Cincinnati, OH, United States of America

Emily Anne Clausing

This inventor holds 1 USPTO granted patent. Top assignee: General Electric Company. Active years: 2005.


% Patents Active = 100.0

Average Co-Inventor Count = 5.0

ph-index = 1

Forward Citations = 18(Granted Patents)


Company Filing History:


Years Active: 2005

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1 patent (USPTO):Explore Patents

Title: Emily Anne Clausing: Innovator in Gas Turbine Technology

Introduction

Emily Anne Clausing is a notable inventor based in Cincinnati, OH (US). She has made significant contributions to the field of gas turbine technology. Her innovative approach has led to the development of a unique patent that enhances the efficiency and functionality of gas turbine engines.

Latest Patents

Emily holds a patent for a "Snap on blade shim." This invention includes a gas turbine engine blade root shim that features a dovetail shim portion with a dovetail shape. The design incorporates a longitudinally extending substantially flat base with distinct forward and aft ends. The shim is specifically designed for a blade dovetail root, ensuring a perfect fit within the root slot formed in the bottom of the dovetail root. This innovative shim design aims to improve the performance and reliability of gas turbine engines.

Career Highlights

Emily is currently employed at General Electric Company, where she continues to push the boundaries of engineering and innovation. Her work has been instrumental in advancing gas turbine technology, making her a valuable asset to her team and the industry.

Collaborations

Emily has collaborated with notable colleagues, including Robert Russell Grant and John Gregory Cargill. These partnerships have fostered a creative environment that encourages the development of groundbreaking technologies.

Conclusion

Emily Anne Clausing is a pioneering inventor whose work in gas turbine technology exemplifies innovation and engineering excellence. Her contributions, particularly her patented snap on blade shim, highlight her commitment to enhancing the efficiency of gas turbine engines.

Profile summary based on public USPTO records.
Please report any incorrect information to [email protected]
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