New Britain, CT, United States of America

Kirk A Shute


 

Average Co-Inventor Count = 2.7

ph-index = 1

Forward Citations = 6(Granted Patents)


Company Filing History:


Years Active: 2017-2019

Loading Chart...
Loading Chart...
2 patents (USPTO):Explore Patents

Title: Kirk A. Shute: Innovator in Turbine Engine Technology

Introduction

Kirk A. Shute is a notable inventor based in New Britain, Connecticut, who has made significant contributions to the field of turbine engine technology. With a total of 2 patents to his name, Shute's work focuses on innovative solutions for mounting turbine engines and enhancing their functionality.

Latest Patents

Shute's latest patents include an assembly for mounting a turbine engine to an airframe. This assembly features a thrust pin linkage that connects the engine core mount and the engine exhaust mount, ensuring a secure attachment to the airframe. Another significant patent is for a flap seal for a gas turbine engine movable nozzle flap. This invention includes a seal assembly that maintains engagement between the seal and the nozzle flap, enhancing the efficiency of the engine's operation.

Career Highlights

Kirk A. Shute is currently employed at United Technologies Corporation, where he continues to develop innovative technologies in the aerospace sector. His work has been instrumental in advancing turbine engine designs, contributing to improved performance and reliability.

Collaborations

Shute has collaborated with notable coworkers such as Shawn M. McMahon and Jeffrey R. Lavin, who have also contributed to advancements in turbine engine technology.

Conclusion

Kirk A. Shute's contributions to turbine engine technology through his patents and work at United Technologies Corporation highlight his role as an influential inventor in the aerospace industry. His innovative solutions continue to shape the future of turbine engine design and functionality.

This text is generated by artificial intelligence and may not be accurate.
Please report any incorrect information to support@idiyas.com
Loading…