FASTENING SYSTEM FOR FASTENING A CABIN FITTING ELEMENT TO A SUPPORT STRUCTURE OF AN AIRCRAFT

摘要

The invention relates to a fastening system for fastening a cabin fitting element (1) with at least one electrical installation on a support structure (2) of an aircraft. During installation into the support structure (2), the cabin fitting element (1) is fixed in succession by at least one loose bearing (13) in at least one degree of translational freedom and then by at least one fixed bearing (3) in the at least one further degree of translational freedom. In order to ensure an improved installation and dismantling of cabin covering panels with electrical installation and to reduce the weight due to the components and also the installation space which is required, according to the invention a contact device with a bush arrangement (17, 21) and a plug arrangement (18, 23) is integrated in the at least one loose bearing (13) and/or the at least one fixed bearing (3), by which an electrical connection is produced between the support structure (2) and the electrical installation of the cabin fitting element (2) on fixing at least of one degree of translational freedom.