Allestree, United Kingdom

James Patterson

This inventor holds 1 USPTO granted patent. Top assignee: Rolls-Royce Corporation. Active years: 1979.

IDiyas Innovation Intelligence. (2026). Inventor Profile: James Patterson. Retrieved from https://idiyas.com/inventor/james-patterson-8xtq8cuu

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile


% Patents Active = 100.0

Average Co-Inventor Count = 2.0

ph-index = 1

Forward Citations = 20(Granted Patents)


Company Filing History:


Years Active: 1979

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1 patent (USPTO):Explore Patents

Title: James Patterson - Innovator in Gas Turbine Technology

Introduction

James Patterson is a notable inventor based in Allestree, GB. He has made significant contributions to the field of gas turbine technology. His innovative work has led to the development of a unique patent that enhances the efficiency and performance of gas turbine engines.

Latest Patents

James Patterson holds a patent for a compressor rotor stage. This invention features an annular array of aerofoil blades, each equipped with circumferentially extending platforms. These platforms are strategically spaced apart from those of adjacent blades. The design incorporates elastomeric dampers positioned between the blades, which engage with the inner faces of adjacent platforms during rotation. This innovative mechanism improves the overall functionality of gas turbine engines.

Career Highlights

James Patterson is associated with Rolls-Royce Corporation, a leading company in aerospace and energy sectors. His work at Rolls-Royce has allowed him to apply his inventive skills in a practical setting, contributing to advancements in turbine technology.

Collaborations

James has collaborated with various professionals in his field, including his coworker, Peter G Farrar. Their combined expertise has fostered innovation and development within the company.

Conclusion

James Patterson's contributions to gas turbine technology exemplify the impact of innovation in engineering. His patent for the compressor rotor stage showcases his commitment to enhancing performance in the aerospace industry.

Profile summary based on public USPTO records.
Data Sources: USPTO Patent Grant XML, Patent Center, EPO & CIPO • Normalized by IDiyas Innovation Graph. Methodology & provenance architecturePlease report any incorrect information to [email protected]
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