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:
Apr. 09, 2024

Filed:

Sep. 27, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Ramon L. Cuenca, Buena Park, CA (US);

Shellini P. Dowell, Bellevue, WA (US);

Thomas A. Jessett, Bellevue, WA (US);

Fadl I. Khalil, Edmonds, WA (US);

Warren S. Ng, Irvine, CA (US);

Scott B. Vacknitz, Kirkland, WA (US);

Collis M. Walker, Stanton, CA (US);

Archibald A. Gray, Seattle, WA (US);

James C. Russell, Bellevue, WA (US);

Charles O. Adler, Mukilteo, WA (US);

Assignee:

THE BOEING COMPANY, Arlington, VA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
G06F 1/18 (2006.01); B64D 45/00 (2006.01); G01S 5/18 (2006.01); G01S 7/02 (2006.01); G01S 13/95 (2006.01); H01M 10/052 (2010.01); H01M 50/202 (2021.01); H01M 50/244 (2021.01); H01M 50/262 (2021.01); H01M 50/375 (2021.01);
U.S. Cl.
CPC ...
G06F 1/182 (2013.01); B64D 45/00 (2013.01); G01S 5/183 (2013.01); G01S 13/953 (2013.01); G06F 1/188 (2013.01); H01M 50/202 (2021.01); H01M 50/244 (2021.01); H01M 50/262 (2021.01); H01M 50/375 (2021.01); B64D 2045/0065 (2013.01); G01S 7/027 (2021.05); H01M 10/052 (2013.01); H01M 2220/20 (2013.01);
Abstract

An avionics unit assembly for an aircraft can include an avionics unit (e.g., an underwater locator device, 'ULD'), and a battery to power the avionics unit. The avionics unit assembly can further include a housing that encases the avionics unit and the battery. The housing includes a vent port for exhausting an emission from the housing during a failure of the avionics unit. The avionics unit assembly can further include one or more of a suppressor that filters the emission, a shield element that is resistant to chemical and/or thermal effects of the emission, and a bracket for mounting the avionics unit to a surface. A method integrating the avionics unit assembly onto a forward aircraft bulkhead at a mount location under an aircraft radome and for manufacturing the avionics unit, and an aircraft including the avionics unit are also described.


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