Energy absorber for aircraft seat

    公开(公告)号:US12031603B2

    公开(公告)日:2024-07-09

    申请号:US16760837

    申请日:2018-10-18

    Applicant: Safran Seats

    Inventor: Julien Dhermand

    Abstract: The invention relates mainly to an energy absorber for an aircraft seat, notably for a helicopter seat, comprising at least one energy-absorption element having:



    a first anchor point and a second anchor point,
    an energy-absorption zone extending between the first anchor point and the second anchor point, said energy-absorption zone being able to stretch as a tensile load is applied between the first anchor point and the second anchor point,
    characterized in that the energy-absorption zone has a meshed structure comprising a plurality of strands connected to one another by junction portions, and in that at least one junction portion provides a junction between at least three strands of said energy-absorption zone.

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