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 11:
12. 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 vent port for exhausting an emission, the emission comprising at least one of a gas component, a vapor component, a liquid component, and a particulate component, wherein the emission is exhausted from the housing through the vent port during a failure of the battery;
a bracket comprising a first mounting arm and a second mounting arm attached to the self-powered avionics unit, wherein the bracket is configured to mount the self-powered avionics unit to a surface;
at least one emission shroud attached to one of the first mounting arm and the second mounting arm, wherein the at least one emission shroud is configured to capture at least one of the particulate component and the liquid component of the emission; and
at least one corrosive jet-resistant shield element mounted to the at least one emission shroud.