Ellington, CT, United States of America

Sonia A Martinez

USPTO Granted Patents = 1 

 

Average Co-Inventor Count = 2.0

ph-index = 1

Forward Citations = 10(Granted Patents)


Company Filing History:


Years Active: 2011

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1 patent (USPTO):Explore Patents

Title: Sonia A. Martinez: Innovator in Thermal Barrier Coatings

Introduction

Sonia A. Martinez is a notable inventor based in Ellington, CT (US). She has made significant contributions to the field of thermal barrier coatings, particularly in the context of turbine blades. Her innovative work focuses on the measurement and analysis of residual stress, which is crucial for predicting damage in these coatings.

Latest Patents

Martinez holds a patent for her invention titled "Local residual stress measurement and analysis for detection and prediction of damage in thermal barrier coatings." This patent outlines a method for evaluating the degradation of thermal barrier coatings on turbine blades. The method involves measuring the residual stress of the coating's outer surface after the turbine blade has been subjected to normal operating conditions. By comparing the residual stress measurement with a control stress measurement, the degradation of the coating can be determined. She has 1 patent to her name.

Career Highlights

Throughout her career, Sonia A. Martinez has worked with prominent organizations, including the United States of America as represented by the Secretary of the Air Force and United Technologies Corporation. Her expertise in thermal barrier coatings has positioned her as a valuable asset in the aerospace and engineering sectors.

Collaborations

Martinez has collaborated with notable colleagues such as Shamachary Sathish and Herbert A. Chin. Their combined efforts have contributed to advancements in the understanding and application of thermal barrier coatings.

Conclusion

Sonia A. Martinez is a pioneering inventor whose work in thermal barrier coatings has the potential to enhance the performance and longevity of turbine blades. Her innovative methods for measuring residual stress are vital for the future of aerospace engineering.

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