| 摘要 |
The invention is based on an aircraft seat mounting device with at least one support profile (10a, 12a; 10b, 12b; 10c, 12c; 10d), with at least one aircraft seat element (14a, 16a, 18a, 42a; 14b, 16b, 18b, 42b; 14c, 16c, 18c, 42c) and with at least one intermediate element (20a, 22a, 24a, 26a, 28a, 30a, 32a, 34a; 36b, 38b, 40b, 96b; 36c,40c) which at least substantially surrounds the at least one support profile (10a, 12a; 10b, 12b; 10c, 12c; 10d) and is coupled to the at least one aircraft seat element (14a, 16a, 18a, 42a; 14b, 16b, 18b, 42b; 14c, 16c, 18c, 42c). It is proposed that the intermediate element (20a, 22a, 24a, 26a, 28a, 30a, 32a, 34a; 36b, 38b, 40b, 96b; 36c, 40c) is arranged rotatably with respect to the support profile (10a, 12a; 10b, 12b; 10c, 12c; 10d) at least in a crash situation/deformation situation. |
