Kimberly Pash Boyington

Title: The Innovative Contributions of Kimberly Pash Boyington

Introduction

Kimberly Pash Boyington is a notable inventor based in Haddam, Connecticut. She has made significant contributions to the field of gas turbine engine technology, holding a total of four patents. Her work exemplifies the intersection of engineering and innovation, showcasing her expertise in designing advanced components for turbomachinery.

Latest Patents

Among her latest patents is the "Gas turbine engine airfoil frequency design." This invention features a turbomachine airfoil element with pressure and suction sides that are spaced apart in a thickness direction. The airfoil extends radially with a span ranging from 0.46 to 0.59 inches. It also includes a chord length that varies from 0.73 to 0.86 inches at 50% span. The airfoil element is designed with multiple modes of frequency, including a first mode at 5133±15% Hz and a sixth mode at 27084±15% Hz. Another significant patent is the "Stress-relieved wire seal assembly for gas turbine engines." This assembly is designed for use in gas turbine engines and includes a circumferential groove in a disk and an annular wire seal positioned within the groove.

Career Highlights

Kimberly has worked with prominent companies in the aerospace sector, including United Technologies Corporation and Raytheon Technologies Corporation. Her experience in these organizations has allowed her to develop and refine her innovative ideas in gas turbine technology.

Collaborations

Throughout her career, Kimberly has collaborated with talented individuals such as David Mikol and Brian J. Schuler. These partnerships have contributed to her success and the advancement of her inventions.

Conclusion

Kimberly Pash Boyington's contributions to gas turbine technology highlight her innovative spirit and dedication to engineering excellence. Her patents reflect her commitment to advancing the field and improving the performance of turbomachinery.