Aircraft seat device
An aircraft seat device with at least one support beam, which is configured to realize at least part of a mounting unit of an aircraft seat. In at least one partial region, viewed in a circumferential direction of the support beam, the at least one support beam has a changing wall thickness.
1. An aircraft seat device with at least one support beam, which is configured to realize at least part of a mounting unit of an aircraft seat, wherein
the at least one support beam is hollow and is configured by a single wall that encompasses an interior space,
in at least one partial region, viewed in a cross-sectional plane of the support beam, the wall has a changing wall thickness in a circumferential direction of the support beam and an at least substantially circular outer contour, and
a basic shape of an inner contour of the support beam differs at least in partial regions from a basic shape of the outer contour.
2. The aircraft seat device according to claim 1 , wherein the support beam is a one-piece element.
3. The aircraft seat device according to claim 1 , wherein the support beam has a changing wall thickness along its longitudinal extension.
4. The aircraft seat device according to claim 1 , wherein the support beam has at least one symmetry axis.
5. The aircraft seat device according to claim 1 , wherein the support beam is at least partially implemented of a rolled metal sheet.
6. An aircraft seat with an aircraft seat device according to claim 1 .
7. The aircraft seat device according to claim 1 , wherein the basic shape of the inner contour is elliptical.
8. The aircraft seat device according to claim 1 , wherein the inner contour includes a plurality of elevations, which extend radially inward.
9. The aircraft seat device according to claim 1 , wherein the basic shape of the outer contour is a circle and the basic shape of the inner contour is non-circular.