Todd M Neill is an accomplished inventor based in Shingle Spring, CA (US). He has made significant contributions to the field of gas turbine engine technology, holding a total of 2 patents. His work focuses on enhancing the performance and efficiency of combustors in gas turbine engines.

Latest Patents

Neill's latest patents include the "Swirler scoop and bearing plate for combustor" and the "Fuel nozzle with combined radial and axial bellows." The swirler scoop patent addresses the effectiveness of a radial inlet air swirler for the fuel nozzle in the combustor of a gas turbine engine. It enhances performance by reducing pressure loss associated with compressor discharge air entering the combustor cowl. This innovation creates a circumferential uniform feed pressure, improving flow and fuel/air mixing, which reduces smoke production without negatively impacting combustor or engine performance. The fuel nozzle patent features evacuated radial and axial bellows that are concentrically mounted to the fuel passages. This design prevents coking of the fuel passages and maintains the structural integrity of the integral parts, particularly the weld joints.

Career Highlights

Neill has had a notable career at United Technologies Corporation, where he has applied his expertise in gas turbine technology. His innovative designs have contributed to advancements in engine performance and efficiency.

Collaborations

Throughout his career, Neill has collaborated with esteemed colleagues such as Jim A Clark and Charles B Graves. These partnerships have fostered a creative environment that encourages innovation and the development of cutting-edge technologies.

Conclusion

Todd M Neill's contributions to gas turbine engine technology through his patents and collaborations highlight his role as a significant inventor in the field. His work continues to influence advancements in engine performance and efficiency.