CA

Kenneth James Young

This inventor holds 1 USPTO granted patent. Top assignees: Rolls-Royce Corporation, Rolls-Royce Deutschland Ltd & Co. Kg. Active years: 2006.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Kenneth James Young. Retrieved from https://idiyas.com/inventor/kenneth-james-young-mfpl36a1

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 = 6.0

ph-index = 1

Forward Citations = 17(Granted Patents)


Company Filing History:


Years Active: 2006

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1 patent (USPTO):Explore Patents

Title: Kenneth James Young: Innovator in Gas Turbine Technology

Introduction

Kenneth James Young is a notable inventor based in California, recognized for his contributions to gas turbine engine technology. He holds a patent for a combustion chamber designed to enhance the efficiency and performance of gas turbine engines.

Latest Patents

His patent, titled "Combustion chamber for gas turbine engine," features a unique design that incorporates at least one Helmholtz resonator. This resonator includes a cavity and a damping tube that is in flow communication with the chamber interior. The damping tube is equipped with cooling holes that extend through its wall, which significantly improves both damping and cooling within the combustion chamber. Kenneth holds 1 patent in this field.

Career Highlights

Throughout his career, Kenneth has worked with prestigious companies, including Rolls-Royce Corporation and Rolls-Royce Deutschland Ltd & Co. Kg. His experience in these organizations has allowed him to contribute to advancements in aerospace engineering and gas turbine technology.

Collaborations

Kenneth has collaborated with esteemed professionals in the industry, including Iain David Jeffrey Dupere and Volker Herzog. Their collective expertise has furthered the development of innovative solutions in gas turbine technology.

Conclusion

Kenneth James Young's work in gas turbine engine technology exemplifies innovation and engineering excellence. His patented designs continue to influence the field and contribute to advancements in aerospace applications.

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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