East Hartford, CT, United States of America

Eunice Allen-Bradley

This inventor holds 10 USPTO granted patents and 3 published patent applications and 7 EPO patents. Top assignees: United Technologies Corporation, Rtx Corporation. Active years: 2011-2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Eunice Allen-Bradley. Retrieved from https://idiyas.com/inventor/eunice-allen-bradley

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

USPTO Granted Patents = 10 

% Patents Active = 100.0

 

Average Co-Inventor Count = 2.3

ph-index = 6

Forward Citations = 101(Granted Patents)


Location History:

  • East Hartford, CT (US) (2011 - 2013)
  • Vernon, CT (US) (2015 - 2018)

Company Filing History:


Years Active: 2011-2026

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10 patents (USPTO):Explore Patents

Title: Innovations of Eunice Allen-Bradley

Introduction

Eunice Allen-Bradley is a notable inventor based in East Hartford, CT (US). She has made significant contributions to the field of gas turbine engine technology, holding a total of 9 patents. Her work focuses on innovative airfoil designs that enhance the performance and efficiency of gas turbine engines.

Latest Patents

One of her latest patents is titled "Airfoil design having localized suction side curvatures." This invention describes an airfoil for a gas turbine engine that features a radially extending body with a transverse cross-section. The design includes a leading edge, a trailing edge, a pressure side with predominantly concave curvature, and a suction side with predominantly convex curvature. The suction side also incorporates a flat portion flanked by convex portions, along with local curvature changes that create inflection points spaced from the trailing edge.

Another significant patent is the "Gas turbine engine turbine blade airfoil profile." This turbine blade includes an airfoil with leading and trailing edges connected by spaced pressure and suction sides. The external airfoil surface is designed to conform to multiple cross-sectional profiles defined by a set of Cartesian coordinates. These coordinates are scaled by local axial chords, ensuring precise aerodynamic performance.

Career Highlights

Eunice Allen-Bradley has built a successful career at United Technologies Corporation, where she has been instrumental in advancing gas turbine technology. Her innovative designs have contributed to the efficiency and effectiveness of turbine engines, making her a key figure in her field.

Collaborations

Throughout her career, Eunice has collaborated with talented individuals such as Thomas J Praisner and Eric A Grover. These partnerships have fostered a creative environment that has led to groundbreaking advancements in turbine technology.

Conclusion

Eunice Allen-Bradley exemplifies the spirit of innovation in the field of gas turbine engines. Her contributions through her patents and collaborations have significantly impacted the industry, showcasing her expertise and dedication to advancing technology.

Profile summary based on public USPTO records.
Data Sources: USPTO Patent Grant XML, Patent Center, EPO & CIPO • Normalized by IDiyas Innovation Graph. Methodology & provenance architecturePlease report any incorrect information to [email protected]
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