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:
Nov. 10, 2020

Filed:

Jun. 27, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Taylor R. Hubbard, Seattle, WA (US);

David T. Yamamoto, Mill Creek, WA (US);

Assignee:

THE BOEING COMPANY, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/42 (2006.01); F15B 13/02 (2006.01); F15B 13/04 (2006.01); F15B 13/042 (2006.01); B60T 13/12 (2006.01);
U.S. Cl.
CPC ...
B64C 25/42 (2013.01); F15B 13/028 (2013.01); F15B 13/0401 (2013.01); F15B 13/042 (2013.01); B60T 13/12 (2013.01); B60T 2270/40 (2013.01); F15B 2211/3052 (2013.01);
Abstract

A braking system for use with a dual landing gear aircraft. The braking system pairs outboard brake control into an outboard brake system control unit (BSCU) and inboard brake control into a second inboard brake system control unit (BSCU). Each BSCU is designed with two independent control lanes in which the forward wheel set is paired in one control lane and the aft wheels are paired onto the other. Alternate braking is provided via an alternate brake module installed in a fore-aft wheel pairing.


Find Patent Forward Citations

Hubbard, Taylor. (2020). Braking system for a dual landing gear aircraft (U.S. Patent No. 10829210). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10829210

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

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