Patent attributes
Disclosed is a lining framework for fastening seats in an aircraft. The lining framework preferably comprises three seat rails, which are arranged in a spaced apart manner parallel to each other along both side walls of the fuselage cell. Sitting surfaces of a plurality of seats are suspended on the seat rails by textile straps consisting of high-strength, woven plastic material. At least two straps are arranged between the upper seat rail and two frames of the fuselage cell of the aircraft. In this case, a strap length is measured so that forces from the fuselage cell cannot be transmitted into the lining framework. By the same token, however, forces from the lining framework can be introduced into the fuselage cell by means of the straps so that the lining framework can be designed statically lighter. This leads to a weight reduction of the lining framework.
