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For the Inventor, By the Inventor

Melun, France

Damien Bonneau

This inventor holds 11 USPTO granted patents and 2 published patent applications and 8 EPO patents. Top assignees: Safran Aircraft Engines, Snecma, Herakles. Active years: 2009-2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Damien Bonneau. Retrieved from https://idiyas.com/inventor/damien-bonneau-ftofgthu

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

USPTO Granted Patents = 11 

% Patents Active = 100.0

 

Average Co-Inventor Count = 4.2

ph-index = 3

Forward Citations = 47(Granted Patents)


Location History:

  • Melun, FR (2009 - 2019)
  • Moissy-Cramayel, FR (2022 - 2024)

Company Filing History:

goldMedal7 out of 1,944 
 
Safran Aircraft Engines
 patents
silverMedal4 out of 1,659 
 
Snecma
 patents
bronzeMedal1 out of 91 
 
Herakles
 patents
where one patent can have more than one assignee

Years Active: 2009-2026

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11 patents (USPTO):Explore Patents
1. 12669059 - Air injection casing for a turbomachine (2026-06-30),
2. 12492644 - High-pressure gas turbine for turbomachine and turbomachine (2025-12-09),
3. 12345161 - High-pressure gas turbine for a turbine engine and turbine engine (2025-07-01),
4. 12000290 - Control method and unit for controlling the clearance of a high-pressure turbine to reduce the effect of EGT overshoot (2024-06-04),
5. 11319830 - Control of clearance between aircraft rotor blades and a casing (2022-05-03),
6. 11221141 - Assembly for a turbomachine (2022-01-11),
7. 10487689 - Turbine casing comprising ring sector attachment means (2019-11-26),
8. 9476690 - Method for controlling the clearance at the tips of blades of a turbine rotor (2016-10-25),
9. 9080463 - Turbine ring assembly (2015-07-14),
10. 8899913 - Assembly including a turbine disk for a gas turbine engine and a bearing-supporting journal, and cooling circuit for the turbine disk of such an assembly (2014-12-02),
11. 7530788 - Hollow turbomachine blade (2009-05-12),

Title: The Innovative Contributions of Damien Bonneau

Introduction

Damien Bonneau is a notable inventor based in Melun, France. He has made significant contributions to the field of turbine engine technology, holding a total of 11 patents. His work focuses on enhancing the efficiency and performance of high-pressure gas turbines.

Latest Patents

Among his latest patents is a high-pressure gas turbine designed for turbomachines. This innovative turbine includes a nozzle guide vane assembly, an annular array of movable blades, and multiple recirculation cavities. Another significant patent involves a control method and unit for managing the clearance of a high-pressure turbine. This method aims to reduce the effects of exhaust gas temperature (EGT) overshoot by estimating the clearance between the rotor blades and the turbine ring, utilizing various parameters to optimize performance.

Career Highlights

Throughout his career, Damien has worked with prominent companies in the aerospace sector, including Safran Aircraft Engines and Snecma. His experience in these organizations has allowed him to develop cutting-edge technologies that contribute to advancements in turbine engine design.

Collaborations

Damien has collaborated with several talented individuals in his field, including Antoine Bruno Van Noort and Christophe Javelot. These partnerships have fostered innovation and have been instrumental in the development of his patented technologies.

Conclusion

Damien Bonneau's contributions to turbine engine technology are noteworthy, and his patents reflect his commitment to innovation in the aerospace industry. His work continues to influence the design and efficiency of high-pressure gas turbines.

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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