Vaux Le Penil, France

Bruno R Masse

This inventor holds 2 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: Bruno R Masse. Retrieved from https://idiyas.com/inventor/bruno-r-masse

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

Calculating rank

% Patents Active = 100.0

Average Co-Inventor Count = 6.9

ph-index = 2

Forward Citations = 68(Granted Patents)


Company Filing History:


Years Active: 1993-1997

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2 patents (USPTO):Explore Patents

Title: Innovations of Bruno R Masse in Gas Turbine Technology

Introduction

Bruno R Masse is a notable inventor based in Vaux Le Penil, France. He has made significant contributions to the field of gas turbine technology, holding two patents that showcase his innovative approach to engineering challenges.

Latest Patents

One of his latest patents is titled "Gas turbine engine having an integral guide vane and separator diffuser." This invention discloses a separator-diffuser for a gas turbine engine, where the diffuser includes 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 features a wall that defines a generally annular oxidizer flow passage, allowing the oxidizer to pass from the oxidizer compressor into the flow passage. Additionally, a generally annular separator member divides the oxidizer flow passage into separate flow paths, directing the oxidizer towards an array of fuel injection heads.

Another significant patent by Masse is the "Gas turbine combustion chamber wall structure for minimizing cooling." This invention consists of a combustion chamber wall structure formed of multiple segments, each with an upstream and downstream portion. The overlapping portions of these segments create a cooling air chamber, allowing for efficient cooling of the combustion chamber. The design maximizes the distance along the inner surface of the segment for cooling air flow, enhancing the overall efficiency of the gas turbine.

Career Highlights

Bruno R Masse is associated with the Société Nationale d'Étude et de Construction de Moteurs d'Aviation, a company known for its advancements in aviation engine technology. His work has contributed to the development of more efficient and effective gas turbine engines.

Collaborations

Masse has collaborated with notable colleagues such as Gerard Y Barbier and Jean-Paul D Alary, further enhancing the innovative efforts within his field.

Conclusion

Bruno R Masse's contributions to gas turbine technology through his patents reflect his commitment to innovation and engineering excellence. His work continues to influence advancements in the aviation industry.

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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