Olivier Arnaud Fabien Lambert

This inventor holds 7 USPTO granted patents and 5 EPO patents. Top assignee: Safran Aircraft Engines. Active years: 2020-2024.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Olivier Arnaud Fabien Lambert. Retrieved from https://idiyas.com/inventor/olivier-arnaud-fabien-lambert

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

USPTO Granted Patents = 7

% Patents Active = 100.0

EPO Patents = 5 (Patent Applications = 5)

Average Co-Inventor Count = 3.4

ph-index = 1

Forward Citations = 4(Granted Patents)

Location History:

Moissy-Cramayel, FR (2020 - 2022)
Sceaux, FR (2022)

Company Filing History:

7 out of 1,948

Safran Aircraft Engines

patents

Years Active: 2020-2024

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7 patents (USPTO):Sort by Forward CitationsExplore Patents

1. 12110840 - Turbine engine separate flow mixer with lobes (2024-10-08),

2. 11225906 - Device for maintaining at least one cooling tube on a turbomachine casing and the mounting method thereof (2022-01-18),

3. 11215066 - Sealing ring element for a turbine comprising an inclined cavity in an abradable material (2022-01-04),

4. 11208909 - Turbine engine and air-blowing sealing method (2021-12-28),

5. 11156129 - Turbine engine casing (2021-10-26),

6. 10760441 - Turbine for a turbine engine (2020-09-01),

7. 10633984 - Turbine for a turbine engine (2020-04-28),

Title: Olivier Arnaud Fabien Lambert: Innovator in Turbomachinery

Introduction

Olivier Arnaud Fabien Lambert is a notable inventor based in Moissy-Cramayel, France. He has made significant contributions to the field of turbomachinery, holding a total of 7 patents. His innovative designs focus on enhancing the efficiency and functionality of turbine engines.

Latest Patents

One of his latest patents is a turbine engine separate flow mixer with lobes. This invention relates to a turbine engine separate flow mixer centered on a longitudinal axis. It comprises an exhaust housing and a shroud directly connected to the exhaust housing, intended to mix the flows originating in the turbine engine. The shroud consists of a metal sheet formed by a succession of first and second longitudinal strips, which are distributed circumferentially around the longitudinal axis of the mixer. The design allows for the formation of grooves in the shroud when operating, defined by an alternation of internal and external lobes. Another significant patent is a device for maintaining at least one cooling tube on a turbomachine casing, which includes a method for mounting the cooling tube outside the turbomachine casing.

Career Highlights

Olivier is currently employed at Safran Aircraft Engines, a leading company in the aerospace industry. His work focuses on developing advanced technologies that improve the performance of aircraft engines. His innovative spirit and technical expertise have made him a valuable asset to his team.

Collaborations

Olivier has collaborated with several talented individuals in his field, including Gaël Frédéric Claude Cyrille Evain and Cyrille Telman. These collaborations have fostered a creative environment that encourages the development of groundbreaking technologies.

Conclusion

Olivier Arnaud Fabien Lambert is a distinguished inventor whose work in turbomachinery has led to several important patents. His contributions continue to shape the future of aerospace technology, demonstrating the impact of innovation in this critical industry.

Profile summary based on public USPTO records.