Tsukuba, Japan

Shinichiro Tokudome


Average Co-Inventor Count = 6.0

ph-index = 1


Company Filing History:


Years Active: 2015

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1 patent (USPTO):Explore Patents

Title: Shinichiro Tokudome: Innovator in Rocket Engine Technology

Introduction

Shinichiro Tokudome is a prominent inventor based in Tsukuba, Japan. He is known for his contributions to rocket engine technology, particularly in the development of systems that enhance performance and efficiency. His innovative approach has led to significant advancements in the field.

Latest Patents

One of Tokudome's notable patents is a rocket engine system designed for realizing high-speed response. This invention features a turbo pump where a pump impeller is connected to one end of a rotary shaft, while a turbine is connected to the other end. The design allows for an operation region defined by an equivalent area between a turbine efficiency curve and an actual machine's efficiency curve, ensuring optimal performance regardless of pump flow rate. This patent showcases his expertise in creating efficient propulsion systems.

Career Highlights

Throughout his career, Tokudome has worked with esteemed organizations such as IHI Corporation and the Japan Aerospace Exploration Agency. His experience in these companies has provided him with a solid foundation in aerospace engineering and innovation. His work has been instrumental in advancing rocket technology and enhancing the capabilities of modern propulsion systems.

Collaborations

Tokudome has collaborated with notable colleagues, including Hatsuo Mori and Yoshihiro Naruo. These partnerships have fostered a creative environment that encourages the exchange of ideas and expertise, further driving innovation in their respective fields.

Conclusion

Shinichiro Tokudome's contributions to rocket engine technology exemplify the spirit of innovation. His patent on the turbo pump system highlights his commitment to enhancing performance in aerospace applications. Through his work and collaborations, he continues to influence the future of rocket propulsion systems.

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