MOISSY-CRAMAYEL, France

Francesco Salvatori

This inventor holds 2 USPTO granted patents and 1 published patent application and 2 EPO patents. Top assignee: Safran Aircraft Engines. Active years: 2025.

USPTO Granted Patents = 2 

% Patents Active = 100.0

 

Average Co-Inventor Count = 5.0

ph-index = 1


Company Filing History:


Years Active: 2025

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2 patents (USPTO):Explore Patents

Title: Francesco Salvatori: Innovator in Turbine Technology

Introduction

Francesco Salvatori is a notable inventor based in Moissy-Cramayel, France. He has made significant contributions to the field of turbine technology, particularly in the design and functionality of high-pressure gas turbines.

Latest Patents

Salvatori holds a patent for a high-pressure gas turbine designed for turbine engines. This innovative turbine includes a nozzle guide vane assembly, an annular array of movable blades positioned downstream of the nozzle guide vane assembly, a first recirculation cavity, a second recirculation cavity, and a bleed cavity. Additionally, an upstream sealing element is mounted on the nozzle guide vane assembly, while a downstream sealing element is attached to the annular array of movable blades. This patent showcases his expertise in enhancing turbine efficiency and performance.

Career Highlights

Francesco Salvatori is currently employed at Safran Aircraft Engines, a leading company in the aerospace industry. His work focuses on advancing turbine technology, contributing to the development of more efficient and powerful engines.

Collaborations

Throughout his career, Salvatori has collaborated with talented professionals such as Damien Bonneau and Nicolas Contini. These partnerships have fostered innovation and have been instrumental in the success of various projects.

Conclusion

Francesco Salvatori's contributions to turbine technology through his patent and work at Safran Aircraft Engines highlight his role as a key innovator in the aerospace sector. His advancements continue to influence the efficiency and performance of turbine engines.

Profile summary based on public USPTO records.
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