TOULOUSE, France

Louise Revy

This inventor holds 1 USPTO granted patent. Top assignee: Airbus Operations (s.a.s.). Active years: 2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Louise Revy. Retrieved from https://idiyas.com/inventor/louise-revy

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 = 1.0

ph-index = 1


Company Filing History:


Years Active: 2026

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1 patent (USPTO):Explore Patents

Title: Louise Revy and an Aircraft Engine Attachment System

Introduction

Louise Revy is an inventor associated with Toulouse, France, and Airbus Operations (S.A.S.). Her patent work concerns an aircraft engine attachment system designed to connect an aircraft’s motive-power unit to the primary structure of an aircraft pylon.

Latest Patents

Revy is named on 1 patent: “Aircraft engine attachment system comprising a two-point shackle equipped with at least one stop, aircraft comprising at least one such engine attachment system.” The invention describes a clevis block secured to the pylon structure or motive-power unit and a two-point shackle with a body and an integral extension. One or more stops on the extension face the clevis block’s flanges. A connection pin passes through the shackle body, with a ball-joint connection positioned between the body and the pin.

Career Highlights

The available information identifies Revy’s work with Airbus Operations (S.A.S.) and highlights her contribution to aircraft engine attachment technology. The patent describes components intended to connect an aircraft engine assembly to its supporting pylon structure.

Collaborations

Michael Berjot is identified as Revy’s coworker. The provided information does not specify his role in the patent or the nature of their collaboration.

Conclusion

Louise Revy’s listed patent focuses on an aircraft engine attachment system that uses a two-point shackle, stops, and a ball-joint connection to link the motive-power unit with the aircraft pylon structure.

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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