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    • 3. 发明申请
    • AIRCRAFT SEAT ARRANGEMENT INCLUDING TABLE
    • 飞机座椅安排包括表
    • US20140145477A1
    • 2014-05-29
    • US14002122
    • 2012-03-30
    • Ali ErsanDaniel Clucas
    • Ali ErsanDaniel Clucas
    • B64D11/06
    • B64D11/06B64D11/00151B64D11/0601B64D11/0606B64D11/0638B64D11/064B64D11/0641
    • An aircraft seat arrangement comprises first and second seats (10, 20) and first and second consoles (12, 22), the first console (12) being in front of the first seat (10) and adjacent to the second seat (20), such that the first and second consoles (12, 22) and the first and second seats (10, 20) are in a staggered arrangement. A table (50) is housed by the first console (12). The table (50) is arranged for movement to a stowed position, in which the table is inserted within said first console (12). The table (50) is arranged for, optionally horizontal, movement to a deployed position, in which the table is positioned aft of the first console (12) so as to be suitable for use by a passenger seated in the first seat (10). The table may be arranged to present different areas of useable table surface.
    • 飞行器座椅装置包括第一和第二座椅(10,20)以及第一和第二控制台(12,22),第一控制台(12)在第一座椅(10)的前面并与第二座椅(20)相邻, ,使得第一和第二控制台(12,22)以及第一和第二座椅(10,20)处于交错排列。 桌子(50)由第一控制台(12)容纳。 工作台(50)被布置成运动到收起位置,其中桌子被插入到所述第一控制台(12)内。 桌子(50)布置成可选地水平地移动到展开位置,其中桌子位于第一控制台(12)的后面,以便适合坐在第一座椅(10)中的乘客使用, 。 桌子可以被布置成呈现可用的桌面的不同区域。
    • 6. 发明授权
    • Table arrangement
    • 表排列
    • US09481464B2
    • 2016-11-01
    • US14679136
    • 2015-04-06
    • Zodiac Seats UK Limited
    • Robert GowPaul Morgan
    • A47B83/02B64D11/06
    • B64D11/0605B64D11/0638
    • The present invention provides table arrangement comprising a housing that has an open configuration and a closed configuration, a table, which, when in a stowed configuration is at least partially housed in the housing, and when in a presented configuration, is partially protruding from the housing, and an activation mechanism for opening and closing the housing, which is linked by a mechanical linkage to the table or housing such that when the activation mechanism closes the housing, the table changes from the presented configuration to the stowed configuration. The invention also provides an aircraft seat module, an aircraft and a method of stowing a table arrangement.
    • 本发明提供了包括具有打开构造和封闭构造的壳体的桌子布置,桌子,当处于收起的构造中至少部分地容纳在壳体中时,并且当呈现配置时,该桌子部分地从 壳体和用于打开和关闭壳体的致动机构,其通过机械联动件与桌子或壳体相连接,使得当启动机构关闭壳体时,工作台从呈现的构型变化到收起构型。 本发明还提供一种飞机座椅模块,飞行器以及收起台面布置的方法。
    • 8. 发明授权
    • Aircraft seat
    • 飞机座椅
    • US08882034B2
    • 2014-11-11
    • US12747997
    • 2008-12-10
    • John McKeever
    • John McKeever
    • B64D11/06
    • B64D11/0601B64D11/06B64D11/0606B64D11/0641B64D11/0643B64D11/0647
    • The seats are swivellable about axes (1) and arranged with their axes in column axes (2). The seats each have a direction (4) extending from the middle of the seat back through the middle of the seat cushion (22), intersecting the seat's swivel axis. Extending equally on either side of the seat direction is defined a seat projection (5) forwards of the seat cushion and having the same width as the seat cushion. The swivel is set up to allow the seat to be turned through 6 from 17.5 to the longitudinal axis of the column (and the aircraft to be equipped with the seats) to 23.5. At 17.5, as in column IV, the seats partially face the seats in front in the column. This is the maximum angle at which the regulatory authorities will allow a lap belt only to be worn by a passenger for TTL. When the seats are swivelled outwards to 23.5, they face the space (6) along side the seat in front and can be converted to bed mode.
    • 座椅可围绕轴线(1)旋转,并将其轴线布置在列轴线(2)中。 座椅各自具有从座椅靠背的中部延伸穿过座垫(22)的中间的方向(4),与座椅的旋转轴线相交。 在座椅方向的任一侧均等地延伸,座椅突出部(5)被定位在座垫的前方并具有与座垫相同的宽度。 旋转架被设置成允许座椅从17.5转到6的纵坐标轴(并且配备座椅的飞机)到23.5。 在第17.5节,如第四栏所示,座位部分地朝向立柱前面的座椅。 这是监管机构允许搭乘腰带仅由乘客穿戴TTL的最大角度。 当座椅向外转动到23.5时,它们面向前面座椅侧面的空间(6),可以转换为床模式。
    • 9. 发明授权
    • Aircraft seat
    • 飞机座椅
    • US08419123B2
    • 2013-04-16
    • US12594592
    • 2008-04-02
    • Christopher HankinsonBenedict Nicholas Samuels
    • Christopher HankinsonBenedict Nicholas Samuels
    • B60N2/32B60N2/00B60N2/02B64N13/00
    • B64D11/0604B64D11/06B64D11/0605B64D11/064B64D11/0641
    • An aircraft seat has a chassis (21), fixed to a pallet which is fixed to the floor of the aircraft. The chassis has two load bearing sides (23) and opposite ends (24, 25). Fixed along the top edge of the sides (23) and facing outwards are pins (26) supporting bearing wheels (27). These on each side engage with a rectangular S form interconnection beam (28) having an inside groove (29) for receiving these wheels. On the outside, the beam has another groove (30) receiving similar wheels (31), on pins (32) fixed to the inside of side plates (41) of a sub-frame (42), these side plates being interconnected by front and rear beams (43, 44). Thus the sub-frame can move back and forth, with the wheels acting as rolling element bearings. The beams move half the distance of the sub-frame, in analogous manner to the bearing of filing cabinet drawers.
    • 飞机座椅具有固定在飞机地板上的托盘上的底盘(21)。 底盘具有两个承载侧(23)和相对端(24,25)。 沿着侧面(23)的顶部边缘固定并面向外是支撑轴承轮(27)的销(26)。 它们在每一侧上与一个具有用于容纳这些轮子的内侧槽(29)的矩形S形互连梁(28)接合。 在外部,梁具有在固定到副框架(42)的侧板(41)的内侧的销(32)上接收相似的轮(31)的另一个槽(30),这些侧板通过前部 和后梁(43,44)。 因此,子框架可以前后移动,车轮用作滚动元件轴承。 梁以与档案柜抽屉的方位相似的方式移动子框架的一半距离。