Company Filing History:
Years Active: 2008-2013
Title: Martin S Goodwin: Innovator in Gas Turbine Technology
Introduction
Martin S Goodwin is a notable inventor based in Loughborough, GB. He has made significant contributions to the field of gas turbine technology, holding a total of 2 patents. His work focuses on enhancing the efficiency and performance of gas turbine engines.
Latest Patents
One of Martin's latest patents is for a "Swirler for a fuel injector." This innovative swirler is designed to direct airflow into the combustor of a gas turbine engine, effectively atomizing fuel as it exits the fuel injector. The swirler features multiple passages that channel airflow, each configured to rotate the airflow around a swirl axis. This design allows for selective variation of the exit swirl angle and direction of rotation, optimizing combustion efficiency.
Another significant patent is for a "Combustion chamber for a gas turbine engine." This combustion chamber incorporates at least one Helmholtz resonator, which includes a resonator cavity and a neck in flow communication with the chamber interior. The resonator neck is equipped with cooling holes that enhance damping and cooling, with at least one hole directed towards the resonator cavity, improving overall performance.
Career Highlights
Martin S Goodwin 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 innovative ideas in real-world applications, contributing to advancements in gas turbine technology.
Collaborations
Throughout his career, Martin has collaborated with esteemed colleagues such as Michael A Macquisten and Anthony John Moran. These collaborations have fostered a creative environment that encourages innovation and the development of cutting-edge technologies.
Conclusion
Martin S Goodwin is a distinguished inventor whose work in gas turbine technology has led to significant advancements in the field. His patents reflect a commitment to improving efficiency and performance in gas turbine engines.