Lake Stevens, WA, United States of America

Kevin R Puzey

This inventor holds 2 USPTO granted patents. Top assignee: The Boeing Company. Active years: 2017-2018.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Kevin R Puzey. Retrieved from https://idiyas.com/inventor/kevin-r-puzey

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


Average Co-Inventor Count = 4.0

ph-index = 1

Forward Citations = 1(Granted Patents)


Company Filing History:


Years Active: 2017-2018

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2 patents (USPTO):Explore Patents

Title: Kevin R Puzey: Innovator in Wing-to-Fuselage Integration

Introduction

Kevin R Puzey is a notable inventor based in Lake Stevens, WA (US). He has made significant contributions to the field of aerospace engineering, particularly in the area of wing-to-fuselage integration. With a total of 2 patents, Puzey's work has been instrumental in advancing aircraft design and functionality.

Latest Patents

Puzey's latest patents focus on methods and components for wing-to-fuselage integration. One of the key innovations involves a method that includes attaching a fitting to a wing box assembly of an aircraft at an early stage of integration. This fitting is then connected to a stub beam attached to a fuselage panel at a later stage. This innovative approach eliminates the need to attach the stub beam directly to the wing box assembly, streamlining the integration process.

Career Highlights

Kevin R Puzey is currently employed at The Boeing Company, where he continues to develop and refine his innovative ideas. His work at Boeing has allowed him to collaborate with some of the brightest minds in the industry, contributing to the advancement of aerospace technology.

Collaborations

Some of Puzey's notable coworkers include Charles B Lockin and Marcus Alexander Erickson. Their collaborative efforts have further enhanced the innovative projects they work on together.

Conclusion

Kevin R Puzey's contributions to wing-to-fuselage integration represent a significant advancement in aerospace engineering. His innovative methods and collaboration with industry experts continue to shape the future of aircraft design.

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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