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    Method of absorbing energy in an aircraft passenger seat assembly
    4.
    发明授权
    Method of absorbing energy in an aircraft passenger seat assembly 有权
    在飞机乘客座椅组件中吸收能量的方法

    公开(公告)号：US08147001B2

    公开(公告)日：2012-04-03

    申请号：US12779479

    申请日：2010-05-13

    申请人： Kelly L. Boren ,  Rush F. Green ,  Max U. Kismarton

    发明人： Kelly L. Boren ,  Rush F. Green ,  Max U. Kismarton

    IPC分类号： A47C7/02 ,  B60N2/42

    CPC分类号： B64D11/0619 ,  B64D11/06 ,  B64D11/0647 ,  B64D11/0649 ,  Y02T50/46

    摘要： An aircraft seat assembly configured in accordance with an example embodiment of the invention offers a light weight and comfortable seat cushioning system that also provides energy-absorption and enhanced passenger maneuverability in extreme conditions such as may be experienced in a hard landing situation. The cushioning system includes a crushable, energy-absorbing layer, a main cushioning layer, a smaller ishial insert layer which may be the same as the main cushioning material and a semi-dynamic pneumatic cell which uses a dual action breather valve to vary its inflation with changes in cabin pressure. The seat cushion may be finished with a covering of cloth or upholstery.

    摘要翻译： 根据本发明的示例性实施例构造的飞行器座椅组件提供了重量轻且舒适的座椅缓冲系统，其还在极端条件下提供能量吸收和增强的乘客机动性，例如在硬着陆情况下可能经历的。 缓冲系统包括可压碎的能量吸收层，主缓冲层，可与主缓冲材料相同的较小间隙插入层和使用双作用通气阀来改变其膨胀的半动态气动元件 随着客舱压力的变化。 座垫可以用布或室内装潢的覆盖物完成。

    Composite seat back structure for a lightweight aircraft seat assembly
    5.
    发明授权
    Composite seat back structure for a lightweight aircraft seat assembly 有权
    用于轻型飞机座椅组件的复合座椅靠背结构

    公开(公告)号：US08016361B2

    公开(公告)日：2011-09-13

    申请号：US12752381

    申请日：2010-04-01

    申请人： Max U. Kismarton ,  Sergey Barmichev

    发明人： Max U. Kismarton ,  Sergey Barmichev

    IPC分类号： B60N2/68

    CPC分类号： B64D11/0649 ,  B64D11/06 ,  B64D11/064 ,  Y02T50/46

    摘要： An aircraft passenger seat configured in accordance with an embodiment of the invention utilizes composite materials to achieve significant weight savings relative to conventional seat designs. The seat includes one or more lightweight composite support legs, a lightweight composite seat pan, and a lightweight composite seat back structure. The support legs are coupled to the seat pan, which is in turn coupled to the seat back structure. The support legs utilize composite frame elements that are formed as continuous compression molded composite extrusions. The seat pan includes composite fore and aft cross beams that are also formed as continuous compression molded composite extrusions. The aft cross beam includes a rear flange that serves as a flexible “hinge” for the seat back structure. The seat can leverage producible and relatively inexpensive composite manufacturing techniques such that the seat can be economically produced for use as an economy class seat.

    摘要翻译： 根据本发明的实施例配置的飞机乘客座椅利用复合材料相对于传统座椅设计实现显着的重量节省。 座椅包括一个或多个轻质复合支撑腿，轻型复合座盘和轻型复合座椅靠背结构。 支撑腿联接到座椅盘，座椅底板又联接到座椅靠背结构。 支撑腿利用形成为连续压塑复合材料挤压件的复合框架元件。 座盘包括还形成为连续压塑复合材料挤压件的复合的前横梁和后横梁。 后横梁包括用于座椅靠背结构的柔性“铰链”的后凸缘。 座椅可以利用可生产且相对便宜的复合制造技术，使得座椅可以经济地生产用作经济舱座椅。

    Airplane floor assembly
    6.
    发明授权
    Airplane floor assembly 有权
    飞机地板总成

    公开(公告)号：US07938362B2

    公开(公告)日：2011-05-10

    申请号：US11358503

    申请日：2006-02-21

    申请人： Max U. Kismarton ,  Willard N. Westre ,  Stuart M. Buchan

    发明人： Max U. Kismarton ,  Willard N. Westre ,  Stuart M. Buchan

    IPC分类号： B64C1/00 ,  B64C30/00

    CPC分类号： B64C1/18 ,  B64F5/10

    摘要： The invention relates to airplane floor assemblies and to methods for their assembly. In one embodiment, an airplane comprises at least one fuselage section and at least one floor section. At least one system component is installed to the floor section prior to installation of the floor section in the fuselage of the airplane. In another embodiment, a floor section adapted to be installed in an airplane includes at least one system component installed to the floor section while it is outside of the airplane. In yet another embodiment, a method is disclosed for assembling an airplane. The method comprises installing at least one system component to a floor section, and installing the floor section into a fuselage section of the airplane.

