Company Filing History:
Years Active: 2022
Title: David A. Burton: Innovator in Gas Turbine Technology
Introduction
David A. Burton is a notable inventor based in San Diego, CA, recognized for his contributions to gas turbine technology. With a focus on enhancing the efficiency and functionality of gas turbine engines, he has developed innovative solutions that address critical engineering challenges.
Latest Patents
David A. Burton holds a patent for a "Stator assembly for compressor mid-plane rotor balancing and sealing in gas turbine engine." This invention features a stator assembly designed to be mounted around a rotor disc at a compressor mid-plane. It allows for access to the rotor disc for trim balancing without the need to disassemble the stator assembly or the compressor case. The design includes a removable stator vane and vane apertures that facilitate radial access to the rotor disc. Additionally, a case access assembly ensures that the removable stator vane is securely sealed within the compressor case when engaged, while also providing access when disengaged. This innovative approach enables efficient trim balancing of a mid-plane compressor rotor assembly.
Career Highlights
David A. Burton is currently employed at Solar Turbines Inc., where he continues to work on advancements in gas turbine technology. His expertise and innovative mindset have made significant contributions to the field, particularly in the design and functionality of compressor systems.
Collaborations
Throughout his career, David has collaborated with talented professionals, including Kwok-Kwong Ben Tse and David Lau. These collaborations have fostered a creative environment that encourages the development of groundbreaking technologies in the gas turbine sector.
Conclusion
David A. Burton's work exemplifies the spirit of innovation in the field of gas turbine technology. His patented inventions and collaborative efforts continue to push the boundaries of engineering, contributing to advancements that enhance the efficiency and performance of gas turbine engines.