A galley insert system for an aircraft galley comprises a galley support structure, a galley insert configured to be coupled to the support structure, and a latch mechanism for coupling the insert to the support structure, the latch mechanism configured to automatically engage to couple the insert to the support structure when the insert is moved into a latching position on the support structure, wherein the latch mechanism comprises a control mechanism configured to be actuated to disengage the latch mechanism.
GALLEY INSERT SYSTEM
2024-01-04
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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