    摘要翻译： 本发明涉及飞机地板组件及其组装方法。 在一个实施例中，飞机包括至少一个机身部分和至少一个地板部分。 在将地板部分安装在飞机的机身之前，至少有一个系统部件安装到地板部分。 在另一个实施例中，适于安装在飞机中的地板部分包括在飞机外部安装到地板部分的至少一个系统部件。 在另一个实施例中，公开了一种组装飞机的方法。 该方法包括将至少一个系统部件安装到地板部分，以及将地板部分安装到飞机的机身部分中。

    Composite seat pan structure for a lightweight aircraft seat assembly
    8.
    发明授权
    Composite seat pan structure for a lightweight aircraft seat assembly 有权
    用于轻型飞机座椅组件的复合座盘结构

    公开(公告)号：US07716797B2

    公开(公告)日：2010-05-18

    申请号：US11614979

    申请日：2006-12-22

    申请人： Max U. Kismarton ,  James A. Fullerton

    发明人： Max U. Kismarton ,  James A. Fullerton

    IPC分类号： B68G7/00 ,  B64D11/06

    CPC分类号： B64D11/0649 ,  B64D11/06 ,  Y02T50/46 ,  Y10T29/481 ,  Y10T29/49622

    摘要： An aircraft passenger seat configured in accordance with an embodiment of the invention utilizes composite materials to achieve significant weight savings relative to conventional seat designs. The seat includes one or more lightweight composite support legs, a lightweight composite seat pan, and a lightweight composite seat back structure. The support legs are coupled to the seat pan, which is in turn coupled to the seat back structure. The support legs utilize composite frame elements that are formed as continuous compression molded composite extrusions. The seat pan includes composite fore and aft cross beams that are also formed as continuous compression molded composite extrusions. The aft cross beam includes a rear flange that serves as a flexible “hinge” for the seat back structure. The seat can leverage producible and relatively inexpensive composite manufacturing techniques such that the seat can be economically produced for use as an economy class seat.

    摘要翻译： 根据本发明的实施例配置的飞机乘客座椅利用复合材料相对于传统座椅设计实现显着的重量节省。 座椅包括一个或多个轻质复合支撑腿，轻型复合座盘和轻型复合座椅靠背结构。 支撑腿联接到座椅盘，座椅底板又联接到座椅靠背结构。 支撑腿利用形成为连续压塑复合材料挤压件的复合框架元件。 座盘包括还形成为连续压塑复合材料挤压件的复合的前横梁和后横梁。 后横梁包括用于座椅靠背结构的柔性“铰链”的后凸缘。 座椅可以利用可生产且相对便宜的复合制造技术，使得座椅可以经济地生产用作经济舱座椅。

    COMPOSITE LEG STRUCTURE FOR A LIGHTWEIGHT AIRCRAFT SEAT ASSEMBLY
    9.
    发明申请
    COMPOSITE LEG STRUCTURE FOR A LIGHTWEIGHT AIRCRAFT SEAT ASSEMBLY 有权
    轻型飞机座椅组件的复合结构

    公开(公告)号：US20090084925A1

    公开(公告)日：2009-04-02

    申请号：US12200790

    申请日：2008-08-28

    申请人： Max U. Kismarton

    发明人： Max U. Kismarton

    IPC分类号： A47B97/00 ,  B23P17/00

    CPC分类号： B64D11/0696 ,  A47C5/00 ,  B60N2/68 ,  B64D11/06 ,  B64D11/0619 ,  B64D11/0649 ,  Y02T50/46 ,  Y10T29/49616

    摘要： A lightweight leg assembly for an aircraft seat assembly includes a leg frame comprising at least one leg attachment bracket and a main frame member carried by the at least one leg attachment bracket and comprising a thermoplastic material. At least one track fitting may be carried by the leg frame. A method of fabricating a leg assembly for an aircraft seat assembly is also disclosed.

    摘要翻译： 一种用于飞机座椅组件的轻型腿部组件，包括腿架，该腿架包括至少一个腿部附接支架和由所述至少一个腿部附接支架承载并且包括热塑性材料的主框架构件。 至少一个轨道配件可以由腿架承载。 还公开了一种制造用于飞机座椅组件的腿部组件的方法。

    AIRCRAFT FLOOR AND METHOD OF ASSEMBLY
    10.
    发明申请
    AIRCRAFT FLOOR AND METHOD OF ASSEMBLY 有权
    飞机地板和装配方法

    公开(公告)号：US20080210820A1

    公开(公告)日：2008-09-04

    申请号：US12056456

    申请日：2008-03-27

    申请人： Max U. Kismarton ,  Willard N. Westre ,  Stuart M. Buchan

    发明人： Max U. Kismarton ,  Willard N. Westre ,  Stuart M. Buchan

    IPC分类号： B64C1/18

    CPC分类号： B64C1/18 ,  B64F5/10

    摘要： The invention relates to aircraft floor assemblies and to methods for their assembly. In one embodiment, an aircraft comprises at least one fuselage section and at least one floor section. At least one system component is installed to the floor section prior to installation of the floor section in the fuselage of the aircraft. In another embodiment, a floor section adapted to be installed in an aircraft includes at least one system component installed to the floor section while it is outside of the aircraft. In yet another embodiment, a method is disclosed for assembling an aircraft. The method comprises installing at least one system component to a floor section, and installing the floor section into a fuselage section of the aircraft.

    摘要翻译： 本发明涉及飞机地板组件及其组装方法。 在一个实施例中，飞行器包括至少一个机身部分和至少一个底板部分。 在将地板部分安装在飞机的机身之前，至少有一个系统部件安装到地板部分。 在另一个实施例中，适于安装在飞行器中的底板部分包括在飞机外部安装到地板部分的至少一个系统部件。 在另一个实施例中，公开了一种组装飞行器的方法。 该方法包括将至少一个系统部件安装到地板部分，以及将地板部分安装到飞行器的机身部分中。