This inventor holds 6 USPTO granted patents and 2 published patent applications and 4 EPO patents. Top assignee: Rolls-Royce Corporation. Active years: 2007-2021.
Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile
Company Filing History:
Years Active: 2007-2021
Title: Michael Philip Keenan: Innovator in Gas Turbine Technology
Introduction
Michael Philip Keenan is a notable inventor based in Sheffield, GB. He has made significant contributions to the field of gas turbine technology, holding a total of 6 patents. His work focuses on enhancing the efficiency and performance of gas turbine engines.
Latest Patents
Among his latest patents is a design for a metallic shaft intended for connecting components of a gas turbine engine. This innovative shaft features a first section composed of a material with a specific thermal expansion coefficient, and a second section with a different thermal expansion coefficient, allowing for improved functionality in high-temperature environments. Another notable patent is for a blade designed for a gas turbine engine, which includes an asymmetrical blade root, further advancing the technology in this field.
Career Highlights
Michael is currently employed at Rolls-Royce Corporation, a leading company in aerospace and defense. His work at Rolls-Royce has allowed him to apply his inventive skills to real-world applications, contributing to the development of advanced gas turbine systems.
Collaborations
Throughout his career, Michael has collaborated with esteemed colleagues such as Gareth M Armstrong and Stewart T Thornton. These partnerships have fostered innovation and have been instrumental in the successful development of his patented technologies.
Conclusion
Michael Philip Keenan's contributions to gas turbine technology through his patents and work at Rolls-Royce Corporation highlight his role as a key innovator in the field. His advancements continue to influence the efficiency and performance of gas turbine engines.
Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile
