Aircraft installation arrangement and installation system for mounting an overhead luggage compartment

An installation arrangement suitable for fastening a portion of an overhead luggage compartment in an aircraft, the installation arrangement comprising:

• a first carrier element configured to fasten the overhead luggage compartment thereto, the first carrier element including:
• a main body comprising a tubular opening,
• a first barrel-shaped component arranged inside the tubular opening of the main body, the first barrel-shaped component comprising a first through hole extending substantially perpendicular to a longitudinal axis of the first barrel-shaped component, and
• fastening means for fastening a portion of the overhead luggage compartment to the main body of the first carrier element;
• and
• a second carrier element being a rotary joint connectable to an installation rail, the rotary joint being movable around a longitudinal axis of the installation rail and an axis perpendicular to the longitudinal axis of the installation rail;
• and
• a rod configured to be coupled with the second carrier element and to fit inside the first through hole,
• wherein the rod is connectable to the first carrier element, when the rod is arranged inside the first through hole.