US 11,953,953 B2
Behind the radome mounting system for aircraft avionics equipment
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); and Charles O. Adler, Mukilteo, WA (US)
Assigned to THE BOEING COMPANY, Arlington, VA (US)
Filed by The Boeing Company, Chicago, IL (US)
Filed on Sep. 27, 2018, as Appl. No. 16/144,165.
Prior Publication US 2020/0102080 A1, Apr. 2, 2020
Int. Cl. 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)
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)] 35 Claims
OG exemplary drawing
 
1. An avionics unit assembly for an aircraft, comprising:
an avionics unit;
a battery configured to power the avionics unit;
a housing that encases the battery and the avionics unit, wherein:
the housing comprises a vent port configured to exhaust an emission from the avionics unit during a failure of the avionics unit; and
the emission comprises one or more of a gas component, a vapor component, a liquid component, and a particulate component;
a shield element;
a emission shroud defining a receptacle; and
a bracket, wherein the avionics unit, the emission shroud, and the shield element are mounted to the bracket.