Clayton Stuart Cooper

This inventor holds 78 USPTO granted patents and 48 published patent applications and 14 EPO patents, primarily in Gas Turbine Combustion. Top assignee: General Electric Company. Active years: 2005-2026.

USPTO Granted Patents = 78 (Patent Applications = 48)

% Patents Active = 100.0

EPO Patents = 14 (Patent Applications = 33)

Average Co-Inventor Count = 5.1

ph-index = 6

Forward Citations = 123(Granted Patents)

Forward Citations (Not Self Cited) = 78(Dec 10, 2025)

Location History:

Loveland, OH (US) (2005 - 2024)
Evendale, OH (US) (2023 - 2024)
Clifton Park, NY (US) (2024)

Company Filing History:

77 out of 52,347

General Electric Company

patents

where one patent can have more than one assignee

Years Active: 2005-2026

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Areas of Expertise:

Gas Turbine

Combustor

Fuel Nozzle

Steam Injection

Vortex Cavity

Rotating Detonation

Fuel Passage

Swirler Assembly

Combustion Section

Turbine Engine

Hydrogen Fuel

78 patents (USPTO):Sort by Forward CitationsExplore Patents

1. 12742550 - Turbine engine including a combustor (2026-09-22),

2. 12723758 - Fuel nozzle and swirler (2026-09-01),

3. 12716586 - Turbine engine having a combustion section with a fuel nozzle having a gaseous fuel supply channel (2026-08-25),

4. 12710175 - COMBUSTION SECTION FOR A TURBINE ENGINE (2026-08-18),

5. 12693019 - Gas turbine engine and fuel nozzle assembly therefor (2026-07-28),

6. 12655980 - Fuel nozzle and swirler (2026-06-16),

7. 12613036 - Turbine engine having a combustion section with a fuel nozzle (2026-04-28),

8. 12601485 - Turbine engine with fuel nozzle (2026-04-14),

9. 12577917 - Method of operating a gas turbine engine (2026-03-17),

10. 12571539 - Turbine engine having a combustion section with a fuel nozzle (2026-03-10),

11. 12560324 - Combustion section with a primary combustor and a set of secondary combustors (2026-02-24),

12. 12535215 - Combustor including a steam injector operably injecting steam into a trapped vortex cavity (2026-01-27),

13. 12492819 - Gas turbine engine fuel nozzle having a secondary fuel passage through a swirler (2025-12-09),

14. 12486982 - Combustor having a main chamber and one or more trapped vortex cavities (2025-12-02),

15. 12429220 - Combustion section with a primary combustor and a set of secondary combustors (2025-09-30),

Title: Innovations by Clayton Stuart Cooper: Pioneering Patents in Combustion Technology

Introduction

Clayton Stuart Cooper, based in Loveland, Ohio, is a renowned inventor with an impressive portfolio of 55 patents. His work primarily focuses on advancements in turbine engine combustion technology, contributing significantly to the field of engineering and energy.

Latest Patents

Cooper's latest inventions include groundbreaking designs in combustion sections for turbine engines. One of his notable patents involves a combustion section featuring a primary combustion chamber and a secondary combustion chamber. This innovative design includes a combustor liner and a dome wall, with a primary fuel nozzle that is fluidly coupled to enhance performance. Additionally, he has developed a gas turbine fuel nozzle with an inner air passage and multiple outer fuel passages, providing improved flame control and fuel mixing before combustion.

Career Highlights

Clayton Cooper's career is marked by his association with General Electric Company, a leader in technology and manufacturing. His contributions have been vital in enhancing the efficiency and effectiveness of combustion processes in turbine engines, pushing the boundaries of traditional designs.

Collaborations

Throughout his career, Cooper has had the privilege of collaborating with esteemed colleagues such as Steven Clayton Vise and Pradeep Naik. These partnerships have fostered innovation and have led to the development of cutting-edge technologies that address the complexities of modern combustion systems.

Conclusion

Clayton Stuart Cooper exemplifies the essence of innovation in the field of combustion technology. His extensive patent portfolio and collaborative efforts demonstrate a relentless pursuit of excellence that continues to influence the engineering landscape. As the industry evolves, Cooper’s contributions remain pivotal in shaping the future of turbine engine technology.