For the Inventor, By the Inventor

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Reno, NV, United States of America

Aerion Corporation

USPTO Granted Patents = 20

% Expired Patents = 35.0

CIPO Patents = 3

EPO Patents = 3

Trademarks = 3

Forward Citations = 91

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11 inventors (with patents filed for the assignee):

James D Chase (13 out of 14 patents)

Peter Sturdza (9 out of 18 patents)

Richard R Tracy (6 out of 10 patents)

4. David L Rodriguez (4 out of 5 patents)

5. Michael Lorenzo Henderson (3 out of 20 patents)

6. German Andres Garzon (3 out of 3 patents)

7. Dev G Rajnarayan (2 out of 9 patents)

8. Ilan Kroo (2 out of 16 patents)

9. Sturdza Peter (2 out of 2 patents)

10. Herve Martins-Rivas (1 out of 12 patents)

11. Yoshifumi Suzuki (1 out of 1 patent)

12. Aerion Corporation (0 patent)

20 patents: Sort by Forward Citations

1. 9494482 - Predicting transition from laminar to turbulent flow over a surface using mode-shape parameters (2016-11-15),

2. 9348956 - Generating a simulated fluid flow over a surface using anisotropic diffusion (2016-05-24),

3. 9233755 - Highly efficient supersonic laminar flow wing structure (2016-01-12),

4. 8991768 - Highly efficient transonic laminar flow wing (2015-03-31),

5. 8935140 - Generating inviscid and viscous fluid-flow simulations over a surface using a fluid-flow mesh (2015-01-13),

6. 8892408 - Generating inviscid and viscous fluid flow simulations over a surface using a quasi-simultaneous technique (2014-11-18),

7. 8882028 - Aircraft emergency and backup secondary power apparatus (2014-11-11),

8. 8538738 - Predicting transition from laminar to turbulent flow over a surface (2013-09-17),

9. 8457939 - Generating inviscid and viscous fluid-flow simulations over an aircraft surface using a fluid-flow mesh (2013-06-04),

10. 8448893 - Laminar flow wing optimized for transonic cruise aircraft (2013-05-28),

11. 8437990 - Generating a simulated fluid flow over an aircraft surface using anisotropic diffusion (2013-05-07),

12. 8371124 - Jet nozzle plug with varying, non-circular cross sections (2013-02-12),

13. 8317128 - Laminar flow wing optimized for transonic cruise aircraft (2012-11-27),

14. 8272594 - Laminar flow wing optimized for supersonic cruise aircraft (2012-09-25),

15. 7967241 - Supersonic aircraft jet engine installation (2011-06-28),

Aerion Corporation, headquartered in Reno, NV, is a pioneering aerospace company focused on the development of supersonic aircraft. The organization specializes in advanced aerodynamics, propulsion systems, and sustainable aviation technologies. Aerion aims to revolutionize air travel by creating efficient, high-speed aircraft that minimize environmental impact. With a commitment to innovation, the company is at the forefront of the aerospace industry, striving to enhance global connectivity while adhering to stringent sustainability standards.

Profile summary based on public USPTO records.

Company Badge

USPTO Data Jan 1 1976 - Sep 29 2026

Aerion Corporation

20 Patents

#30 in Reno, NV

#127 in Nevada

#16,368 in US

#31,196 in the World

Reno, NV, United States of America

Aerion Corporation

Forward Citations = 91

11 inventors:

James D Chase (13 out of 14 patents)

Peter Sturdza (9 out of 18 patents)

Richard R Tracy (6 out of 10 patents)

4. David L Rodriguez (4 out of 5 patents)

5. Michael Lorenzo Henderson (3 out of 20 patents)

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