Location History:
- Fontainebleau, FR (2015 - 2018)
- Moissy-Cramayel, FR (2018 - 2023)
Company Filing History:
Years Active: 2015-2025
Title: Tangi Brusq: Innovator in Turbomachinery Technology
Introduction
Tangi Brusq is a notable inventor based in Moissy-Cramayel, France. He has made significant contributions to the field of turbomachinery, particularly in the maintenance and control of high-pressure turbines. With a total of seven patents to his name, Brusq's work has advanced the efficiency and reliability of gas turbine engines.
Latest Patents
Brusq's latest patents include a method for maintaining a bladed wheel of a high-pressure turbine of a turbomachine. This innovative method involves a disc with cavities and blades that extend radially from a root mounted in the disc. The method allows for the measurement of radial clearance between the blade tips and the turbine shroud, enabling the removal of a foil if the clearance exceeds a predetermined value. Another significant patent is a method and control unit for controlling the play of a high-pressure turbine. This method includes detecting transient acceleration phases of the engine and controlling a valve that delivers air to the turbine shroud based on specific temperature thresholds.
Career Highlights
Throughout his career, Tangi Brusq has worked with prominent companies in the aerospace industry, including Snecma and Safran Aircraft Engines. His experience in these organizations has allowed him to develop and refine his innovative ideas in turbomachinery technology.
Collaborations
Brusq has collaborated with notable professionals in his field, including Emmanuel Berche and Jean-Luc Bacha. These collaborations have contributed to the advancement of his research and the successful implementation of his patented technologies.
Conclusion
Tangi Brusq is a distinguished inventor whose work in turbomachinery has led to significant advancements in the industry. His innovative patents and collaborations reflect his commitment to enhancing the performance and reliability of gas turbine engines.