Fastening apparatus and fastening arrangement for fastening a cabin interior component, aircraft cabin and aircraft

An aircraft or aircraft cabin comprising:

• an attachment structure having at least one fastening tube;
• a fastening apparatus for fastening a cabin interior component to the attachment structure, the fastening apparatus comprising:
• an inner sleeve fixed on the fastening tube such that that the inner sleeve cannot be moved relative to the fastening tube, the inner sleeve having an inner sleeve opening, into which the fastening tube is received;
• an outer sleeve fastened to the inner sleeve such that the outer sleeve is rotatable relative to the inner sleeve about a common axis;
• and
• a holding element, which is:
• fastened to the outer sleeve;
• and
• fixed on the cabin interior component such that the holding element cannot be moved relative to the cabin interior component;
• wherein the outer sleeve comprises:
• an outer sleeve opening, which receives and rotatably supports the inner sleeve therein;
• and
• an alignment region, which aligns the holding element relative to the outer sleeve and the fastening tube;
• and
• wherein the holding element engages with the alignment region of the outer sleeve to align the holding element relative to the fastening tube about the common axis.

An aircraft or aircraft cabin comprising:

• a fastening arrangement for fastening a cabin interior component to an attachment structure, the fastening arrangement comprising:
• the attachment structure, which has at least one fastening tube;
• the cabin interior component;
• and
• a fastening apparatus comprising:
• an inner sleeve fixed on the fastening tube such that the inner sleeve cannot be moved relative to the fastening tube, wherein the inner sleeve has an inner sleeve opening, into which the fastening tube is received such that the inner sleeve cannot be moved relative to the fastening tube;
• an outer sleeve fastened to the inner sleeve such that the outer sleeve is rotatable relative to the inner sleeve about a common axis;
• and
• a holding element, which is:
• fastened to the outer sleeve;
• and
• fixed on the cabin interior component such that the holding element cannot be moved relative to the cabin interior component;
• wherein the outer sleeve comprises:
• an outer sleeve opening, which receives and rotatably supports the inner sleeve therein;
• and
• an alignment region, which aligns the holding element relative to the outer sleeve and the fastening tube;
• wherein the holding element grips the alignment region over a full surface area, such that the holding element is aligned relative to the fastening tube in an axial direction of the fastening tube.