Madison, CT, United States of America

Michael Li


 

Average Co-Inventor Count = 4.0

ph-index = 1

Forward Citations = 1(Granted Patents)


Company Filing History:


Years Active: 2019-2021

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3 patents (USPTO):Explore Patents

Title: Michael Li: Innovator in Gas Turbine Technology

Introduction

Michael Li is a notable inventor based in Madison, CT (US), recognized for his contributions to gas turbine technology. With a total of 3 patents, he has made significant advancements in the design and functionality of fan blades used in gas turbine engines.

Latest Patents

One of Michael Li's latest patents is focused on a fan blade attachment root with improved strain response. This innovative design includes a leading edge, an attachment root extending aft of the leading edge, and a trench formed in the surface of the attachment root. The attachment root also features a dovetail extending aft of the leading edge, enhancing the overall performance of the gas turbine engine. The gas turbine engine itself comprises a compressor section configured to rotate about an axis, a combustor located aft of the compressor section, and a turbine section that also rotates about the same axis. A fan is positioned forward of the turbine section and includes a blade that incorporates a trench formed in its attachment root.

Career Highlights

Michael Li has had a distinguished career, working with prominent companies such as Raytheon Technologies Corporation and United Technologies Corporation. His experience in these organizations has allowed him to develop and refine his innovative ideas in the field of gas turbine technology.

Collaborations

Throughout his career, Michael has collaborated with talented individuals, including Lee Drozdenko and William R Graves. These partnerships have contributed to the successful development of his patented technologies.

Conclusion

Michael Li's work in gas turbine technology exemplifies the spirit of innovation and dedication to improving engineering solutions. His patents reflect a commitment to advancing the efficiency and performance of gas turbine engines.

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