Ellington, CT, United States of America

David D Chapdelaine

This inventor holds 2 USPTO granted patents. Top assignee: Rtx Corporation. Active years: 2024-2025.


% Patents Active = 100.0

Average Co-Inventor Count = 5.5

ph-index = 1


Company Filing History:


Years Active: 2024-2025

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2 patents (USPTO):Explore Patents

Title: David D Chapdelaine: Innovator in Gas Turbine Technology

Introduction

David D Chapdelaine is a notable inventor based in Ellington, CT (US). He has made significant contributions to the field of gas turbine technology, holding 2 patents that showcase his innovative approach to engineering.

Latest Patents

Chapdelaine's latest patents include the "Airfoil Cooling Circuit" and "Non-Circular Stress Reducing Crossover." The Airfoil Cooling Circuit patent describes an airfoil for a gas turbine engine that features a first wall in an interior cavity, extending in the spanwise direction and forming a cooling channel. It also includes a second wall that creates another cooling channel, connected by holes that facilitate airflow. The Non-Circular Stress Reducing Crossover patent outlines an airfoil designed to extend radially from an inner diameter to an outer diameter, incorporating a body with a cooling channel and a tapered hole for efficient airflow management.

Career Highlights

David D Chapdelaine is currently employed at RTX Corporation, where he continues to develop innovative solutions in gas turbine technology. His work has been instrumental in advancing the efficiency and performance of gas turbine engines.

Collaborations

Throughout his career, Chapdelaine has collaborated with talented individuals such as Dana K Bondarevsky and Christopher Perron. These collaborations have contributed to the successful development of his patented technologies.

Conclusion

David D Chapdelaine is a distinguished inventor whose work in gas turbine technology has led to significant advancements in the field. His innovative patents reflect his commitment to engineering excellence and contribute to the ongoing evolution of gas turbine design.

Profile summary based on public USPTO records.
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