Steven R Bissell

Title: The Innovations of Steven R Bissell

Introduction

Steven R Bissell is an accomplished inventor based in Andover, Connecticut. He has made significant contributions to the field of engineering, particularly in the area of gas turbine engine components. His innovative approach has led to the development of a unique heat treating apparatus that enhances the durability and performance of these critical components.

Latest Patents

Bissell holds a patent for a "Heat treating apparatus and method of using same." This invention involves an apparatus and method for heat treating the welded area of a repaired gas turbine engine component. The design utilizes first and second heating elements, each consisting of an insulating tube supported by a support rod and wrapped with conducting wire. One heating element is specifically sized to fit inside a recess in the gas turbine engine component, adjacent to the welded area, while the second heating element is positioned outside the recess, also adjacent to the welded area. This dual heating approach effectively treats the welded area from two sides, improving the overall integrity of the component.

Career Highlights

Bissell is associated with United Technologies Corporation, where he has applied his expertise in engineering and innovation. His work has not only contributed to the advancement of gas turbine technology but has also positioned him as a key figure in the field of aerospace engineering.

Collaborations

Throughout his career, Bissell has collaborated with notable colleagues, including Thomas DeMichael and Michael J Labbe. These partnerships have fostered a creative environment that encourages the exchange of ideas and the development of groundbreaking technologies.

Conclusion

Steven R Bissell's contributions to the field of engineering, particularly through his patented heat treating apparatus, demonstrate his commitment to innovation and excellence. His work continues to influence the aerospace industry, ensuring the reliability and performance of gas turbine engine components.