SEAT UNIT STRUCTURE, SEAT UNIT, AND ATTACHMENT METHOD THEREOF

    公开(公告)号:US20210114735A1

    公开(公告)日:2021-04-22

    申请号:US16500255

    申请日:2017-12-18

    Abstract: An object of the present invention is to provide a seat unit structure, a seat unit, and an attachment method thereof in which component reinstallation does not arise when the seat unit is attached in an aircraft. One representative seat unit structure according to the present invention relates to a seat unit structure configured to support a seat, wherein the structure has a lower structure having a monocoque structure and defines an outermost shell in at least one direction of the seat unit. That is, the member mounted in the one direction of the seat unit can be stored inside the outermost shell of the structure. In addition, the one direction is the width direction of the airframe.

    SEAT UNIT AND LOWER STRUCTURE THEREOF

    公开(公告)号:US20210107657A1

    公开(公告)日:2021-04-15

    申请号:US16498528

    申请日:2017-12-18

    Abstract: An object of the present invention is to provide a seat unit and a lower structure thereof that are not restricted in their positional relationship with seat tracks provided in advance in the airframe. One representative seat unit of the present invention and the lower structure thereof includes a hollow structure integrally formed using a composite member. The hollow structure is hollow in a front direction of the seat unit. The hollow structure has a quadrilateral shape in the front direction of the seat unit. In addition, a partition plate is disposed in the hollow structure. Furthermore, the lower structure includes attachment points to an aircraft at three locations on its bottom. In addition, a block is embedded in the composite member at the attachment point, and a thickness of the composite member around a bracket coupled to the block is less than thickness at other locations.

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