General Electric Company

Craig Daniel Ivancic

Edward John Sharrow

Edward Jay Cooper

Xiaoqing Zheng

Sean Cornelius O'Meara

William Patrick Rusch

Timothy Andrew Melsert

James Wilson Clark

Hemanth A Kumar

David Montgomery Ritz

Peter John Eizenzopf

Jean-francois Lavie

Rotor support structures for industrial machines are disclosed. The support structures may include a rigid base component including a top portion, a slide plate positioned above the rigid base component, and a bearing housing for a rotor, coupled to the slide plate. The bearing housing and the slide plate may be configured to slide or move over the rigid base component. The support structure may also include a plurality of retention blocks coupled to the bearing housing. Each of the plurality of retention blocks may include a moveable retention pin positioned through each of the plurality of retention blocks. The axial movement of the bearing housing and slide plate may compensate for thermal expansion of a turbine shell and/or may reduce vibrations of the rotor and bearing housing during operation of the industrial machines.

Support structures for rotors

A standard for supporting a turbine rotor and a turbine shell includes a bearing block including a housing enclosing bearing surfaces engageable by the turbine rotor. Turbine shell-arm supports are located on opposite sides of the housing, the turbine shell-arm supports each having a horizontal and one or more vertical surfaces adapted to be engaged by support arms of a turbine shell enclosing at least a portion of the turbine. An internal cooling/heating circuit is arranged to simultaneously cool or heat the bearing block and the turbine shell-arm supports to thereby reduce differential thermal growth characteristics of the turbine rotor and turbine shell.

Cooling circuit for reducing thermal growth differential of turbine rotor and shell supports

Embodiments include a system having a turbine support key having a set of key segments selectively stackable together in a plurality of combinations to adjust a thickness between turbine supports based solely on a selection of the key segments from the set.

System and method for aligning turbine components

Growing community of inventors

Gloversville, NY, United States of America

Craig Daniel Ivancic