Boucherville, Canada

Christophe Tremblay


 

Average Co-Inventor Count = 3.0

ph-index = 1


Company Filing History:


Years Active: 2023

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2 patents (USPTO):Explore Patents

Title: The Innovative Contributions of Christophe Tremblay

Introduction

Christophe Tremblay is a notable inventor based in Boucherville, Canada. He has made significant contributions to the field of gas turbine technology, holding a total of 2 patents. His work focuses on enhancing the efficiency and performance of turbine systems.

Latest Patents

Tremblay's latest patents include innovative designs that improve turbine functionality. One of his patents is for turbine stator vanes having inserts and splitter plates. This invention features a stator with vanes that define an internal passage, incorporating an insert that allows for effective cooling air management. The design includes a splitter plate that enhances airflow, ensuring optimal performance of the turbine.

Another significant patent is the tangential on-board injector (TOBI) for gas turbine engines. This invention includes a casing assembly that directs cooling air toward the turbine rotor. The TOBI's design features a fastener-free engagement, which prevents relative movement between components, thereby enhancing the reliability of the gas turbine engine.

Career Highlights

Christophe Tremblay is currently employed at Pratt & Whitney Canada Corp., a leading company in aerospace technology. His work at Pratt & Whitney has allowed him to contribute to cutting-edge advancements in turbine design and efficiency.

Collaborations

Throughout his career, Tremblay has collaborated with talented individuals such as Franco Di Paola and Olivier Nadeau. These collaborations have fostered an environment of innovation and creativity, leading to the development of groundbreaking technologies in the aerospace sector.

Conclusion

Christophe Tremblay's contributions to turbine technology exemplify the spirit of innovation in the aerospace industry. His patents reflect a commitment to enhancing performance and efficiency in gas turbine engines.

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