Meriden, CT, United States of America

Jordan Tresser


Average Co-Inventor Count = 8.0

ph-index = 1

Forward Citations = 42(Granted Patents)


Company Filing History:

goldMedal1 out of 832,843 
Other
 patents

Years Active: 2004

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1 patent (USPTO):Explore Patents

Title: Innovations of Jordan Tresser in Micro Gas Turbine Technology.

Introduction

Jordan Tresser is an accomplished inventor based in Meriden, CT (US). He has made significant contributions to the field of micro gas turbine engines, showcasing his expertise through innovative designs and patents. His work focuses on enhancing the efficiency and precision of turbine technology.

Latest Patents

One of Jordan Tresser's notable patents is for a micro gas turbine engine with active tip clearance control. This invention utilizes a capacitive sensor to measure the tip clearance of a radial compressor section. An actuator is employed to axially displace the rotor shaft based on the sensor's output. This technology allows for highly sensitive measurements, particularly in areas where tip clearance is minimal, thus enabling precise control over the turbine's performance.

Career Highlights

Throughout his career, Jordan has demonstrated a commitment to innovation in turbine technology. His patent reflects a deep understanding of engineering principles and a dedication to improving existing systems. His work has the potential to influence the future of micro gas turbine engines significantly.

Collaborations

Jordan Tresser has collaborated with notable professionals in his field, including Friedrich B Prinz and Sangkyun Kang. These partnerships have likely contributed to the advancement of his projects and the successful development of his patented technologies.

Conclusion

Jordan Tresser's contributions to micro gas turbine technology exemplify the spirit of innovation. His patent for a micro gas turbine engine with active tip clearance control highlights his ability to address complex engineering challenges. Through his work, he continues to pave the way for advancements in turbine efficiency and precision.

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