Etobicoke, Canada

Stephen Phillips



Average Co-Inventor Count = 3.8

ph-index = 6

Forward Citations = 154(Granted Patents)


Location History:

  • Toronto, CA (2010 - 2012)
  • Etobicoke, CA (2010 - 2012)

Company Filing History:


Years Active: 2010-2012

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8 patents (USPTO):Explore Patents

Title: The Innovative Contributions of Stephen Phillips

Introduction

Stephen Phillips is a notable inventor based in Etobicoke, Canada. He has made significant contributions to the field of gas turbine technology, holding a total of eight patents. His work focuses on enhancing the efficiency and functionality of combustor components in gas turbine engines.

Latest Patents

Among his latest patents is the "Combustor liner with integrated anti-rotation and removal feature." This invention features a combustor liner for a gas turbine engine, which includes first and second annular liner portions engaged with an interference fit. The first liner portion has at least one anti-rotation feature that engages the second liner portion, allowing for a threaded hole to receive a pushing tool for easy removal. Another significant patent is the "Method for manufacturing a combustor heat shield." This heat shield comprises a member with an opening for a fuel nozzle, and a louver that directs air along the hot side of the heat shield member.

Career Highlights

Stephen Phillips has built a successful career at Pratt & Whitney Canada Corp., where he has been instrumental in developing advanced technologies for gas turbine engines. His innovative designs have contributed to improved performance and reliability in the aerospace industry.

Collaborations

Throughout his career, Phillips has collaborated with talented individuals such as Kenneth D Parkman and Bhawan Bhai Patel. These partnerships have fostered a creative environment that has led to the development of groundbreaking technologies.

Conclusion

Stephen Phillips exemplifies the spirit of innovation in the aerospace sector. His patents and contributions continue to influence the design and efficiency of gas turbine engines.

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