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:
Dec. 30, 2014

Filed:

Mar. 26, 2010
Applicants:

Casey Hanlon, Queen Creek, AZ (US);

Kellan Geck, Chandler, AZ (US);

James Neil Quitmeyer, Chandler, AZ (US);

Allan Blunt, Granger, IN (US);

Inventors:

Casey Hanlon, Queen Creek, AZ (US);

Kellan Geck, Chandler, AZ (US);

James Neil Quitmeyer, Chandler, AZ (US);

Allan Blunt, Granger, IN (US);

Assignee:

Honeywell International Inc., Morristown, NJ (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60L 7/00 (2006.01); B60T 7/04 (2006.01); B60T 7/08 (2006.01); B60T 13/74 (2006.01); F16D 65/18 (2006.01); F16D 65/28 (2006.01); F16D 65/00 (2006.01); F16D 121/24 (2012.01); F16D 125/40 (2012.01); F16D 125/48 (2012.01); F16D 127/06 (2012.01);
U.S. Cl.
CPC ...
B60T 7/042 (2013.01); F16D 2121/24 (2013.01); F16D 2125/40 (2013.01); F16D 2125/48 (2013.01); F16D 2127/06 (2013.01); B60T 7/085 (2013.01); B60T 13/741 (2013.01); F16D 65/18 (2013.01); F16D 65/28 (2013.01); F16D 65/0043 (2013.01);
Abstract

An aircraft brake system electromechanical actuator is provided. The actuator is configured with features that allow the electric motor to be a line replaceable unit. One such feature is a foreign-object-damage shield that inhibits dust, debris, and/or other particulate contaminants from entering the electromechanical actuator during electric motor removal and replacement.


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