Seat unit and lower structure thereof

    公开(公告)号:US11753168B2

    公开(公告)日:2023-09-12

    申请号:US16498528

    申请日:2017-12-18

    CPC classification number: B64D11/0627 B64D11/0605 B64D11/0606 B64D11/0696

    Abstract: 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.

    Passenger seat for aircraft
    2.
    发明授权

    公开(公告)号:US10093423B2

    公开(公告)日:2018-10-09

    申请号:US15506091

    申请日:2014-08-28

    Abstract: A passenger seat 100 for an aircraft, including a seat bottom frame 210, a backrest frame 220 and a headrest frame 230 that constitute a reclining assembly, which are supported by a spreader 170 and pipes 130 and 132 fastened to a floor by seat track fittings 110, the pipes 130 and 132 passing through left and right legs 120. A direct-acting-type damper 300 is attached to the backrest frame 230, and an extension member 400 is attached to the headrest frame 230, whereby a structural design is provided in which the reclining assembly, the direct-acting-type damper and the extension member can be easily replaced.

    Lock mechanism for aircraft passenger seat

    公开(公告)号:US10011360B2

    公开(公告)日:2018-07-03

    申请号:US15531815

    申请日:2014-12-22

    Abstract: In order to improve ease of maintenance of an aircraft passenger seat, the aircraft passenger seat 100 is adapted to be changeable between an upright position and a bed mode position at which the backrest is folded forward. A mechanism for locking the seat at each of the positions is provided with lock pins 350 provided on both sides of the backrest, a handle unit 200 mounted to a rear face of the backrest, and two wires 300 for connecting the handle unit 200 and the lock pins 350. A structure for connecting the wires 300 to the handle unit 200 is improved to facilitate the maintenance of the wires and to make the handle unit lightweight.

    SEAT UNIT AND ATTACHMENT METHOD THEREOF

    公开(公告)号:US20210129994A1

    公开(公告)日:2021-05-06

    申请号:US16500268

    申请日:2017-12-18

    Abstract: A seat unit for an aircraft that can be directly fixed at three points to a seat track provided on the floor of the aircraft. One representative seat unit and attachment method thereof relates to a seat unit comprising a lower structure of the seat unit and three fixtures configured to attach the lower structure directly to a pair of seat tracks of a mobile body, wherein the three fixtures include a lateral position adjustment member configured to laterally adjust a fitting position with the pair of seat tracks, a first fixture is fixed to one of the pair of seat tracks, a second fixture is fixed to one of the pair of seat tracks at a point separated from the first fixture, and a third fixture is fixed to another one of the pair of seat tracks at a corresponding portion between the first fixture and the second fixture.

    LOCK MECHANISM FOR AIRCRAFT PASSENGER SEAT

    公开(公告)号:US20170313427A1

    公开(公告)日:2017-11-02

    申请号:US15531815

    申请日:2014-12-22

    Abstract: In order to improve ease of maintenance of an aircraft passenger seat, the aircraft passenger seat 100 is adapted to be changeable between an upright position and a bed mode position at which the backrest is folded forward. A mechanism for locking the seat at each of the positions is provided with lock pins 350 provided on both sides of the backrest, a handle unit 200 mounted to a rear face of the backrest, and two wires 300 for connecting the handle unit 200 and the lock pins 350. A structure for connecting the wires 300 to the handle unit 200 is improved to facilitate the maintenance of the wires and to make the handle unit lightweight.

    AIRCRAFT PASSENGER SEAT
    6.
    发明申请

    公开(公告)号:US20170152046A1

    公开(公告)日:2017-06-01

    申请号:US15309587

    申请日:2014-11-14

    CPC classification number: B64D11/0619 B60N2/427 B64D11/06 B64D11/0696

    Abstract: An aircraft passenger seat (100) is fixed to a floor via a seat track fitting (110), and a reclining assembly of the seat is supported by pipes (130, 132) passed through left and right legs (120) and spreaders (170). A linear actuator (300) operates a reclining motion. A curved arm for deformation is provided to a mount (320) on which the actuator (300) is mounted, and a slit (145) is provided in a link plate (140) to which a rod is connected, and in a state where a forward force F is applied, the curved arm deforms and absorbs the impact. An impact absorbing structure is also provided to the legs (120).

