Lining framework for an aircraft
View Patent ↗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.
1. An aircraft comprising a lining framework, the lining framework comprising:
at least three seat rails, including a lower seat rail and an upper seat rail, the lower and upper seat rails extending horizontally; and
at least two supports extending vertically and connecting the lower and upper seat rails to a fuselage cell of the aircraft, the supports being spaced apart horizontally; and
at least one seat connected to the lower and upper seat rails;
wherein at least two straps connect the upper seat rail to frames of the aircraft, the straps being configured to only transmit tensile forces in a vertical direction.
2. The aircraft according to claim 1 , wherein the straps are formed by a band-form fabric with a mechanically high-strength plastic material.
3. The aircraft according to claim 2 , wherein the straps are made of an ultra-high molecular weight polyethylene.