Moissy-Cramayel, France

Christian Michel Jacques Gosselin



Average Co-Inventor Count = 6.0

ph-index = 1


Company Filing History:


Years Active: 2019

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1 patent (USPTO):Explore Patents

Title: The Innovations of Christian Michel Jacques Gosselin

Introduction

Christian Michel Jacques Gosselin is an accomplished inventor based in Moissy-Cramayel, France. He has made significant contributions to the field of turbomachinery, particularly with his innovative designs that enhance the efficiency and functionality of turbine systems. His work is recognized within the industry, and he is associated with Safran Aircraft Engines.

Latest Patents

Gosselin holds a patent for a turbomachine that features a shaft sleeve and an associated sleeve tube. This innovative turbine design includes a rotor with blades arranged on the periphery of disks in radial planes. A tie rod extends along slots in the disks, while an annular spacer fixes the position of the tie rod relative to the center line of the disks. The spacer is designed with through-openings that are arranged radially relative to the tie rod, allowing for the flow of a cooling medium through a channel limited by a separating pipe.

Career Highlights

Throughout his career, Gosselin has demonstrated a commitment to advancing turbine technology. His work at Safran Aircraft Engines has positioned him as a key player in the development of efficient and innovative turbomachinery solutions. His patent reflects his expertise and dedication to improving turbine performance.

Collaborations

Gosselin has collaborated with notable colleagues, including Maurice Guy Judet and Cecile Marie Emilienne Alirot. These partnerships have contributed to the successful development of innovative technologies in the field of aerospace engineering.

Conclusion

Christian Michel Jacques Gosselin's contributions to turbomachinery through his patent and work at Safran Aircraft Engines highlight his role as a significant inventor in the aerospace industry. His innovative designs continue to influence the efficiency and effectiveness of turbine systems.

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