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    • 3. 发明申请
    • TABLE ARRANGEMENT
    • 表格安排
    • US20150284091A1
    • 2015-10-08
    • US14679117
    • 2015-04-06
    • Zodiac Seats UK Limited
    • Robert GowPaul Morgan
    • B64D11/06A47B3/00A47B3/14
    • B64D11/0638A47B3/002A47B3/14B60N3/001B60N3/002B60N3/004
    • The present invention provides a table arrangement comprising a table moveably mounted to a table mounting structure, a compensation arrangement connected between the table and table mounting structure for reducing the force required to lift the table from a lowered position to a raised position, and a damper arrangement for reducing the speed of the table as it moves from the raised position to the lowered position, wherein the compensation arrangement is mounted on a shaft, such that as the table is lowered, the shaft rotates about its longitudinal axis and wherein the damping arrangement is arranged to act on the shaft to reduce the speed of its rotation about its longitudinal axis. The invention also provides an aircraft seat module and a method of deploying or stowing a table arrangement.
    • 本发明提供了一种桌子布置,其包括可移动地安装到工作台安装结构的工作台,连接在工作台和工作台安装结构之间的补偿装置,用于减小将工作台从降低位置提升到升高位置所需的力,以及阻尼器 用于当桌子从升高位置移动到降低位置时降低工作台的速度,其中补偿装置安装在轴上,使得当桌子下降时,轴围绕其纵向轴线旋转,并且其中阻尼装置 被布置成作用在轴上以减小其围绕其纵向轴线的旋转速度。 本发明还提供了一种飞机座椅模块和一种展现或收起桌子布置的方法。
    • 4. 发明申请
    • HIGH DENSITY AIRCRAFT SEAT ARRANGEMENT
    • 高密度飞机座椅安装
    • US20150001341A1
    • 2015-01-01
    • US14376617
    • 2013-03-15
    • Zodiac Seats UK Limited
    • Ali ErsanRichard NicholasJohn McKeever
    • B64D11/06
    • B64D11/06B64D11/0601B64D11/0606B64D11/0641
    • An aircraft cabin (26) has a plurality of seat units (10) including first (10) and second (12) seat units in a first row (22) and a third seat unit (14) in a second row (24). The first and second seat units (10, 12) are separated by an aisle (38). The seats all face in the same direction (31), said direction (31) being inclined to the longitudinal axis (30) by a seat offset angle (Sθ), and are configurable between a bed mode and a seat mode. A console (20a) of the first seat unit (10) is directly adjacent to the aisle (38) and accommodates a foot-well (40) for use by a passenger in the seat (18c) of the third seat unit (14). At least a part of the console (20a) of the first seat unit (10), in a region no higher than a first distance from the floor, extends further into the aisle (38) than the rest of the first seat unit (10) in a region higher than the first distance from the floor.
    • 飞机机舱(26)具有多个座单元(10),其包括位于第一排(22)中的第一座椅单元(10)和第二座椅单元(12)和第二排(24)中的第三座椅单元(14)。 第一和第二座椅单元(10,12)由通道(38)分开。 所述座椅全部朝向相同的方向(31),所述方向(31)以纵向轴线(30)倾斜座椅偏移角(S& L),并且可在床模式和座椅模式之间配置。 第一座椅单元(10)的控制台(20a)直接邻近通道(38)并容纳由第三座椅单元(14)的座椅(18c)中的乘客使用的脚部(40) 。 第一座椅单元(10)的控制台(20a)的不超过地板第一距离的区域的至少一部分比第一座椅单元(10)的其余部分进一步延伸到通道(38) )在高于距离地面的第一距离的区域中。
    • 5. 发明申请
    • TOOL FOR CURING A COMPOSITE COMPONENT
    • 固化组合物的工具
    • US20160236454A1
    • 2016-08-18
    • US15040505
    • 2016-02-10
    • Zodiac Seats UK Limited
    • Nicholas PottsBhaskar Biswas
    • B32B37/10B32B38/18B32B27/08B32B37/00
    • The present invention provides a tool 1 for curing a composite component, the tool comprising a lay-up surface 8 for laying-up layers of an uncured composite component, a cover assembly 9 for moving in relation to the lay-up surface to cover a layed-up uncured composite component on the lay-up surface, the cover assembly comprising a sealable cover for sealing around the uncured composite component on the lay-up surface to form a sealed zone, and a vacuum port 25 for providing a vacuum to the sealed zone, wherein the tool further comprises at least one heating element 15, 53 within the sealed zone for heating the uncured composite component. The invention also provides a method of manufacturing a composite component and a composite component. The composite component may form at least part of a piece of aircraft furniture, such as an aircraft seat shell.
