Weyarn, Germany

Hendrik Riedmann

USPTO Granted Patents = 1 

 

Average Co-Inventor Count = 4.0

ph-index = 1


Company Filing History:


Years Active: 2024

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1 patent (USPTO):Explore Patents

Title: Hendrik Riedmann: Innovator in Rocket Engine Technology

Introduction

Hendrik Riedmann is a notable inventor based in Weyarn, Germany. He has made significant contributions to the field of rocket engine technology, particularly with his innovative designs that enhance performance and efficiency. His work is characterized by a focus on integrating advanced materials and engineering techniques.

Latest Patents

Riedmann holds a patent for a "Rocket engine section having a porous inner wall portion and method for manufacturing a rocket engine section." This invention features a combustion chamber body with an inner wall and a channel that carries a cooling medium. The design includes a porous portion that is integrally formed with the inner wall, allowing the cooling medium to flow into the combustion chamber body. The porosity of this portion is crucial as it determines the volume and mass flow rates of the cooling medium, thereby optimizing the engine's performance.

Career Highlights

Hendrik Riedmann is currently associated with Arianegroup GmbH, where he applies his expertise in aerospace engineering. His innovative approach to rocket engine design has positioned him as a key player in the industry. With a focus on enhancing the efficiency and reliability of rocket propulsion systems, Riedmann continues to push the boundaries of aerospace technology.

Collaborations

Throughout his career, Riedmann has collaborated with talented professionals in the field, including Dietmar Wiedmann and Daniel Eiringhaus. These collaborations have fostered an environment of innovation and creativity, leading to advancements in rocket engine technology.

Conclusion

Hendrik Riedmann's contributions to rocket engine technology exemplify the spirit of innovation in the aerospace industry. His patented designs and collaborative efforts continue to influence the future of rocket propulsion systems.

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