Brian R Pelletier

Title: Innovations of Brian R Pelletier

Introduction

Brian R Pelletier is a notable inventor based in Berwick, ME (US). He has made significant contributions to the field of gas turbine engine technology, holding a total of 6 patents. His work focuses on enhancing the efficiency and performance of gas turbine engines.

Latest Patents

Among his latest patents is a design for a gas turbine engine flowpath component that includes vectored cooling flow holes. This innovative design features a primary flowpath connecting a compressor section, a combustor section, and a turbine section. The turbine section incorporates a stage vane with a radially outward platform that contains a cooling plenum. The design includes retaining features that extend radially outward from the platform, with vectored cooling holes directing cooling air from the plenum to adjacent gaspath components. Another significant patent is for a gas turbine engine rapid response clearance control system with an air seal segment interface. This active clearance control system features an air seal segment equipped with a bridge hook that has a lugged aperture, enhancing the operational efficiency of gas turbine engines.

Career Highlights

Brian has worked with prominent companies in the aerospace and defense sectors, including United Technologies Corporation and Raytheon Technologies Corporation. His experience in these organizations has allowed him to develop and refine his innovative ideas in gas turbine technology.

Collaborations

Throughout his career, Brian has collaborated with talented individuals such as Michael G McCaffrey and Brandon T Rouse. These collaborations have contributed to the advancement of his projects and innovations.

Conclusion

Brian R Pelletier's contributions to gas turbine engine technology through his patents and collaborations highlight his role as a significant inventor in the field. His work continues to influence advancements in engine performance and efficiency.