Kevin Baker

Title: Kevin Baker - Innovator in Aircraft Propulsion Systems

Introduction

Kevin Baker is a notable inventor based in Tempe, AZ (US). He has made significant contributions to the field of aircraft propulsion systems. His innovative work focuses on enhancing the efficiency and control of turboprop engines.

Latest Patents

Kevin Baker holds a patent for an "Aircraft turboprop engine propeller pitch control system including a controllable feather valve." This advanced propeller pitch control system is designed for turboprop engines and incorporates a negative torque sensor, a full feather control valve assembly, and a feather valve assembly. The feather valve assembly is responsive to fluid pressures from the negative torque sensor and the control valve assembly, allowing it to move between multiple positions. Additionally, an engine control unit or a manual user interface can be utilized to control the position of the feather.

Career Highlights

Kevin Baker is currently employed at Honeywell International Inc., where he continues to develop innovative solutions in aerospace technology. His work has been instrumental in improving the performance and reliability of aircraft engines.

Collaborations

Throughout his career, Kevin has collaborated with talented professionals, including Paul W Futa, Jr. and Hannah Amor. These collaborations have fostered a creative environment that encourages innovation and the development of cutting-edge technologies.

Conclusion

Kevin Baker's contributions to aircraft propulsion systems exemplify the spirit of innovation in the aerospace industry. His patent for a propeller pitch control system showcases his commitment to enhancing aircraft performance and safety.