Measurement system for adjusting trunnion bearing assemblies for a rotary drum

    公开(公告)号:US11714014B2

    公开(公告)日:2023-08-01

    申请号:US17104597

    申请日:2020-11-25

    Applicant: ANDRITZ INC.

    CPC classification number: G01L5/0023 G01L5/0019

    Abstract: A trunnion roller thrust measurement assembly includes a trunnion roller assembly and a thrust measurement assembly. The trunnion roller assembly includes a roller configured to provide rotary support of a rotary drum; a shaft attached to the roller, the shaft being aligned with an axis of rotation of the roller; and a bearing housing configured support an end of the shaft. The thrust measurement assembly includes a bearing housing end cap attachable to an end of the bearing housing; and one or more thrust sensors disposed on the bearing housing end cap. The one or more thrust sensors are configured to sense a thrust force exerted on the bearing housing end cap by an axial displacement of the shaft. An adjustment mechanism is utilized to skew the roller based on the sensed thrust force.

    MEASUREMENT SYSTEM FOR ADJUSTING TRUNNION BEARING ASSEMBLIES FOR A ROTARY DRUM

    公开(公告)号:US20210156423A1

    公开(公告)日:2021-05-27

    申请号:US17104597

    申请日:2020-11-25

    Applicant: ANDRITZ INC.

    Abstract: A trunnion roller thrust measurement assembly includes a trunnion roller assembly and a thrust measurement assembly. The trunnion roller assembly includes a roller configured to provide rotary support of a rotary drum; a shaft attached to the roller, the shaft being aligned with an axis of rotation of the roller; and a bearing housing configured support an end of the shaft. The thrust measurement assembly includes a bearing housing end cap attachable to an end of the bearing housing; and one or more thrust sensors disposed on the bearing housing end cap. The one or more thrust sensors are configured to sense a thrust force exerted on the bearing housing end cap by an axial displacement of the shaft. An adjustment mechanism is utilized to skew the roller based on the sensed thrust force.

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