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    Slider seat for aircraft
    4.
    发明授权
    Slider seat for aircraft 有权
    飞机座椅

    公开(公告)号：US09359079B2

    公开(公告)日：2016-06-07

    申请号：US14558110

    申请日：2014-12-02

    Applicant: Molon Labe LLC

    Inventor： Frank Matthew Scott ,  Kevin Lee Van Liere

    IPC: B60N2/01 ,  B64D11/06

    CPC classification number: B64D11/0601 ,  B64D11/0639 ,  B64D11/0693

    Abstract: An aircraft seat set is provided that allows for providing extra room for passengers and/or allow for selectively increasing the width of an aircraft aisle during enplaning and deplaning and/or increasing the width of some seats during flight. In one embodiment, the aisle seat of the seat set is movably connected to the seat frame of the seat set to allow the aisle seat to be disposed above and in front of the middle seat of the seat set for enplaning and deplaning.

    Abstract translation: 提供了一种飞行器座椅组件，其允许为乘客提供额外的空间和/或允许在飞行过程中选择性地增加飞机通道的宽度，并且/或者在飞行期间增加一些座椅的宽度。 在一个实施例中，座椅组的过道座可移动地连接到座椅组的座椅框架，以允许过道座位置在座椅组的中间座椅的上方和前方，以便进行放行和取消。

    Aircraft seat assembly
    7.
    发明授权
    Aircraft seat assembly 失效
    飞机座椅总成

    公开(公告)号：US07578551B2

    公开(公告)日：2009-08-25

    申请号：US11642106

    申请日：2006-12-20

    Applicant: Luis Gonzalez Liñero

    Inventor： Luis Gonzalez Liñero

    IPC: A47C4/00 ,  A47C4/28 ,  A47C1/124 ,  A47C15/00 ,  A47C7/02

    CPC classification number: B64D11/0693 ,  A47C1/122

    Abstract: An aircraft seat assembly comprises a continuous row of a plurality of seats including a convertible aisle seat at one end of the row and one or more other seats. The seats are moveable between (i) a first configuration in which all of the seats are positioned in a useable position and a second configuration in which (a) the convertible seat is positioned in an unusable position in the row, (b) said one or more other seats are positioned in a useable position, and (c) the row of seats has a length, along the row, that is less than the length of the row in the first configuration for example by a distance of more than half the width of the convertible seat in the first configuration. The width of said one or more other seats may remain unchanged as between the first and second configurations.

    Abstract translation: 飞机座椅组件包括连续排的多个座椅，其包括在行的一端的可转换通道座和一个或多个其它座。 所述座椅可以在（i）所有座椅都位于可使用位置的第一构型和第二构型中移动，其中（a）可转换座椅位于行中不可用的位置，（b）所述座椅 或更多的其它座位被定位在可使用的位置，并且（c）所述排座具有沿所述行的长度小于所述第一构造中的所述行的长度，例如距离所述第一配置的一半以上的距离 可转换座椅的宽度在第一配置。 所述一个或多个其它座的宽度可以保持不变，如第一和第二构型之间。

    Aircraft seat assembly
    8.
    发明申请
    Aircraft seat assembly 失效
    飞机座椅总成

    公开(公告)号：US20070145789A1

    公开(公告)日：2007-06-28

    申请号：US11642106

    申请日：2006-12-20

    Applicant: Luis Linero

    Inventor： Luis Linero

    IPC: A47C13/00

    CPC classification number: B64D11/0693 ,  A47C1/122

    Abstract: An aircraft seat assembly comprises a continuous row of a plurality of seats including a convertible aisle seat at one end of the row and one or more other seats. The seats are moveable between (i) a first configuration in which all of the seats are positioned in a useable position and a second configuration in which (a) the convertible seat is positioned in an unusable position in the row, (b) said one or more other seats are positioned in a useable position, and (c) the row of seats has a length, along the row, that is less than the length of the row in the first configuration for example by a distance of more than half the width of the convertible seat in the first configuration. The width of said one or more other seats may remain unchanged as between the first and second configurations.

