Trollhättan, Sweden

Kent Holmedahl

This inventor holds 1 USPTO granted patent and 1 EPO patent. Top assignee: Gknaerospace Sweden Ab. Active years: 2017.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Kent Holmedahl. Retrieved from https://idiyas.com/inventor/kent-holmedahl

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 = 3.0

ph-index = 1

Forward Citations = 2(Granted Patents)


Company Filing History:


Years Active: 2017

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1 patent (USPTO):Explore Patents

Title: Kent Holmedahl: Innovator in Gas Turbine Engine Technology

Introduction

Kent Holmedahl is a notable inventor based in Trollhättan, Sweden. He has made significant contributions to the field of gas turbine engine technology. His innovative approach has led to the development of a unique method for manufacturing gas turbine engine components.

Latest Patents

Kent Holmedahl holds 1 patent for his invention titled "Method for manufacturing of a gas turbine engine component." This invention involves a method that includes an outer ring structure, an inner ring structure, and a series of circumferentially spaced elements. These elements create a primary gas channel for axial gas flow, facilitating efficient gas entrance and outflow in the turbine engine.

Career Highlights

Kent is currently employed at GKN Aerospace Sweden AB, where he applies his expertise in aerospace engineering. His work focuses on enhancing the performance and efficiency of gas turbine engines through innovative manufacturing techniques.

Collaborations

Kent has collaborated with esteemed colleagues such as Lars-Olof Hellgren and Olof Lewin, contributing to advancements in aerospace technology.

Conclusion

Kent Holmedahl's contributions to gas turbine engine technology exemplify the spirit of innovation in the aerospace industry. His patented method showcases his commitment to improving engineering practices and enhancing the performance of gas turbine engines.

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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