Kerry J Lighty is a prolific inventor based in Plainfield, IN, recognized for his significant contributions to gas turbine technology. With an impressive portfolio of 21 patents, Lighty has been instrumental in developing innovative systems that enhance the efficiency and performance of gas turbine engines.

Latest Patents

Among his latest patents is the "Bypass Duct Heat Exchanger Mount System with Reduced Motion." This innovative design involves a gas turbine engine featuring a bypass duct that houses a heat exchanger and a turnbuckle assembly. The turnbuckle assembly enhances the lateral stiffness of the heat exchanger while ensuring that the dynamic mode remains outside the fan rotor operating range. Another significant patent is for "Heat Exchanger Inlet Vane Assemblies with Improved Mixing Trailing Edge Features," which focuses on optimizing heat transfer capabilities and is coupled with an inlet shroud to ensure effective performance in gas turbine applications.

Career Highlights

Throughout his career, Kerry J Lighty has held various prominent positions, particularly at Rolls-Royce North American Technologies Inc. and Rolls-Royce Corporation. His work with these industry leaders has enabled him to make substantial advancements in gas turbine technology, contributing to the overall efficiency and reliability of their engine systems.

Collaborations

Collaboration has played a vital role in Lighty’s career, where he has worked alongside talented professionals such as Paul O'Meallie and Phillip Burnside. Their combined expertise has fostered a creative environment, leading to the development of patents that push the boundaries of current technology.

Conclusion

Kerry J Lighty’s commitment to innovation is evident in his extensive patent portfolio and his contributions to the field of gas turbine technology. His inventions not only represent individual milestones in engineering but also pave the way for future advancements in the industry. As he continues to develop new solutions, Lighty’s work remains critical for the evolution of turbine systems.

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