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    • 2. 发明公开
    • FLUGZEUGSITZAUFSTÄNDERVORRICHTUNG
    • EP3083401A1
    • 2016-10-26
    • EP14814838.0
    • 2014-12-16
    • Recaro Aircraft Seating GmbH & Co. KG
    • RODERWALD, MartinDRENZECK, Thomas
    • B64D11/06
    • 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.
    • 本发明基于具有至少一个支撑型材(10a,12a; 10b,12b; 10c,12c; 10d)的飞机座椅安装装置,其具有至少一个飞机座椅元件(14a,16a,18a,42a; 14b, 至少一个中间元件(20a,22a,24a,26a,28a,30a,32a,34a; 36b,38b,40b,96b; 36c,40c) 其至少基本上围绕所述至少一个支撑轮廓(10a,12a; 10b,12b; 10c,12c; 10d)并且联接到所述至少一个飞机座椅元件(14a,16a,18a,42a; 14b,16b, 18b,42b; 14c,16c,18c,42c)。 建议中间元件(20a,22a,24a,26a,28a,30a,32a,34a; 36b,38b,40b,96b; 36c,40c)相对于支撑型材(10a,12a; 10b,12b; 10c,12c; 10d)至少在碰撞情况/变形情况下。