San Diego, CA, United States of America

Sheila Cornejo

This inventor holds 1 USPTO granted patent. Top assignee: Rohr, Inc.. Active years: 2005.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Sheila Cornejo. Retrieved from https://idiyas.com/inventor/sheila-cornejo

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

Calculating rank

Average Co-Inventor Count = 5.0

ph-index = 1

Forward Citations = 43(Granted Patents)


Company Filing History:


Years Active: 2005

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1 patent (USPTO):Explore Patents

Title: Sheila Cornejo and Her Patent for Turbofan Thrust Reverser Design.

Introduction

Sheila Cornejo is an inventor associated with San Diego, California, and Rohr, Inc. Her patent work addresses aircraft engine technology, particularly the control of airflow from a turbofan thrust reverser.

Latest Patents

The available information lists one patent for Cornejo: “Cascadeless Fan Thrust Reverser with Plume Control.” The invention describes a thrust reverser that directs air from a turbofan engine’s air duct through an outlet formed when a translating cowl moves to its open position. Shaped surfaces on the bulkhead and kicker plate can help control the forward component of the discharged airflow. A plume control device can divide the flow into multiple plumes, while an aft vane guides air toward the outlet to manage turning and area matching. Cornejo is credited with 1 patent in the information provided.

Career Highlights

Cornejo’s listed patent reflects work on thrust-reverser design and airflow management for turbofan engines. The patent identifies Rohr, Inc. as her company affiliation.

Collaborations

The provided information names Stuart James Byrne and Randall J. Seaver as Cornejo’s coworkers. Their specific roles in the patent or related work are not stated.

Conclusion

Sheila Cornejo’s listed invention focuses on controlling airflow and plume formation in a turbofan thrust reverser, highlighting her contribution to aircraft engine 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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