COMPOSITE COMPRESSOR BLADE AND METHOD OF ASSEMBLING
    2.
    发明申请
    COMPOSITE COMPRESSOR BLADE AND METHOD OF ASSEMBLING 审中-公开
    复合压缩机叶片及组装方法

    公开(公告)号:US20160130955A1

    公开(公告)日:2016-05-12

    申请号:US14893217

    申请日:2014-05-21

    Abstract: Compressor blades constructed of composite materials are disclosed. Some example compressor blades may include a composite blade panel including an airfoil having a span extending radially outward with respect to an axis of rotation and/or a blade attachment feature radially inward from the airfoil with respect to the axis of rotation. The blade attachment feature may be circumferentially oriented with respect to the axis of rotation. The blade attachment feature may be arranged to releasably engage a generally circumferentially oriented spool attachment feature. The spool attachment feature may be generally shaped as a circumferential dovetail slot configured to slidably receive the blade attachment feature therein.

    Abstract translation: 公开了由复合材料构成的压缩机叶片。 一些示例性压缩机叶片可以包括复合叶片面板,其包括具有相对于旋转轴线径向向外延伸的跨度的翼型和/或相对于旋转轴线从翼型件径向向内的叶片附接特征。 叶片附接特征可以相对于旋转轴线沿周向定向。 叶片附接特征可以被布置成可释放地接合大致周向定位的卷轴附接特征。 卷轴附接特征可以通常成形为周向燕尾槽,其构造成可滑动地容纳其中的叶片附接特征。

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