Fairfield, OH, United States of America

Steven J Reilly


Average Co-Inventor Count = 4.0

ph-index = 1

Forward Citations = 7(Granted Patents)


Company Filing History:


Years Active: 1994

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1 patent (USPTO):Explore Patents

Title: Steven J Reilly - Innovator in Damper Technology

Introduction

Steven J Reilly is a notable inventor based in Fairfield, OH (US). He has made significant contributions to the field of engineering, particularly in the development of innovative damper systems. His work is characterized by a focus on enhancing the performance and reliability of mechanical systems.

Latest Patents

Reilly holds a patent for a "Free-riding oil tube damper." This invention features a free-floating damper system designed to allow a damper arm to move freely in the x/y plane while restricting movement in the z plane. The damper arm is equipped with first and second wear bushings positioned in a spring-biased support, ensuring the generation of coulomb dampening forces between the bushings and the damper housing. This technology can be fixedly mounted to components of a gas turbine engine, such as the turbine frame, to effectively dissipate vibrational forces that could potentially damage the accessory tube.

Career Highlights

Reilly is associated with General Electric Company, where he has applied his expertise in mechanical engineering to develop advanced technologies. His work has contributed to the enhancement of various engineering applications, particularly in the aerospace sector.

Collaborations

Throughout his career, Reilly has collaborated with esteemed colleagues, including Charles L Williams and John G Buechler. These partnerships have fostered innovation and the successful development of cutting-edge technologies.

Conclusion

Steven J Reilly's contributions to damper technology exemplify the impact of innovative engineering solutions in modern mechanical systems. His patent for the free-riding oil tube damper showcases his commitment to improving the reliability and performance of critical components in gas turbine engines.

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