Strafford, NH, United States of America

Gary F Fowler


 

Average Co-Inventor Count = 2.6

ph-index = 1


Company Filing History:


Years Active: 2020

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3 patents (USPTO):Explore Patents

Title: Gary F Fowler: Innovator in Gas Turbine Technology

Introduction

Gary F Fowler is a notable inventor based in Strafford, NH (US). He has made significant contributions to the field of gas turbine technology, holding a total of 3 patents. His work focuses on enhancing the efficiency and reliability of gas turbine engines.

Latest Patents

One of his latest patents is a stator assembly with a retention clip for gas turbine engines. This innovative stator assembly includes a first shroud that extends about an axis to bound a flow path. The first shroud defines a first shroud opening, and an airfoil has an airfoil body that extends from a first end portion. The first end portion is received in the first shroud opening and defines a retention aperture. A retention clip, which includes a body and at least one locking feature, is designed to limit the movement of the airfoil relative to the first shroud when in the installed position. Another patent also focuses on a stator assembly with a retention clip, emphasizing the importance of the retention clip in maintaining the stability of the airfoil within the gas turbine engine.

Career Highlights

Throughout his career, Gary has worked with prominent companies in the aerospace sector, including United Technologies Corporation and Raytheon Technologies Corporation. His experience in these organizations has allowed him to develop and refine his innovative ideas in gas turbine technology.

Collaborations

Gary has collaborated with several talented individuals in his field, including Brian Barainca and Paul W Baumann. These collaborations have contributed to the advancement of technology in gas turbine engines.

Conclusion

Gary F Fowler is a distinguished inventor whose work in gas turbine technology has led to multiple patents and significant advancements in the industry. His contributions continue to influence the design and functionality of gas turbine engines.

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