Chevilly-Larue, France

Marcel R Soligny

This inventor holds 20 USPTO granted patents, primarily in Gas Turbine Engineering. Top assignees: Societe Nationale D'etude Et De Construction De Moteurs D'aviation, Snecma. Active years: 1982-1997.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Marcel R Soligny. Retrieved from https://idiyas.com/inventor/marcel-r-soligny

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 = 2.2

ph-index = 12

Forward Citations = 436(Granted Patents)


Location History:

  • Chevilly-Larve, FR (1985)
  • Chevilly Larue, FR (1982 - 1997)

Company Filing History:


Years Active: 1982-1997

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Areas of Expertise:
Gas Turbine
Turbojet Engine
Nozzle
Sealing Device
Compressor
Turbomachine
Rotor
Cooling System
Variable Section
Combustion Chamber
Thrust Reverser
Containment Structure
20 patents (USPTO):Explore Patents

Title: Marcel R. Soligny: Innovator in Gas Turbine Technology

Introduction

Marcel R. Soligny, based in Chevilly-Larue, France, is a prominent inventor who has made significant contributions to the field of gas turbine technology. With a remarkable portfolio of 20 patents, Soligny has been at the forefront of innovation in aeronautical engineering, focusing on advancements that enhance the efficiency and functionality of gas turbine engines.

Latest Patents

Among Soligny's latest inventions is the "Device for Cooling and Gas Turbine Rotor." This innovative device features a centrifugal compressor connected to a joint-carrier disk that is affixed to the upstream flange of the rotor disk to be cooled. The design allows for recompressed air to be ejected through channels located near the roots of the blades of the disk, showcasing a keen understanding of thermal management in turbine applications.

Another significant patent is the "Gas Turbine Engine Rotor Blading Sealing Device." This invention introduces a sealing mechanism for rotor blades that allows real-time adjustments of the clearances between the tips of the rotor blades and the sealing structure. The sealing shroud surrounding the turbine wheel is composed of sectors attached to both monolithic short and long response time rings. Air from upstream is directed onto these rings, facilitating radial expansion or contraction in sync with the rotor blades' operational changes, thereby maintaining optimal clearance throughout the engine's operational range.

Career Highlights

Throughout his career, Soligny has worked with notable companies such as Société Nationale d'Étude et de Construction de Moteurs d'Aviation and Snecma. His experiences in these prestigious organizations have undoubtedly played a pivotal role in honing his engineering and innovative skills in turbine development.

Collaborations

Marcel R. Soligny has collaborated with esteemed colleagues, including Gérard E. Jourdain and Jean G. Bouiller. These partnerships have further fueled collaboration and shared knowledge within the field of turbine technology, leading to pioneering developments in gas turbine efficiency and functionality.

Conclusion

With 20 patents to his name, Marcel R. Soligny exemplifies the spirit of innovation in the aerospace sector. His contributions, particularly in developing advanced cooling and sealing devices for gas turbines, continue to influence modern engineering practices and enhance the performance of turbine engines globally. Soligny's legacy as an inventor and collaborator is marked by a commitment to advancing technology that benefits both the industry and society.

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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