Cincinnati, OH, United States of America

Richard S Beitler


Average Co-Inventor Count = 3.4

ph-index = 2

Forward Citations = 70(Granted Patents)


Company Filing History:


Years Active: 1981-1982

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2 patents (USPTO):Explore Patents

Title: Richard S Beitler: Innovator in Gas Turbine Engine Control Systems

Introduction

Richard S Beitler is a notable inventor based in Cincinnati, OH (US), recognized for his contributions to gas turbine engine technology. With a total of 2 patents, Beitler has made significant advancements in control systems that enhance the performance and efficiency of gas turbine engines.

Latest Patents

Beitler's latest patents include "Control means for a gas turbine engine" and "Integrated control system for a gas turbine engine." The first patent focuses on a clearance control mechanism for compressor blades, which involves developing signals that represent various temperatures and speeds. This system allows for precise control of the clearance between compressor blades and the casing, ensuring optimal performance. The second patent describes an integrated control system that utilizes signals from multiple engine sensors to regulate parameters such as fan exhaust nozzle area and fuel flow, ultimately maintaining engine thrust and minimizing noise.

Career Highlights

Throughout his career, Richard S Beitler has worked with the United States of America as represented by the Administrator of the. His innovative work in gas turbine technology has positioned him as a key figure in the field, contributing to advancements that benefit both military and civilian aviation.

Collaborations

Beitler has collaborated with notable colleagues, including Jack E Cornett and Andrew A Saunders, Jr. These partnerships have fostered a collaborative environment that encourages innovation and the sharing of ideas.

Conclusion

Richard S Beitler's contributions to gas turbine engine control systems exemplify his dedication to innovation in engineering. His patents reflect a commitment to enhancing the efficiency and performance of gas turbine engines, making a lasting impact in the field.

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