Phoenix, AZ, United States of America

Art Payne



Average Co-Inventor Count = 5.0

ph-index = 2

Forward Citations = 22(Granted Patents)


Company Filing History:


Years Active: 2015-2016

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2 patents (USPTO):Explore Patents

Title: The Innovations of Art Payne: A Pioneer in Turbine Engine Technology

Introduction

Art Payne is an esteemed inventor based in Phoenix, AZ, who has made significant contributions to the field of turbine engine technology. With a total of two patents registered, Payne is recognized for his expertise in developing advanced combustor designs that enhance the efficiency and performance of gas turbine engines.

Latest Patents

Art Payne's latest patents focus on innovative combustors that utilize effusion and impingement cooling methods. One notable patent details a combustor for turbine engines that features an annular liner portion equipped with a unique cold-side metering hole and an impingement chamber. This innovative design allows for efficient cooling by directing airflow onto the hot side annular surface, ensuring optimal combustion performance. The specifications include a carefully calculated ratio of the annular liner's radial thickness to the entry hole's diameter, which ranges from about 2 to about 6.

Another significant patent addresses combustors with quench inserts, designed to improve combustion chamber dynamics. This combustor includes a well-structured arrangement of liners and inserts that facilitate the effective capture and retention of air-fuel mixtures, promoting more efficient combustion processes.

Career Highlights

Art Payne has dedicated his career to advancing turbine engine technologies while working for Honeywell International Inc. His experience in the industry has enabled him to develop groundbreaking solutions that contribute to the efficiency and safety of turbine engines. With his two patents, Payne has established himself as a key figure in the engineering and aviation sectors.

Collaborations

Throughout his career, Art Payne has collaborated with notable peers, including Nagaraja S Rudrapatna and Daniel Ludwig. These professional relationships have fostered a collaborative environment that enhanced his innovation efforts and led to the development of advanced technologies within the field of turbine engines.

Conclusion

In summary, Art Payne's work exemplifies the spirit of innovation in turbine engine technology. His patents on combustor designs demonstrate a commitment to improving efficiency and performance within the aviation industry. As he continues his work at Honeywell International Inc., Payne remains an influential figure whose contributions significantly impact aerospace engineering.

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