Konstantinos Panagiotis Giannakopolous

Title: Konstantinos Panagiotis Giannakopolous: Innovator in Gas Turbine Engine Design

Introduction

Konstantinos Panagiotis Giannakopolous is a notable inventor based in Middletown, CT (US). He has made significant contributions to the field of turbomachinery, particularly in the design of gas turbine engine airfoils. His innovative work has led to the development of a unique airfoil design that enhances the performance of gas turbine engines.

Latest Patents

Giannakopolous holds a patent for a gas turbine engine airfoil frequency design. This patent describes a turbomachine airfoil element that features pressure and suction sides spaced apart in a thickness direction, joined at leading and trailing edges. The airfoil extends radially with a span ranging from 2.85 to 3.15 inches (72.4 to 80.0 mm). The chord length, measured from the leading edge to the trailing edge at 50% span, is between 1.52 and 1.82 inches (38.6 to 46.2 mm). The design includes multiple modes of frequency, with the first mode at 506±10% Hz, and subsequent modes at frequencies of 1732±10% Hz, 2268±10% Hz, 4007±10% Hz, 4851±10% Hz, and 6416±10% Hz.

Career Highlights

Giannakopolous is currently employed at Raytheon Technologies Corporation, where he continues to innovate in the field of aerospace engineering. His work focuses on enhancing the efficiency and performance of gas turbine engines, contributing to advancements in aviation technology.

Collaborations

Throughout his career, Giannakopolous has collaborated with esteemed colleagues, including Kurt R. Heinemann and Sumin Tao. These collaborations have fostered a productive environment for innovation and development in gas turbine technology.

Conclusion

Konstantinos Panagiotis Giannakopolous is a distinguished inventor whose work in gas turbine engine design has made a significant impact on the aerospace industry. His innovative airfoil design and contributions at Raytheon Technologies Corporation exemplify his commitment to advancing technology in this critical field.