General Electric Company

Chris Robin Bron

William James Sumner

Mary Clarkeson Phillips

Peter Schofield

John David Alaksiewicz

David Edwin Kautzmann

Brian William Marriner

A method and system of evaluating a turbine component comprises obtaining data relating to respective surface conditions at a plurality of different surface locations of the turbine component and calculating the total profile efficiency loss for the turbine component based on the data. Calculating the total profile efficiency of the turbine component may include calculating the local profile efficiency loss percentage for each of the surface conditions at the different surface locations (and/or sub-areas of the different surface locations) and calculating an average of the local profile efficiency loss percentages, each of the local efficiency loss percentages being weighted by respective predetermined weight factors. The turbine component may be a nozzle or a bucket and each of the turbine component's surface locations may be an admission suction surface, an admission pressure surface, a discharge suction surface or a discharge pressure surface.

System and method for evaluating efficiency losses for turbine components

A small particle impingement comparator for surface finishes in excess of 1000 micro-inches standardizes the evaluation of such surface finishes within a turbine steam path. The small particle impingement comparator includes a plurality of sample cells arranged side-by-side in ascending order of roughness from 1190 micro-inches to 6950 micro-inches. With this comparator, users can compare the steam path component surface roughness with the roughness of the plurality of sample cells using a visual and tactile feel comparison.

Small particle impingement comparator and method of determining numerical estimation of a steam path component surface roughness

Growing community of inventors

Springfield, IL, United States of America

Chris Robin Bron