Systems and methods for heat shield assemblies

    公开(公告)号:US09903671B2

    公开(公告)日:2018-02-27

    申请号:US14790832

    申请日:2015-07-02

    CPC classification number: F28F13/00 F16D55/36 F16D65/84

    Abstract: Systems and methods disclosed herein may be useful for aircraft heat shield assemblies. In this regard, a heat shield assembly is provided comprising a heat shield having an aperture, the aperture comprising an end portion and an insertion portion, the insertion portion having a width larger than the end portion, a spacer comprising an upper portion, an undermount flange and a gap between the upper portion and the undermount flange, wherein a surface of the gap is engaged with the heat shield, and wherein the undermount flange has a width less than the insertion portion of the aperture and greater than the width of the end portion.

    SYSTEMS AND METHODS FOR HEAT SHIELD ASSEMBLIES
    6.
    发明申请
    SYSTEMS AND METHODS FOR HEAT SHIELD ASSEMBLIES 有权
    热屏蔽组件的系统和方法

    公开(公告)号:US20150308758A1

    公开(公告)日:2015-10-29

    申请号:US14790832

    申请日:2015-07-02

    CPC classification number: F28F13/00 F16D55/36 F16D65/84

    Abstract: Systems and methods disclosed herein may be useful for aircraft heat shield assemblies. In this regard, a heat shield assembly is provided comprising a heat shield having an aperture, the aperture comprising an end portion and an insertion portion, the insertion portion having a width larger than the end portion, a spacer comprising an upper portion, an undermount flange and a gap between the upper portion and the undermount flange, wherein a surface of the gap is engaged with the heat shield, and wherein the undermount flange has a width less than the insertion portion of the aperture and greater than the width of the end portion.

    Abstract translation: 本文公开的系统和方法可用于飞机防护罩组件。 在这方面,提供一种隔热罩组件,其包括具有孔的隔热罩,所述开口包括端部和插入部分,所述插入部分的宽度大于所述端部部分,所述隔离件包括上部, 凸缘和上部和下部装卸法兰之间的间隙,其中间隙的表面与隔热罩接合,并且其中未装卸法兰具有小于孔的插入部分的宽度并且大于端部的宽度 一部分。

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