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:
Mar. 25, 2025

Filed:

May. 02, 2023
Applicant:

Honeywell International Inc., Charlotte, NC (US);

Inventors:

Ronald Vaughan, Tempe, AZ (US);

James N. Quitmeyer, Tempe, AZ (US);

Everett Canepa, Phoenix, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Charlotte, NC (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 31/14 (2006.01); B64C 11/00 (2006.01); B64D 27/30 (2024.01); B64D 31/08 (2006.01); B64D 35/08 (2006.01);
U.S. Cl.
CPC ...
B64D 31/08 (2013.01); B64C 11/002 (2013.01); B64D 27/30 (2024.01); B64D 31/14 (2013.01); B64D 35/08 (2013.01);
Abstract

A propulsor brake lock system includes an aircraft propulsor, a reduction gear assembly, a brake shaft, and a brake assembly. The aircraft propulsor includes a propeller having a propeller input shaft coupled thereto. The reduction gear assembly includes at least an input gear and an output gear. The input gear and output gear are both rotatable with the propeller input shaft. The brake shaft is coupled to, and is rotatable with, the output gear. The brake assembly is coupled to the brake shaft and is moveable between a disengaged position, in which the brake shaft may rotate whenever the output gear rotates, and an engaged position, in which the brake shaft is prevented from rotating, thereby preventing rotation of the output gear, the input gear, and the propeller input shaft.


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