    Abstract translation: 飞机座椅组件包括连续排的多个座椅，其包括在行的一端的可转换通道座和一个或多个其它座。 所述座椅可以在（i）所有座椅都位于可使用位置的第一构型和第二构型中移动，其中（a）可转换座椅位于行中不可用的位置，（b）所述座椅 或更多的其它座位被定位在可使用的位置，并且（c）所述排座具有沿所述行的长度小于所述第一构造中的所述行的长度，例如距离所述第一配置的一半以上的距离 可转换座椅的宽度在第一配置。 所述一个或多个其它座的宽度可以保持不变，如第一和第二构型之间。

    Aircraft passenger seat row
    9.
    发明申请
    Aircraft passenger seat row 审中-公开
    飞机乘客座椅排

    公开(公告)号：US20050184566A1

    公开(公告)日：2005-08-25

    申请号：US11059314

    申请日：2005-02-17

    Applicant: Jurgen Baumann ,  Andreas Erb ,  Christian Pilgram

    Inventor： Jurgen Baumann ,  Andreas Erb ,  Christian Pilgram

    IPC: B64D11/06 ,  A47C15/00

    CPC classification number: B64D11/0638 ,  B64D11/06 ,  B64D11/064 ,  B64D11/0644 ,  B64D11/0693

    Abstract: 1. Aircraft passenger seat [row]. 2. The invention relates to an aircraft passenger seat row having a) at least three seats (10, 12, 14), b) a seat frame (16) common to all seats and having a front transverse spar (18) and a rear transverse spar (20) in parallel with the front spar which spars are rigidly connected by means of seat pedestals (22) so as to be stationary in relation to each other, c) cushion carriers (26) supporting seat element cushions (24), d) seat dividers (28) supported by both transverse spars (18, 20) and mounted at the ends of the row of seats and between the seats, e) backrests (30) the inclined position of which may be adjusted and which are pivotably connected to the seat dividers (28), and f) arm rests (32), preferably at both ends of the row of seats and between the seats (10, 12, 14), the last-named arm rests (32) being pivotably mounted on at least one guide web (34) extending in parallel with the transverse spars (18, 20) and supported by seat dividers (28) mounted between the seats (10, 12, 14), a center seat (12) of a row of seats having between adjacent seats (10, 14) a separating element (36) which, when in a non-use position, is mounted at least partly in the area of the associated seat pedestals (22) for this center seat (12) and, when in a use position, is mounted at least partly above the seat dividers (28), and it being possible to move the separating element (36) between the positions named by means of a pivot mechanism (38).

    Abstract translation: 飞机乘客座位[行]。 本发明涉及一种具有a）至少三个座（10,12,14）的飞机乘客座椅排，b）一个与所有座椅共用的座椅框架（16），并具有前横梁（18）和后 横梁（20）与前翼梁平行，翼梁通过座椅座（22）刚性连接，以相对于彼此固定; c）支撑座椅座垫（24）的缓冲支架（26） d）座椅分隔器（28），由两个横向翼梁（18,20）支撑并安装在座椅排的端部和座椅之间，e）靠背（30），其倾斜位置可被调整并且可枢转 连接到座椅分隔器（28），以及f）扶手（32），优选地在座椅排的两端和座椅（10,12,14）之间，最后命名的扶手（32）可枢转地 安装在与横向翼梁（18,20）平行延伸并由座椅分隔器（28）支撑的至少一个导向腹板（34）上 ）安装在所述座（10,12,14）之间，具有在相邻座（10,14）之间的一排座椅的中心座（12），分离元件（36），当处于不使用位置时， 至少部分地安装在用于该中心座（12）的相关联的座椅座（22）的区域中，并且当处于使用位置时，至少部分地安装在座椅分隔器（28）上方，并且可以移动 在通过枢转机构（38）命名的位置之间的分离元件（36）。

    Convertible seat systems for wide body aircraft
    10.
    发明授权
    Convertible seat systems for wide body aircraft 失效

    公开(公告)号：US5957407A

    公开(公告)日：1999-09-28

    申请号：US689804

    申请日：1996-08-14

    Applicant: Craig A. Auestad

    Inventor： Craig A. Auestad

    IPC: B64D11/06

    CPC classification number: B64D11/0693

    Abstract: Selected rows of seats for a wide body aircraft (i.e., having two or more passenger aisles) have seat groups that can expand or contract to change the number of seats in a row and the seat width. Conversion is possible with all seat components remaining attached to their respective frames, so that no detachable units have to be stowed. The convertible seat configurations are adaptable to incorporating individual amenities, including individual electronic displays.

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