    Seat unit and attachment method thereof

    公开(公告)号:US11319076B2

    公开(公告)日:2022-05-03

    申请号:US16500268

    申请日:2017-12-18

    Abstract: A seat unit for an aircraft that can be directly fixed at three points to a seat track provided on the floor of the aircraft. One representative seat unit and attachment method thereof relates to a seat unit comprising a lower structure of the seat unit and three fixtures configured to attach the lower structure directly to a pair of seat tracks of a mobile body, wherein the three fixtures include a lateral position adjustment member configured to laterally adjust a fitting position with the pair of seat tracks, a first fixture is fixed to one of the pair of seat tracks, a second fixture is fixed to one of the pair of seat tracks at a point separated from the first fixture, and a third fixture is fixed to another one of the pair of seat tracks at a corresponding portion between the first fixture and the second fixture.

    Bed mode mechanism for aircraft passenger seat

    公开(公告)号:US09849989B2

    公开(公告)日:2017-12-26

    申请号:US15123044

    申请日:2014-08-26

    CPC classification number: B64D11/0641 B60N2/3011 B60N2/3065

    Abstract: An aircraft passenger seat (100) has a seat bottom frame (150), and the seat bottom frame (150) is supported by an eccentric cam (210). A seat back frame (170) which rotates about a support point (250) is provided with a damper mechanism (300). When the seat back frame (170) is tilted forward from an upright position about the support point (250), a gas damper (310) is compressed and prevents rapid tilting. This energy assists force for returning the seat back to the upright position. The eccentric cam (210) rotates and lowers the seat bottom frame (150) so as to prevent cushions from being collapsed. A lock mechanism (400) highly rigidly retains the seat back frame at a bed mode position.

    BED MODE MECHANISM FOR AIRCRAFT PASSENGER SEAT

    公开(公告)号:US20170113802A1

    公开(公告)日:2017-04-27

    申请号:US15123044

    申请日:2014-08-26

    CPC classification number: B64D11/0641 B60N2/3011 B60N2/3065

    Abstract: An aircraft passenger seat (100) has a seat bottom frame (150), and the seat bottom frame (150) is supported by an eccentric cam (210). A seat back frame (170) which rotates about a support point (250) is provided with a damper mechanism (300). When the seat back frame (170) is tilted forward from an upright position about the support point (250), a gas damper (310) is compressed and prevents rapid tilting. This energy assists force for returning the seat back to the upright position. The eccentric cam (210) rotates and lowers the seat bottom frame (150) so as to prevent cushions from being collapsed. A lock mechanism (400) highly rigidly retains the seat back frame at a bed mode position.

    DIVIDER UNIT FOR AIRCRAFT PASSENGER SEAT
    10.
    发明申请
    DIVIDER UNIT FOR AIRCRAFT PASSENGER SEAT 有权
    飞机乘客座椅分机单元

    公开(公告)号:US20160368608A1

    公开(公告)日:2016-12-22

    申请号:US15102219

    申请日:2014-04-11

    CPC classification number: B64D11/0606

    Abstract: A divider unit (100) for a passenger seat has a slide rail (120) that is fixed onto a side shell (12) surrounding the seat. A plate-like divider (150) is equipped with two linear guides (170) inserted in the slide rail (120) and slides within the slide rail (120). A stopper (130) attached to a front end of the slide rail (120) has, a tapered surface (132), and the divider (150) is stopped when a front end of the divider (150) rides over the tapered surface (132), thereby preventing generation of collision noise.

    Abstract translation: 用于乘客座椅的分隔器单元(100)具有固定在围绕座椅的侧壳体(12)上的滑轨(120)。 板状分隔件(150)配备有插入在滑轨(120)中并在滑轨(120)内滑动的两个直线导轨(170)。 附接到滑轨(120)的前端的止动件(130)具有锥形表面(132),并且当分隔器(150)的前端越过锥形表面(...)时,分隔件(150)停止 132),从而防止产生碰撞噪声。

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