The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 02, 2025

Filed:

Jun. 23, 2022
Applicant:

Goodrich Corporation, Charlotte, NC (US);

Inventors:

Marc J. Georgin, Dayton, OH (US);

Paul R. Burte, Clayton, OH (US);

Lane B. Robbins, Pleasant Hill, OH (US);

Richard A. Poisson, Avon, CT (US);

Assignee:

GOODRICH CORPORATION, Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/44 (2006.01); B60T 7/04 (2006.01); B60T 8/17 (2006.01); B60T 13/68 (2006.01); B60T 17/22 (2006.01);
U.S. Cl.
CPC ...
B60T 8/1703 (2013.01); B60T 7/042 (2013.01); B60T 13/686 (2013.01); B60T 17/22 (2013.01); B64C 25/44 (2013.01); B60T 2220/04 (2013.01); B60T 2270/404 (2013.01); B60T 2270/413 (2013.01); B60T 2270/82 (2013.01);
Abstract

An aircraft braking system is disclosed that includes a first pedal, first and second pedal sensors for the first pedal, a first brake control unit (e.g., primary), and a separate second brake control unit (e.g., secondary). The first pedal position sensor is operatively interconnected with one of the first brake control unit and the second brake control unit, while the second pedal position sensor is operatively interconnected with the other of the first brake control unit and the second brake control unit. Outputs from these pedal sensors may be used to control operation of the aircraft braking system in at least some fashion.


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