Thierry Georges Paul Papin

This inventor holds 24 USPTO granted patents and 3 published patent applications, plus 1 CIPO patent and 11 EPO patents, primarily in Turbomachinery Engineering. Top assignees: Safran Aircraft Engines, Snecma. Active years: 2014-2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Thierry Georges Paul Papin. Retrieved from https://idiyas.com/inventor/thierry-georges-paul-papin

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

USPTO Granted Patents = 24 (Patent Applications = 3)

% Patents Active = 100.0

CIPO Patents = 1 (Patent Applications = 1)

EPO Patents = 11 (Patent Applications = 14)

Average Co-Inventor Count = 3.2

ph-index = 5

Forward Citations = 54(Granted Patents)

Location History:

Varennes-Jarcy, FR (2014 - 2021)
Moissy-Cramayel, FR (2020 - 2024)

Company Filing History:

17 out of 1,948

Safran Aircraft Engines

Years Active: 2014-2026

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Areas of Expertise:

Noise Reduction

Turbomachine

Variable-Pitch Blades

Aircraft Engine

Vane Pitch Setting

Lubricant Cooling

Acoustic Treatment

Flow Guide Vane

Fan Frame

Casing Structure

Turbine Engine

Structural Frame

24 patents (USPTO):Sort by Forward CitationsExplore Patents

1. 12753720 - Noise reducing device having an obliquely pierced honeycomb structure (2026-10-06),

2. 12448110 - Assembly comprising a vane and a vane pitch setting system (2025-10-21),

3. 12270348 - Sealing device for a discharge valve of a turbomachine (2025-04-08),

4. 12098690 - Assembly for an aircraft turbine engine, comprising means for the axial and radial retention of a fan (2024-09-24),

5. 12012201 - Assembly comprising a vane and a vane pitch setting system (2024-06-18),

6. 11780562 - Turbomachine module for a propeller having variable-pitch blades and turbomachine comprising same (2023-10-10),

7. 11753143 - Turbomachine module equipped with a system for changing the pitch of the blades of a propeller and with a device for feathering the blades (2023-09-12),

8. 11428199 - Turbomachine module for a variable pitch blade propeller and turbomachine comprising it (2022-08-30),

9. 11143045 - Intermediate case for an aircraft turbomachine made from a single casting with a lubricant duct (2021-10-12),

10. 10907489 - Vaned ring for turbomachine stator having vanes connected to an outer shell by conical seating and frangible pin (2021-02-02),

11. 10723476 - Ring of turbojet vanes including an acoustic treatment structure (2020-07-28),

12. 10697312 - Outlet guide vane for aircraft turbomachine, with improved lubricant cooling function (2020-06-30),

13. 10662974 - Turbine engine flow guide vane with removable attachment (2020-05-26),

14. 10648356 - Bypass turbomachine fitted with bleed system (2020-05-12),

15. 10392955 - Turbomachine fan frame comprising improved attachment means (2019-08-27),

Title: Innovations by Thierry Georges Paul Papin

Introduction

Thierry Georges Paul Papin is a prolific inventor based in Varennes-Jarcy, France, holding a total of 21 patents. His contributions primarily focus on advancements in aircraft turbine engine technology. With a career spanning notable companies in the aviation sector, he has made significant strides in engineering and innovation.

Latest Patents

Among his recent patents, two standout inventions showcase his expertise:

1. **Assembly for an Aircraft Turbine Engine**: This assembly comprises means for the axial and radial retention of a fan. It features an internal annular structure that houses an epicyclic gear train equipped with a planet carrier, along with a secondary retention device for the ring gear. This innovative design allows for efficient cooperation between projections that ensure stability and functionality within the turbine engine.

2. **Assembly Comprising a Vane and a Vane Pitch Setting System**: This assembly includes an un-ducted propeller blade with a bulbous portion at its root and a pitch setting system. The design incorporates a locking member and a radial retention prong that help secure the blade within the outer casing. This invention highlights a combination of simplicity and effectiveness in improving aircraft engine performance.

Career Highlights

Throughout his career, Thierry has worked with prestigious companies such as Safran Aircraft Engines and Snecma. His experience in these leading aviation firms has allowed him to hone his skills and contribute groundbreaking innovations to the field of aerospace engineering.

Collaborations

In his journey as an inventor, Thierry has collaborated with notable colleagues, including Cedric Zaccardi and Kaelig Merwen Orieux. These partnerships have fostered a productive environment for generating innovative solutions and advancing their shared goals in aircraft technology.

Conclusion

Thierry Georges Paul Papin continues to be an influential figure in aerospace engineering through his numerous patents and collaborations. His work on aircraft turbine engine systems not only enhances performance but also sets the stage for future innovations in the aviation industry. The impact of his inventions promises to lead to safer and more efficient aircraft designs, solidifying his reputation as a leading inventor in the field.

Profile summary based on public USPTO records.