A system may include an aircraft galley insert configured to be installed within an aircraft galley insert bay, a mounting plate attached to a rear of the aircraft galley insert, and a power connector assembly attached to the mounting plate. The power connector assembly may include compressible spring assemblies that compress as the power connector assembly is mated with a corresponding power connector assembly of the aircraft galley insert bay. The power connector assembly may self-align with the corresponding power connector assembly of the aircraft galley insert bay when the aircraft galley insert is installed within the aircraft galley insert bay.
Galley Insert Power Connector Assembly with Spring Assemblies
16.09.2021
Patent
Elektronische Ressource
Englisch
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