Melun, France

Francois J Mirville

This inventor holds 5 USPTO granted patents. Top assignee: Societe Nationale D'etude Et De Construction De Moteurs D'aviation. Active years: 1991-1997.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Francois J Mirville. Retrieved from https://idiyas.com/inventor/francois-j-mirville

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


% Patents Active = 100.0

Average Co-Inventor Count = 1.9

ph-index = 4

Forward Citations = 190(Granted Patents)


Location History:

  • Melun, FR (1991 - 1993)
  • Hericy, FR (1997)

Company Filing History:


Years Active: 1991-1997

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5 patents (USPTO):Explore Patents

Title: The Innovative Contributions of Francois J Mirville

Introduction

Francois J Mirville is a notable inventor based in Melun, France. He has made significant contributions to the field of engineering, particularly in the development of advanced gas turbine technologies. With a total of five patents to his name, Mirville's work has had a profound impact on the efficiency and design of gas turbine engines.

Latest Patents

One of Mirville's latest patents is for a gas turbine engine featuring an integral guide vane and separator diffuser. This innovative design incorporates axial walls that function as a guide vane stage for the oxidizer compressor. By integrating the last guide vane stage into the diffuser structure, the overall axial length and bulk of the gas turbine engine can be significantly reduced. The separator-diffuser includes a wall that defines a generally annular oxidizer flow passage, allowing the oxidizer to flow from the compressor into the passage. Additionally, a separator member divides the oxidizer flow passage into separate paths, directing the oxidizer towards the fuel injection heads.

Another significant patent by Mirville is a turbopump system designed for driving multiple pumps. This system features a series of concentric turbine rotors within a turbine casing, each connected directly to a pump impeller. The design allows for the simultaneous pumping of two separate fluids, enhancing operational efficiency. The propellant fluid is directed through an annular space between the turbine rotors, which rotate in opposite directions, driven by turbine blades that extend into this space.

Career Highlights

Francois J Mirville is associated with the Société Nationale d'Étude et de Construction de Moteurs d'Aviation, a company renowned for its contributions to aviation engine technology. His work at this institution has allowed him to push the boundaries of gas turbine design and functionality.

Collaborations

Throughout his career, Mirville has collaborated with esteemed colleagues such as Georges Mazeaud and Jean-Paul D Alary. These partnerships have fostered an environment of innovation and creativity, leading to groundbreaking advancements in their field.

Conclusion

Francois J Mirville's contributions to gas turbine technology exemplify the spirit of innovation in engineering. His patents reflect a commitment to enhancing efficiency and performance in aviation engines. Through his work and collaborations, Mirville continues to influence the future of aerospace engineering.

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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