Serge M Meunier

This inventor holds 8 USPTO granted patents. Top assignee: Societe Nationale D'etude Et De Construction De Moteurs D'aviation. Active years: 1993-1997.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Serge M Meunier. Retrieved from https://idiyas.com/inventor/serge-m-meunier

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

USPTO Granted Patents = 8

% Patents Active = 100.0

Average Co-Inventor Count = 4.0

ph-index = 7

Forward Citations = 131(Granted Patents)

Company Filing History:

8 out of 701

Societe Nationale D'etude Et De Construction De Moteurs D'aviation

patents

Years Active: 1993-1997

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8 patents (USPTO):Sort by Forward CitationsExplore Patents

1. 5598697 - Double wall construction for a gas turbine combustion chamber (1997-02-04),

2. 5499499 - Cladded combustion chamber construction (1996-03-19),

3. 5339622 - Gas turbine engine with improved water ingestion prevention (1994-08-23),

4. 5295354 - Low pollution combustion chamber for a turbojet engine (1994-03-22),

5. 5261239 - Lean premixture combustion-chamber comprising a counterflow enclosure to (1993-11-16),

6. 5235805 - Gas turbine engine combustion chamber with oxidizer intake flow control (1993-08-17),

7. 5211675 - Variable volume combustion chamber for a gas turbine engine (1993-05-18),

8. 5209066 - Counter flow combustion chamber for a gas turbine engine (1993-05-11),

Title: Innovations of Serge M Meunier

Introduction

Serge M Meunier is a notable inventor based in Le Chatelet en Brie, France. He has made significant contributions to the field of gas turbine technology, holding a total of eight patents. His work focuses on enhancing the efficiency and functionality of combustion chambers in gas turbines.

Latest Patents

Among his latest patents is the "Double wall construction for a gas turbine combustion chamber." This invention features a wall structure that includes a first wall with an inner surface forming a boundary of the combustion chamber. The outer surface is designed to prevent the formation of a cooling layer, thereby improving performance. Additionally, the invention incorporates a second wall that defines a cooling fluid circulatory space, allowing for effective cooling of the combustion chamber.

Another significant patent is the "Cladded combustion chamber construction." This design allows for cladding tiles to be assembled and replaced without disassembling the structural wall of the combustion chamber. The innovative use of channel-shaped attaching devices facilitates the easy attachment of cladding tiles, enhancing the overall efficiency of the combustion chamber.

Career Highlights

Serge M Meunier is associated with the Société Nationale d'Étude et de Construction de Moteurs d'Aviation, a company renowned for its advancements in aviation engine technology. His work has been instrumental in developing innovative solutions that address the challenges faced in gas turbine design and construction.

Collaborations

Throughout his career, Serge has collaborated with notable colleagues, including Michel A Desaulty and Xavier M Bardey. These partnerships have contributed to the successful development of his patented technologies.

Conclusion

Serge M Meunier's contributions to gas turbine technology through his innovative patents have significantly impacted the industry. His work continues to inspire advancements in combustion chamber design and efficiency.

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]