Christophe Marcel Lucien Perdrigeon

This inventor holds 21 USPTO granted patents and 5 published patent applications, plus 1 CIPO patent and 14 EPO patents, primarily in Turbomachinery Engineering. Top assignee: Safran Aircraft Engines. Active years: 2020-2026.

IDiyas Innovation Intelligence. (2026). Inventor Profile: Christophe Marcel Lucien Perdrigeon. Retrieved from https://idiyas.com/inventor/christophe-marcel-lucien-perdrigeon

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

USPTO Granted Patents = 21 (Patent Applications = 5)

% Patents Active = 100.0

CIPO Patents = 1 (Patent Applications = 1)

EPO Patents = 14 (Patent Applications = 15)

Average Co-Inventor Count = 3.6

ph-index = 3

Forward Citations = 28(Granted Patents)

Location History:

Ballainvilliers, FR (2020 - 2021)
Moissy-Cramayel, FR (2020 - 2024)

Company Filing History:

21 out of 1,944

Safran Aircraft Engines

patents

Years Active: 2020-2026

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Areas of Expertise:

Pitch Change Mechanism

Turbomachine

Heat Exchanger

Oil Distribution

Aircraft Turbine

Fan Module

Lubricant Duct

Thermal Conducting Matrix

Guide Vane

Acoustic Treatment

Intermediate Case

Reduction Gearbox

21 patents (USPTO):Sort by Forward CitationsExplore Patents

1. 12601272 - Pitch change mechanism with an actuator surrounding a fluid transfer bearing (2026-04-14),

2. 12553353 - Pitch-change mechanism with pitch-locking device comprising a satellite roller screw (2026-02-17),

3. 12460550 - Fan module equipped with an oil transfer device (2025-11-04),

4. 12247498 - System for changing the pitch of the blades of a turbomachine propeller (2025-03-11),

5. 12180912 - Turbine engine comprising a heat exchanger consisting of at least one deck between vanes (2024-12-31),

6. 12071865 - Air flow straightening stage for a turbomachine (2024-08-27),

7. 11982316 - Device for distributing oil from a rolling bearing for an aircraft turbine engine (2024-05-14),

8. 11982197 - Device for distributing oil from a rolling bearing for an aircraft turbine engine (2024-05-14),

9. 11946381 - Stator support for a fan shaft driven by a reduction gearbox in a turbomachine (2024-04-02),

10. 11686249 - Turbine engine comprising a heat exchanger in the secondary path (2023-06-27),

11. 11639665 - Turbomachine comprising a heat exchanger in the secondary path (2023-05-02),

12. 11346247 - Turbine engine including a heat exchanger formed in a platform (2022-05-31),

13. 11143045 - Intermediate case for an aircraft turbomachine made from a single casting with a lubricant duct (2021-10-12),

14. 11125091 - Aircraft turbo machine exit guide vane comprising a bent lubricant passage of improved design (2021-09-21),

15. 11015468 - Outlet guide vane for turbomachine, comprising a lubricant cooling passage equipped with a thermal conducting matrix compressed between the intrados and extrados walls (2021-05-25),

Title: The Innovative Journey of Christophe Marcel Lucien Perdrigeon

Introduction

Christophe Marcel Lucien Perdrigeon, an esteemed inventor based in Ballainvilliers, France, has made remarkable contributions to the field of aeronautics. With a prolific portfolio of 18 patents, Perdrigeon has established himself as a leading figure in the development of advanced turbomachine technologies.

Latest Patents

Among his notable inventions, two stand out for their innovation and impact on turbine engine performance:

1. **System for Changing the Pitch of the Blades of a Turbomachine Propeller** - This invention involves a sophisticated control system that allows for the adjustment of blade pitch in turbomachine propellers. Each blade is designed to pivot around its pitch axis, facilitated by a mechanism that includes a connecting rod and an eccentric. This design enhances the performance and efficiency of turbomachines by optimizing blade positioning.

2. **Turbine Engine Comprising a Heat Exchanger Consisting of at Least One Deck Between Vanes** - Perdrigeon's second latest patent focuses on an aircraft turbine engine that features a heat exchanger integrated between vanes. This innovative design allows for improved thermal management within the engine, utilizing pressurized air to facilitate heat exchange and improve overall functionality.

Career Highlights

Christophe Perdrigeon currently works with Safran Aircraft Engines, a company recognized for its commitment to aerospace innovation. His work in this prestigious organization emphasizes his role in advancing aerospace technologies and enhancing engine performance.

Collaborations

Throughout his career, Perdrigeon has collaborated closely with talented professionals such as Cedric Zaccardi and Cédric Zaccardi. These collaborations illustrate the team-oriented approach prevalent in the aerospace industry, where sharing knowledge and expertise leads to groundbreaking innovations.

Conclusion

With a deep understanding of turbomachine operations and an impressive list of patents, Christophe Marcel Lucien Perdrigeon continues to be a vital contributor to advancements in aerospace engineering. His innovative spirit and dedication to improving aircraft performance position him as a noteworthy inventor in the field.

Profile summary based on public USPTO records.