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:
Jul. 19, 2022

Filed:

Oct. 10, 2019
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Nima Forghani, Seattle, WA (US);

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

Levi A. Mulkey, Edmonds, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 25/48 (2006.01); B60T 8/17 (2006.01); B60T 8/32 (2006.01); B64C 25/42 (2006.01); B64C 25/46 (2006.01);
U.S. Cl.
CPC ...
B64C 25/48 (2013.01); B60T 8/1703 (2013.01); B60T 8/325 (2013.01); B64C 25/426 (2013.01); B64C 25/46 (2013.01);
Abstract

There is provided a pivot turn load alleviation (PTLA) brake system for alleviating structural loads on a pivoting main landing gear of an aircraft in a pivot turn maneuver. The PTLA brake system includes a brake control system operatively coupled to at least two main landing gear, each having two or more wheels. The PTLA brake system further includes a PTLA brake inhibit subsystem coupled to the brake control system. The subsystem inhibits braking of one or more of the two or more wheels of the pivoting main landing gear, in the pivot turn maneuver, so that at least one wheel of the two or more wheels is in an unbraked state, and a remaining number of the two or more wheels are in a braked state. The PTLA brake system alleviates structural loads, and reduces wear on the at least one wheel that is in the unbraked state.


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