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 14:
15. An avionics unit assembly for an aircraft, comprising:
a self-powered avionics unit comprising a battery as an internal power source, a housing comprising a body and at least one detachable end cap configured to provide a vent port for exhausting an emission during failure of the avionics unit, wherein the emission comprises at least one of a gas component, a vapor component, a liquid component, and a particulate component;
a bracket comprising a first arm and at least a second arm attached to the housing;
a first emission shroud mounted to the first arm and a second emission shroud mounted to the second arm; and
a first corrosive jet-resistant shield element mounted to the first emission shroud and a second corrosive jet-resistant shield element mounted to the second emission shroud.