West Suffield, CT, United States of America

Justin J Phillips

USPTO Granted Patents = 1 

 

Average Co-Inventor Count = 7.0

ph-index = 1

Forward Citations = 1(Granted Patents)


Company Filing History:


Years Active: 2018

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1 patent (USPTO):Explore Patents

Title: Justin J Phillips - Innovator in Gas Turbine Cooling Systems

Introduction

Justin J Phillips is a notable inventor based in West Suffield, CT (US). He has made significant contributions to the field of gas turbine technology, particularly in cooling systems. His innovative approach has led to the development of a unique cooling system that enhances the efficiency of gas turbine engines.

Latest Patents

Justin holds 1 patent for his invention titled "Cooling system with a bearing compartment bypass." This cooling system is designed to provide buffer cooled cooling air to the turbine section of a gas turbine engine. The system includes a first conduit for transmitting cooling air, a heat exchanger for cooling bleed airflow, and a bypass conduit that directs buffer air through a passageway that bypasses the bearing compartment. Additionally, it features a manifold for mixing cooling air and buffer air, along with a nozzle assembly for delivering the cooled air to the turbine section.

Career Highlights

Justin is currently employed at United Technologies Corporation, where he continues to work on innovative solutions in the aerospace sector. His expertise in gas turbine technology has positioned him as a valuable asset to his team and the company.

Collaborations

Throughout his career, Justin has collaborated with esteemed colleagues such as James D Hill and William K Ackermann. These partnerships have fostered a creative environment that encourages the development of cutting-edge technologies.

Conclusion

Justin J Phillips exemplifies the spirit of innovation in the field of gas turbine technology. His contributions, particularly in cooling systems, demonstrate his commitment to advancing engineering solutions. His work continues to impact the efficiency and performance of gas turbine engines.

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