Suffield, CT, United States of America

Oleg Ivanov

USPTO Granted Patents = 3 

 

Average Co-Inventor Count = 2.6

ph-index = 2

Forward Citations = 10(Granted Patents)


Location History:

  • Granby, CT (US) (2018)
  • Suffield, CT (US) (2017 - 2019)

Company Filing History:


Years Active: 2017-2019

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3 patents (USPTO):Explore Patents

Title: Oleg Ivanov: Innovator in Gas Turbine Engine Technology

Introduction

Oleg Ivanov is a notable inventor based in Suffield, CT (US), recognized for his contributions to gas turbine engine technology. With a total of 3 patents, Ivanov has developed innovative methods and designs that enhance the performance and reliability of gas turbine engines.

Latest Patents

Ivanov's latest patents include a method for repairing a casing for a gas turbine engine, specifically focusing on flange partial section replacement. This method involves removing a defective portion of the flange, which includes at least one bolt hole, and securing a replacement portion in the opening left by the removed section. Additionally, he has patented an inner diameter scallop case flange for a gas turbine engine, which features a radial flange with a partial scallop along its inner diameter. This design allows for improved alignment and sealing between case assemblies.

Career Highlights

Throughout his career, Oleg Ivanov has worked with prominent companies in the aerospace sector, including United Technologies Corporation and RTX Corporation. His experience in these organizations has significantly contributed to his expertise in gas turbine technology.

Collaborations

Ivanov has collaborated with several professionals in his field, including Derek W. Anderson and Wai Tuck Chow. These collaborations have fostered innovation and development in gas turbine engine design.

Conclusion

Oleg Ivanov's work in gas turbine engine technology showcases his innovative spirit and dedication to improving engineering solutions. His patents reflect a commitment to advancing the industry and enhancing the performance of gas turbine engines.

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