Fairfield, OH, United States of America

Eugene F Pridgett

This inventor holds 1 USPTO granted patent. Top assignee: General Electric Company. Active years: 2002.


% Patents Active = 100.0

Average Co-Inventor Count = 3.0

ph-index = 1

Forward Citations = 26(Granted Patents)


Company Filing History:


Years Active: 2002

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1 patent (USPTO):Explore Patents

Title: The Innovative Contributions of Eugene F. Pridgett

Introduction

Eugene F. Pridgett is a notable inventor based in Fairfield, OH (US). He has made significant contributions to the field of gas turbine engine technology. His innovative approach has led to the development of a unique method for fabricating combustion chamber liners.

Latest Patents

Eugene F. Pridgett holds 1 patent for his invention titled "Method of making a combustion chamber liner." This patent describes a method for creating an annular liner for the combustion chamber of a gas turbine engine. The design includes a dome with a fuel nozzle for delivering fuel. The method involves forming a metal piece into an annular section that has at least one seam extending axially. The upstream end of the liner is machined to include a registration feature, ensuring proper connection to the combustion chamber dome.

Career Highlights

Eugene has had a distinguished career at General Electric Company, where he has applied his expertise in engineering and innovation. His work has contributed to advancements in gas turbine technology, enhancing efficiency and performance in various applications.

Collaborations

Throughout his career, Eugene has collaborated with talented individuals such as David Bruce Patterson and Christopher K. Nelson. These partnerships have fostered a creative environment that has led to further innovations in their respective fields.

Conclusion

Eugene F. Pridgett's contributions to the field of gas turbine technology exemplify the impact of innovative thinking in engineering. His patent for a combustion chamber liner showcases his commitment to advancing technology and improving performance in gas turbine engines.

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