STATIONARY NON-ROTATING BRUSH SEALS
    7.
    发明申请
    STATIONARY NON-ROTATING BRUSH SEALS 有权
    静止不旋转的刷子密封

    公开(公告)号:US20160032750A1

    公开(公告)日:2016-02-04

    申请号:US14882244

    申请日:2015-10-13

    Abstract: The present disclosure relates to an aircraft brush seal comprising a first brush seal member and a second brush seal member comprising a channel that receives a plurality of interwoven brush fibers. The interwoven brush fibers may be coupled to the first brush seal member and/or may extend into the second brush seal member. The interwoven brush fibers may not couple to the second brush seal member and/or may form an air seal. The air seal may be formed between a first air compartment and a second air compartment.

    Abstract translation: 本公开涉及一种包括第一刷密封构件和第二刷密封构件的飞行器刷密封件,该第二刷密封构件包括容纳多个交织毛刷纤维的通道。 交织毛刷纤维可以联接到第一刷密封构件和/或可以延伸到第二刷密封构件中。 交织毛刷纤维可能不耦合到第二刷密封件和/或可形成空气密封。 空气密封件可以形成在第一空气室和第二空气室之间。

    LINKAGE TO CONTROL AND RESTRAIN FLAP MOVEMENT
    8.
    发明申请
    LINKAGE TO CONTROL AND RESTRAIN FLAP MOVEMENT 有权
    连接控制和限制襟翼运动

    公开(公告)号:US20150053789A1

    公开(公告)日:2015-02-26

    申请号:US14459752

    申请日:2014-08-14

    CPC classification number: F02K1/1207

    Abstract: The present disclosure relates to systems for controlling movement of a divergent flap (24) in an exhaust nozzle (20). A nozzle flap assembly may include a first link (42) pivotably coupled to a divergent flap (24). A second link (40) may be pivotably coupled to the first link and a static portion (44) of the exhaust nozzle. The second link may comprise a bumper (50). The first link may be configured to contact the bumper in response to the divergent flap being in a high thrust mode. The second link may be configured to contact the divergent flap in response to the divergent flap being in a low thrust mode.

    Abstract translation: 本公开涉及用于控制排气喷嘴(20)中的发散片(24)的移动的系统。 喷嘴翼片组件可以包括可枢转地联接到发散片(24)的第一连杆(42)。 第二连杆(40)可以可枢转地联接到第一连杆和排气喷嘴的静止部分(44)。 第二连杆可以包括保险杠(50)。 第一连杆可以被配置为响应于处于高推力模式的发散挡板而接触保险杠。 第二连杆可以被配置为响应于处于低推力模式的发散翼板而接触发散翼片。

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