Loudspeaker system for aircraft cabin
View Patent ↗A loudspeaker system for an aircraft cabin for passengers has a support structure, which includes multiple flexible flat elements, forming the internal walls of the cabin, and fastening devices for fastening flat elements to the support structure, so that the flat elements may oscillate. At least one acoustic driver is connected to one or more flat elements, to induce a bending movement in the one or more flat elements. The particular flat element may oscillate as an acoustic diaphragm. The acoustic driver has a film-shaped piezoelectric exciter, which is bonded flatly to the flat element. The flat element bonded to an exciter has a first cover layer, a second cover layer, and a core layer between them. The core layer is subdivided in a plane parallel to the first and second cover layers by a horizontal incision in at least one predefined area.
1. A loudspeaker system for an aircraft cabin for passengers, having a support structure, which comprises:
multiple flexible flat elements, which together form the internal walls of the cabin,
fastening devices for fastening at least some of the flat elements to the support structure, so that the flat elements may oscillate per se,
at least one acoustic driver which is connected to one or more flat elements, to induce a bending movement in the one or more flat elements, so that the particular flat element may oscillate as an acoustic diaphragm,
the at least one acoustic driver comprising a film-shaped piezoelectric exciter, which is bonded flatly to the flat element,
wherein
the flat element bonded to an exciter comprises a first cover layer, a second cover layer, and a core layer between them, and the core layer is subdivided in a plane parallel to the first and second cover layers by a horizontal incision in at least one predefined area,
wherein the exciter is laminated into the flat element and a further covering layer is located on its rear side.
2. The loudspeaker system according to claim 1 , wherein multiple exciters are bonded to a flat element, which each preferably have different geometrical dimensions.
3. The loudspeaker system according to claim 2 , wherein each exciter on the flat element is assigned to one of multiple core layer areas situated adjacent to one another, the multiple core layer areas being separated from one another.
4. The loudspeaker system according to claim 3 , wherein constrictions of the flat elements are provided for more efficient decoupling of the acoustically active areas from one another.
5. The loudspeaker system according to claim 1 , wherein the acoustically active flat elements are an integral component of a service duct.
6. The loudspeaker system according to claim 1 , wherein the flat elements bonded to acoustic drivers are fastened to the support structure using vibration-insulating retainers.
7. The loudspeaker system according to claim 1 , wherein sound absorber elements are provided between the flat elements bonded to acoustic drivers and the flat elements neighboring them.
8. The loudspeaker system according to claim 1 , wherein the exciter on the flat element is offset laterally to the horizontal incision in the core layer.