Company Filing History:
Years Active: 1989
Title: Masamichi Ito: Innovator in High Temperature Combustion Catalysts
Introduction
Masamichi Ito is a notable inventor based in Yokosuka, Japan. He is recognized for his contributions to the field of combustion technology, particularly in the development of high temperature combustion catalysts. His innovative work has implications for improving the efficiency and durability of gas turbine combustors.
Latest Patents
Masamichi Ito holds a patent for a high temperature combustion catalyst and the method for producing the same. This catalyst is designed for use in catalytic combustion type gas turbine combustors. It features superior low temperature ignitionability and exceptional thermal durability at high temperatures. The catalyst comprises a porous carrier layer and a catalyst component, which includes palladium and platinum. Additionally, it incorporates first, second, and third promoter components, which enhance its performance. The first promoter component consists of rare earth elements and alkaline earth metals, while the second includes magnesium and silicon. The third promoter component features heavy metals and their oxides. A method for producing this high temperature combustion catalyst is also disclosed in his patent.
Career Highlights
Throughout his career, Masamichi Ito has worked with prominent companies, including Kabushiki Kaisha Toshiba and The Tokyo Electric Power Company, Incorporated. His experience in these organizations has contributed to his expertise in combustion technology and innovation.
Collaborations
Masamichi Ito has collaborated with notable colleagues, including Akio Ohkoshi and Kenjiro Shizukawa. These collaborations have likely enriched his research and development efforts in the field of combustion catalysts.
Conclusion
Masamichi Ito's work in high temperature combustion catalysts showcases his innovative spirit and dedication to advancing combustion technology. His contributions are significant in enhancing the efficiency and performance of gas turbine combustors.