SYSTEMS AND METHODS FOR ATTACHING A PROBE TO A CASING OF A GAS TURBINE ENGINE
    6.
    发明申请
    SYSTEMS AND METHODS FOR ATTACHING A PROBE TO A CASING OF A GAS TURBINE ENGINE 有权
    将探测器连接到气体涡轮发动机的系统和方法

    公开(公告)号:US20160084736A1

    公开(公告)日:2016-03-24

    申请号:US14489759

    申请日:2014-09-18

    CPC classification number: G01M15/14 F01D17/02 G01D11/30

    Abstract: A system for attaching a probe to a casing of a gas turbine engine is disclosed. The system may include a probe receptacle attachable to the casing. The probe receptacle may include an internal bore, a bayonet slot, a spring disposed within the internal bore adjacent to the bayonet slot, and a sealing surface within the internal bore. The system also may include a probe attachment assembly disposed about the probe and configured to engage the probe receptacle. The probe attachment assembly may include at least one bayonet positionable within the bayonet slot and a seal positionable adjacent to the sealing surface within the internal bore.

    Abstract translation: 公开了一种用于将探头附接到燃气涡轮发动机的壳体的系统。 该系统可以包括可附接到壳体的探针插座。 探针插座可以包括内孔,卡口槽,布置在邻近卡口槽的内孔内的弹簧以及内孔内的密封表面。 该系统还可以包括围绕探针设置的探测器附接组件,并且被配置成接合探针插座。 探针附接组件可以包括可定位在卡口槽内的至少一个卡口和可在内孔内靠近密封表面定位的密封件。

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