Avon, France

Gerard J Bayle-Laboure

This inventor holds 6 USPTO granted patents. Top assignees: Societe Nationale D'etude Et De Construction De Moteurs D'aviation, 501 Societe Nationale D'etude Et De Construction De Meteur. Active years: 1984-1989.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Gerard J Bayle-Laboure. Retrieved from https://idiyas.com/inventor/gerard-j-bayle-laboure

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 = 4.4

ph-index = 5

Forward Citations = 92(Granted Patents)


Location History:

  • Paris, FR (1984)
  • Avon, FR (1986 - 1989)

Company Filing History:


Years Active: 1984-1989

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6 patents (USPTO):Explore Patents

Title: Gerard J Bayle-Laboure: Innovator in Turbojet Engine Technology

Introduction

Gerard J Bayle-Laboure is a notable inventor based in Avon, France, recognized for his contributions to turbojet engine technology. With a total of six patents to his name, he has made significant advancements in the field of aviation engineering.

Latest Patents

One of his latest patents is an air-fuel injection system for a turbojet engine. This invention features an improved swirler system for the combustion chamber, where stationary first vanes and moveable second vanes are oriented at different angles. This design allows for the adjustment of the incoming air angle between full power and idle conditions, thereby varying the conical shape of the atomized air-fuel mixture according to the engine's operating conditions. Additionally, radial and axial inlet duct portions are included to attenuate the wakes of the air flow generated by the vanes before entering the combustion chamber. Another significant patent is for an enlarged bowl member for a turbojet engine combustion chamber. This fuel system enhances the engine's operating parameters across various conditions by increasing the reactive volume while ensuring adequate cooling to prevent burn-through or uneven performance. The bowl extends radially outward beyond the combustion chamber's base and includes a row of air inlet orifices to improve fuel atomization prior to ignition.

Career Highlights

Throughout his career, Gerard has worked with prominent companies in the aviation sector, including Société Nationale d'Étude et de Construction de Moteurs d'Aviation and 501 Société Nationale d'Étude et de Construction de Moteurs. His work has been instrumental in advancing turbojet engine technology.

Collaborations

Gerard has collaborated with notable colleagues such as Gerard Y Barbier and Michel A Desaulty, contributing to various projects that have furthered the field of aviation engineering.

Conclusion

Gerard J Bayle-Laboure's innovative work in turbojet engine technology has made a lasting impact on the aviation industry. His patents reflect a deep understanding of engineering principles and a commitment to improving engine performance.

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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