Indianapolis, IN, United States of America

Michael S Bell

USPTO Granted Patents = 2 

 

 

Average Co-Inventor Count = 2.9

ph-index = 1

Forward Citations = 4(Granted Patents)


Company Filing History:


Years Active: 2017-2019

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2 patents (USPTO):Explore Patents

Title: Michael S. Bell: Innovator in Gas Turbine Technology

Introduction

Michael S. Bell is a notable inventor based in Indianapolis, IN (US), recognized for his contributions to gas turbine technology. With a total of 2 patents, Bell has made significant advancements in the design and functionality of combustor systems.

Latest Patents

One of Bell's latest patents is the "Dual-wall impingement, convection, effusion combustor tile." This innovation involves a gas turbine engine that features a combustor with a dual-wall impingement convection effusion combustor tile assembly. The design enhances cooling efficiency through a dedicated air flow channel and secure attachments to the cold skin liner of the combustor. The dual-wall construction minimizes parasitic leakage and improves performance at lower temperatures. Another significant patent is the "Flexible bellows igniter seal." This invention presents a flexible bellows assembly designed to seal an engine igniter. The assembly can be mounted to a combustor diffuser, creating a sealed chamber that allows an igniter to pass through and provide ignition to the combustor.

Career Highlights

Throughout his career, Michael S. Bell has worked with prominent companies in the aerospace sector, including Rolls-Royce Corporation and Rolls-Royce North American Technologies Inc. His work has focused on enhancing the efficiency and reliability of gas turbine engines.

Collaborations

Bell has collaborated with esteemed colleagues such as Russell N. Bennett and Jack D. Petty, Sr., contributing to the advancement of technology in their field.

Conclusion

Michael S. Bell's innovative work in gas turbine technology has led to significant advancements in engine design and efficiency. His patents reflect a commitment to improving performance and reliability in aerospace applications.

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