| 摘要 |
PROBLEM TO BE SOLVED: To provide a connecting structure of an aircraft interior panel that is configured to reduce weight and also to reduce cost.SOLUTION: Two pieces of aircraft interior panels 12, 14 include a corner 24 extending along the extending direction of those edges by the attachment between a distal edge of the inside surface sheet 20 and a distal edge of the outside surface sheet 22 on an inside surface sheet 20. In the corner 24, a plurality of belt-shaped connecting pieces 26 configured by a portion of the inside surface sheet 20 projected from the corner 24 are projected in the extending direction of the corner 24 at intervals over a full length of the corner 24. The corners 24 of the two pieces of aircraft interior panels 12, 14 are brought into abutment with each other, and the connecting pieces 26 of the two pieces of the aircraft interior panels 12, 14 pass through a gap between the connecting pieces 26 of the aircraft interior panels 14, 12 of a connected partner, and are bonded to the outside surface sheet 22 of the aircraft interior panels 14, 12 of the partner by adhesives B, and thereby the two pieces of aircraft interior panels 12, 14 are connected. |
