Patent ID: 11953953
Assignee: THE BOEING COMPANY
Field: Electrical machinery, apparatus, energy (Electrical engineering)
Classification: CPC G  B  H  Y | IPC B  G  H

Claim 17:
18. An aircraft, comprising:
a forward bulkhead;
a radome mounted to the forward bulkhead, wherein a volume between the forward bulkhead and the radome is external to an aircraft pressure vessel; and
an avionics unit assembly mounted to the forward bulkhead and positioned directly between the radome and the forward bulkhead in a direction perpendicular to a major plane of the forward bulkhead, the avionics unit assembly comprising:
an avionics unit;
a battery configured to power the avionics unit;
a housing that encases the avionics unit and the battery, 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;
an emission shroud defining a receptacle; and
a bracket, wherein the avionics unit, the emission shroud, and the shield element are mounted to the bracket.