Company Filing History:
Years Active: 2011-2019
Title: **David Lynn Dawson: Innovator in Jet Engine Technology**
Introduction
David Lynn Dawson is an accomplished inventor based in Liberty Township, OH. With a total of three patents to his name, he has significantly contributed to the field of jet engine technology. His innovative designs aim to improve engine efficiency and performance, particularly in variable cycle aircraft engines.
Latest Patents
Dawson's most recent patents showcase his expertise in enhancing jet engine performance. The first patent is for a **secondary nozzle for jet engine**, which introduces a third air stream at reduced pressure that enhances thrust. This third stream is exhausted through a concentric nozzle located in a low-pressure area, effectively reducing drag and improving engine efficiency.
The second patent, a **multi-nozzle flow diverter for jet engine**, pertains to an exhaust system designed for variable cycle aircraft engines. This system features a core exhaust for bypass air and combustion gases, utilizing a convergent-divergent nozzle made up of various flaps and seals. This innovative exhaust system allows for selective control of air flow, optimizing performance depending on the flight mode.
Career Highlights
Dawson's professional journey includes a key role at General Electric Company, where he applies his expertise in aerospace technology. His innovative designs reflect a commitment to advancing aircraft performance through effective engineering solutions.
Collaborations
David has worked alongside talented colleagues such as Erin Lee Lariviere and Brian Joseph Petersen. Their collaborations have been instrumental in bringing advanced concepts and inventions to fruition, contributing collectively to the aerospace industry's growth.
Conclusion
David Lynn Dawson's contributions to jet engine technology through his innovative patents embody the spirit of engineering advancement. His work continues to inspire developments in aircraft efficiency, showcasing his invaluable role in the field of aerospace engineering.