Shelton, CT, United States of America

James Steven Johnson


Average Co-Inventor Count = 1.7

ph-index = 3

Forward Citations = 29(Granted Patents)


Location History:

  • Jupiter, FL (US) (1995)
  • Shelton, CT (US) (2002)

Company Filing History:


Years Active: 1995-2002

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3 patents (USPTO):Explore Patents

Title: Innovations of James Steven Johnson

Introduction

James Steven Johnson is a notable inventor based in Shelton, CT (US). He has made significant contributions to the field of gas turbine engine technology. With a total of 3 patents, his work focuses on enhancing the performance and efficiency of exhaust nozzles.

Latest Patents

One of his latest patents is the "Throat configuration for axisymmetric nozzle." This invention optimizes the radius of the hinged portion of the convergent/divergent axisymmetrical exhaust nozzle of a gas turbine engine. The design aims to improve flow characteristics and reduce radar visibility. Another significant patent is the "Axi-nozzle ejector seal." This innovation features a nozzle that includes an outer casing, a convergent section, a divergent section, and a collapsible seal member. The design enhances the functionality of gas turbine engines by ensuring better performance and efficiency.

Career Highlights

James Steven Johnson has had a successful career at United Technologies Corporation, where he has been instrumental in developing advanced technologies for gas turbine engines. His expertise in nozzle design has contributed to the company's reputation for innovation in aerospace engineering.

Collaborations

Throughout his career, Johnson has collaborated with talented individuals such as Timothy J McAlice and Rudolph J Novotny. These partnerships have fostered a creative environment that has led to groundbreaking advancements in their field.

Conclusion

James Steven Johnson's contributions to gas turbine engine technology through his patents and collaborations highlight his role as a key innovator in the industry. His work continues to influence advancements in aerospace engineering.

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