Structure and equipment system for installation in an aircraft

A structure and equipment system for installation in an aircraft, comprising:

• a plurality of vertical supports,
• a rail device,
• at least one connector,
• a plurality of guiding elements,
• a plurality of pivot joints, and
• a plurality of locking devices,
• wherein the rail device is configured to be attached to a structure of the aircraft and is configured to guide the guiding elements along an axis of extension of the rail device and, in so doing, move them relative to the structure,
• wherein by means of the at least one connector, the vertical supports are arranged parallel to and at a distance from one another and are connected to form a grid arrangement,
• wherein the guiding elements are arranged on the grid arrangement,
• wherein the pivot joints are configured to be attached to upper ends of the vertical supports and are configured to pivot the vertical supports about the upper ends thereof,
• wherein the locking devices each have a first locking element which is arranged at a lower end of a vertical support and is configured to be locked in a second locking element which can be positioned on the structure, and
• wherein the grid arrangement are configured to be inserted into the structure of the aircraft into an installation position with the guiding elements on the rail device with vertical supports pivoted upwards from the vertical, by pivoting down into a vertical orientation, the first locking elements are configured to interlock with correspondingly arranged second locking elements so that a load-bearing support structure can be formed thereby.