    • 本发明提供了一种用于固化复合部件的工具1,该工具包括用于铺设未固化复合部件层的铺层表面8,用于相对于铺层表面移动的盖组件9以覆盖 在叠置表面上铺设未固化的复合材料部件,盖组件包括用于密封围绕铺设表面上的未固化的复合材料部件以形成密封区域的可密封的盖,以及用于向真空端口25提供真空的真空端口25 密封区,其中所述工具还包括在所述密封区域内的至少一个加热元件15,53,用于加热未固化的复合部件。 本发明还提供了一种制造复合部件和复合部件的方法。 复合部件可以形成飞机家具的至少一部分,例如飞机座椅壳。
    • 6. 发明申请
    • TABLE ARRANGEMENT
    • 表格安排
    • US20150284088A1
    • 2015-10-08
    • US14679095
    • 2015-04-06
    • Zodiac Seats UK Limited
    • Robert GowPaul Morgan
    • B64D11/06A47B5/04A47B13/08A47B5/00
    • B64D11/0605A47B5/006A47B5/04A47B13/081B64D11/0638
    • The present invention provides a table arrangement 100 for use in an aircraft seat module, the table arrangement comprising a first table element suitable for being movably mounted to a mounting structure of the aircraft seat module, the first table element being provided with a first table surface, a second table element provided with a second table surface substantially parallel to the first table surface, wherein the second table element is mounted to the first table element, such that the second table element is moveable from a first position with respect to the first table element to a second position with respect to the first table element, the second position being transformed from the first position within the plane of the second table element. The present invention also provides an aircraft seat module, an aircraft and a method of deploying a table arrangement.
    • 本发明提供了一种用于飞行器座椅模块的工作台装置100,该工作台装置包括适于可移动地安装到飞行器座椅模块的安装结构的第一工作台部件,第一工作台部件设置有第一工作台面 ,第二台元件,其具有基本上平行于所述第一台面的第二工作台表面,其中所述第二工作台元件安装到所述第一工作台元件,使得所述第二工作台元件可相对于所述第一工作台从第一位置移动 元件相对于第一台元件到第二位置,第二位置从第二台元件的平面内的第一位置变换。 本发明还提供了一种飞机座椅模块,飞行器和一种部署桌子布置的方法。
    • 10. 发明授权
    • High density aircraft seat arrangement
    • 高密度飞机座椅安排
    • US09550573B2
    • 2017-01-24
    • US14376617
    • 2013-03-15
    • Zodiac Seats UK Limited
    • Ali ErsanRichard NicholasJohn McKeever
    • B64D11/06
    • B64D11/06B64D11/0601B64D11/0606B64D11/0641
    • An aircraft cabin (26) has a plurality of seat units (10) including first (10) and second (12) seat units in a first row (22) and a third seat unit (14) in a second row (24). The first and second seat units (10, 12) are separated by an aisle (38). The seats all face in the same direction (31), said direction (31) being inclined to the longitudinal axis (30) by a seat offset angle (Sθ), and are configurable between a bed mode and a seat mode. A console (20a) of the first seat unit (10) is directly adjacent to the aisle (38) and accommodates a foot-well (40) for use by a passenger in the seat (18c) of the third seat unit (14). At least a part of the console (20a) of the first seat unit (10), in a region no higher than a first distance from the floor, extends further into the aisle (38) than the rest of the first seat unit (10) in a region higher than the first distance from the floor.
    • 飞机机舱(26)具有多个座单元(10),其包括位于第一排(22)中的第一座椅单元(10)和第二座椅单元(12)和第二排(24)中的第三座椅单元(14)。 第一和第二座椅单元(10,12)由通道(38)分开。 所述座椅全部朝向相同的方向(31),所述方向(31)以纵向轴线(30)倾斜座椅偏移角(Sθ),并且可配置在床模式和座椅模式之间。 第一座椅单元(10)的控制台(20a)直接邻近通道(38)并容纳由第三座椅单元(14)的座椅(18c)中的乘客使用的脚部(40) 。 第一座椅单元(10)的控制台(20a)的不超过地板第一距离的区域的至少一部分比第一座椅单元(10)的其余部分进一步延伸到通道(38) )在高于距离地面的第一距离的区域中。