Sherbrooke, France

Stéphane Moreau

This inventor holds 1 USPTO granted patent and 1 published patent application. Top assignees: Centre National De La Recherche Scientifique, Ecole Centrale De Lyon, Safran Aircraft Engines. Active years: 2023.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Stéphane Moreau. Retrieved from https://idiyas.com/inventor/stéphane-moreau-2uthj8yq

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

Calculating rank
USPTO Granted Patents = 1 

% Patents Active = 100.0

Average Co-Inventor Count = 4.0

ph-index = 1


Company Filing History:


Years Active: 2023

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1 patent (USPTO):Explore Patents

Title: Stéphane Moreau: Aircraft Engine Acoustics Inventor

Introduction

Stéphane Moreau is an inventor associated with Sherbrooke, France. His patent work addresses the design of a discharge grate for a turbine engine, with a focus on guiding gas flow and optimizing acoustics. He is credited with 1 patent.

Latest Patents

Moreau’s patent, “Acoustically Optimized Discharge Line Grid with Channels,” describes a perforated discharge grate intended for installation inside or at the outlet of a turbine-engine discharge valve conduit. The grate has parallel upstream and downstream faces, with orifices that carry gas through the plate. A coaxial tubular channel projects from the downstream face at each orifice, forming a structure designed to manage the gas flow and support acoustic optimization.

Career Highlights

Moreau’s listed professional affiliations include Safran Aircraft Engines and École Centrale de Lyon. The available information does not specify his roles or dates of employment at these organizations.

Collaborations

His listed coworkers include Paul Clément Guillaume Laffay and Marc Cornelius Jacob. Their specific contributions to the patented invention are not provided.

Conclusion

Stéphane Moreau’s patent presents a channel-based discharge grate design that combines gas-flow guidance with acoustic optimization for aircraft turbine-engine applications.

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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