Company Filing History:
Years Active: 2019
Title: Curtis Vedder: Innovator in Gas Turbine Engine Diagnostics
Introduction
Curtis Vedder is a notable inventor based in Avondale, AZ (US), recognized for his contributions to the field of gas turbine engine diagnostics. With a focus on enhancing the reliability and performance of gas turbine engines, Vedder has developed innovative solutions that address critical challenges in engine testing.
Latest Patents
Vedder holds a patent for a "Gas turbine engine and test cell real-time diagnostic fault detection and corrective action system and method." This invention provides a real-time diagnostic and fault detection system for gas turbine engines under test conditions. By utilizing sensor data from instrumentation linked to the engine, the system processes this information through a physics-based component level aero-thermal model. This model calculates various engine parameters at non-instrumented locations within the engine. The system is designed to detect faults and render images indicating the most likely causes and corrective actions. Additionally, it generates projections of engine performance under selected test conditions, allowing for prognostication regarding the engine's ability to pass these conditions.
Career Highlights
Vedder's career is marked by his work at Honeywell International Inc., where he has applied his expertise in gas turbine technology. His innovative approach has contributed significantly to advancements in engine diagnostics and performance evaluation.
Collaborations
Throughout his career, Vedder has collaborated with talented professionals, including Christopher Gill and Kevin Moeckly. These collaborations have fostered an environment of innovation and have led to the development of cutting-edge technologies in the field.
Conclusion
Curtis Vedder's work in gas turbine engine diagnostics exemplifies the impact of innovation in engineering. His patented technology not only enhances the testing process but also contributes to the overall efficiency and reliability of gas turbine engines.