General Electric Company

Sheldon Dirk Westwood

James Michael Kostrubanic

John Matthew Sassatelli

Joseph Paul Turley

James Alfred Day

Kurt Neal Laurer

Mark Stephen Clough

Paul Howard Davidson

David Britton Green

Rory Todd Hersom

Francisco Jesus Godines

Troy Eugene Mallory

Ronald Roy Patterson

Michael Wayne Quillin

Christopher Charles Krosky

A method of repairing a diaphragm of a rotary machine includes removing an initial steam path from the diaphragm. The initial steam path includes a plurality of initial partitions. Each initial partition is associated with an original trailing edge profile and an original axial length. The method also includes coupling a replacement steam path to the diaphragm. The replacement steam path includes a plurality of replacement partitions. Each replacement partition has a replacement axial length that is greater than the original axial length.

Method for repair of a diaphragm of a rotary machine

This disclosure describes embodiments of a method of repairing a diaphragm found in a turbine, and a diaphragm assembly resulting from the same, that does not require welds in between the partitions. The method inserts a replacement part in place of certain machine-removed portions of the existing partitions on the diaphragm. The replacement part includes coupons that work in combination with the remaining portions of the partitions to form the aerodynamic shape of the original partitions.

Method for repairing a turbine diaphragm and diaphragm assembly resulting therefrom

A bearing manipulator for supporting and manipulating a bearing is provided. In one embodiment, the bearing manipulator includes a frame having at least one adjustable roller to support the bearing, and at least one adjustable arm to secure the bearing to the frame. The bearing manipulator further includes a motor configured to incrementally rotate the bearing.

Elliptical bearing manipulator

A turbine diaphragm airfoil, a turbine diaphragm assembly employing such an airfoil, and a method of repair are described. In one embodiment, a turbine diaphragm airfoil includes: a composite airfoil body which includes a pressure side and a suction side, the composite airfoil including: a leading edge section forming a portion of each of the pressure side and the suction side; and a trailing edge section integral with the leading edge section, the trailing edge section including: a prefabricated member affixed to the leading edge section, the prefabricated member forming a remainder of the pressure side of the composite airfoil body; and a weld or braze section contacting the leading edge section and the prefabricated member, the weld or braze section forming a remainder of the suction side of the composite airfoil body.

Turbine diaphragm airfoil, diaphragm assembly, and method of repair

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Albany, NY, United States of America

Sheldon Dirk Westwood