面部分各自具有非圆形横截面轮廓,以阻止主体之间的轴向相对旋转。

    METHOD OF PRELOADING AN AIRCRAFT ASSEMBLY, A PRELOADING TOOL AND AN AIRCRAFT ASSEMBLY
    3.
    发明申请
    METHOD OF PRELOADING AN AIRCRAFT ASSEMBLY, A PRELOADING TOOL AND AN AIRCRAFT ASSEMBLY 审中-公开
    推进飞机装配的方法,推进工具和飞机装配

    公开(公告)号:US20160375989A1

    公开(公告)日:2016-12-29

    申请号:US15190335

    申请日:2016-06-23

    IPC分类号: B64C25/10

    摘要: A method of preloading an aircraft assembly involving a step of operating an extendible preloading tool to move a landing gear strut to decrease the distance between first and second link attachment joints for attachment of a preloading linkage. A tool and aircraft assembly are also provided.

    摘要翻译: 一种预加载飞行器组件的方法,包括操作可延伸的预加载工具以移动起落架支柱的步骤,以减小第一和第二连杆附接接头之间的距离,以连接预加载连杆。 还提供工具和飞机组件。

    Aircraft brake assembly
    4.
    发明授权
    Aircraft brake assembly 有权
    飞机制动总成

    公开(公告)号:US09440733B2

    公开(公告)日:2016-09-13

    申请号:US14401886

    申请日:2013-04-15

    摘要: An aircraft brake assembly comprising a support leg, a main wheel rotatably mounted on the support leg, a brake comprising a first sub-assembly fixed to the main wheel and a second sub-assembly moveably mounted on the support leg and a ground reaction wheel coupled to the second sub-assembly, wherein on application of the brake, the first sub-assembly engages with the second sub-assembly to exert a braking force on the second sub-assembly; and wherein the ground reaction wheel is arranged to transfer the braking force from the second sub-assembly to the ground.

    摘要翻译: 一种飞机制动组件,包括支撑腿,可旋转地安装在支撑腿上的主轮,制动器,其包括固定到主轮的第一子组件和可移动地安装在支撑腿上的第二子组件, 第二子组件,其中在施加制动器时,第一子组件与第二子组件接合以在第二子组件上施加制动力; 并且其中所述接地反作用轮被布置成将所述制动力从所述第二子组件传递到地面。

    Landing gear fairing
    5.
    发明授权
    Landing gear fairing 有权
    起落架整流罩

    公开(公告)号:US09346538B2

    公开(公告)日:2016-05-24

    申请号:US14377018

    申请日:2013-01-23

    IPC分类号: B64C25/00 B64C25/16 B64C25/32

    摘要: An aircraft landing gear including wheels and a fairing arranged to be moveable between a first and a second configuration, wherein in the first configuration the fairing is arranged to shield an element of the landing gear from incident airflow and wherein in the second configuration the fairing is arranged to deflect debris or spray propelled from one or more of the wheels.

    摘要翻译: 一种包括轮和整流罩的飞行器起落架,其布置成可在第一和第二构造之间移动,其中在第一构造中,整流罩布置成将起落架的元件与入射气流屏蔽,并且其中在第二构造中, 布置成偏转碎片或从一个或多个轮子推进的喷雾。

    LANDING GEAR FAIRING
    6.
    发明申请
    LANDING GEAR FAIRING 有权
    起落架齿轮传动

    公开(公告)号:US20150083857A1

    公开(公告)日:2015-03-26

    申请号:US14377018

    申请日:2013-01-23

    IPC分类号: B64C25/16

    摘要: An aircraft landing gear including wheels and a fairing arranged to be moveable between a first and a second configuration, wherein in the first configuration the fairing is arranged to shield an element of the landing gear from incident airflow and wherein in the second configuration the fairing is arranged to deflect debris or spray propelled from one or more of the wheels.

    摘要翻译: 一种包括轮和整流罩的飞行器起落架,其布置成可在第一和第二构造之间移动,其中在第一构造中,整流罩布置成将起落架的元件与入射气流屏蔽,并且其中在第二构造中, 布置成偏转碎片或从一个或多个轮子推进的喷雾。