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    • 1. 发明授权
    • Connector assembly for gas turbine engines
    • 燃气轮机发动机连接器总成
    • US06669393B2
    • 2003-12-30
    • US09974194
    • 2001-10-10
    • Jan Christopher Schilling
    • Jan Christopher Schilling
    • F16D910
    • F02C7/32B60G2204/143B60G2204/41B60G2204/4402F02C7/20F05B2260/3011F05D2300/431F16C11/045Y10T403/11Y10T403/17
    • A connector assembly for mounting turbomachinery including a link connector to be coupled to a clevis. The clevis includes a pair of arms and an opening that extends therethrough. The link connector includes a first end that includes an elastomer portion that defines an opening. The connector assembly further includes a support washer having an opening extending therethrough adjacent the link connector elastomer portion, and a fastener inserted through the clevis opening, the support washer opening, and the link connector elastomer opening to couple the link connector and the support washer to the clevis such that the link connector is coupled between the clevis arms by the fastener, and such that the support washer thermally insulates at least a portion of the link connector elastomer portion. At least a portion of the connector assembly being configured to shear when subjected to a predetermined load such that loading induced to the connector assembly is transmitted through the link connector elastomer portion.
    • 一种用于安装涡轮机械的连接器组件,包括要联接到U形夹的连杆连接器。 U形夹包括一对臂和延伸穿过其中的开口。 连杆连接器包括包括限定开口的弹性体部分的第一端。 所述连接器组件还包括支撑垫圈,所述支撑垫圈具有穿过所述连杆连接器弹性体部分延伸穿过的开口,以及通过所述U形夹开口插入的紧固件,所述支撑垫圈开口以及所述连杆连接器弹性体开口, U形夹,使得连杆连接器通过紧固件联接在U形夹臂之间,并且使得支撑垫圈使连接件连接器弹性体部分的至少一部分热绝缘。 连接器组件的至少一部分被配置成在受到预定负载时剪切,使得引导到连接器组件的负载通过连接件连接器弹性体部分传递。