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    Mid-wing multi-deck airplane
    2.
    发明授权
    Mid-wing multi-deck airplane 有权
    中翼多层飞机

    公开(公告)号：US08746616B2

    公开(公告)日：2014-06-10

    申请号：US13276357

    申请日：2011-10-19

    申请人： Sergey D. Barmichev ,  Mithra M. K. V. Sandrithi ,  Kevin M. Retz

    发明人： Sergey D. Barmichev ,  Mithra M. K. V. Sandrithi ,  Kevin M. Retz

    IPC分类号： B64C25/14 ,  B64C25/20

    CPC分类号： B64D11/06 ,  B64C1/10 ,  B64C1/26 ,  B64C2001/0027 ,  B64C2001/0045 ,  B64C2025/125 ,  Y02T50/12 ,  Y02T50/46

    摘要： An airplane comprises a twin-deck fuselage in which an upper deck support structure is utilized for carry-through of a mid-mount main wing box. The main landing gear of the airplane is mounted to the fuselage and is stowed in a non-pressurized area below the main wing box (enabled due to an optimized wing box geometry). A pressurized passageway/cargo/galley complex separates the main landing gear box and the main wing box. The upper deck is continuous, while the lower deck is separated by the wheel wells into two distinct fore and aft areas (for either cargo or passengers). The airplane further comprises an integrated vertical fin and an aft-extended pressurized deck area for reduced double-deck wetted area. More specifically, the double-deck pressurized fuselage structure is extended to form a blending structure to which a structural box of the vertical fin is attached.

    摘要翻译： 一架飞机包括一个双层机身，其中上甲板支撑结构用于中档安装的主翼箱的穿通。 飞机的主起落架安装在机身上，并存放在主机箱下方的非加压区域（由于优化的机翼箱几何形状而启用）。 加压通道/货物/厨房复合体分离主起落架和主翼箱。 上甲板是连续的，而下甲板由轮井分隔成两个不同的前后区域（货物或乘客）。 飞机还包括集成的垂直翼片和用于减小双层接液面积的后延伸的加压甲板区域。 更具体地，双层加压机身结构被延伸以形成连接垂直翅片的结构箱的混合结构。

    PILOT REST FOR AIRPLANE
    3.
    发明申请
    PILOT REST FOR AIRPLANE 有权
    飞机的飞行休息

    公开(公告)号：US20080149765A1

    公开(公告)日：2008-06-26

    申请号：US11614438

    申请日：2006-12-21

    申请人： Kevin M. Retz ,  Kelly L. Boren

    发明人： Kevin M. Retz ,  Kelly L. Boren

    IPC分类号： B64D11/06 ,  B64D11/04

    CPC分类号： B64D11/00 ,  B64D2011/0076

    摘要： A pilot rest system for use in a flight deck of an aircraft comprising a sleeping area, which comprises two parts, the first part being the space beneath one or more observer seats and the second part being a seat-free area adjacent to said seats. A curtain is preferably provided to enclose the second part of the sleeping area to ensure privacy and keep the sleep area dark if desired. The rest system can further comprise a mini-lavatory and a mini-galley in the flight deck.

    摘要翻译： 一种用于飞行器飞行甲板的飞行员休息系统，其包括睡眠区域，该睡眠区域包括两部分，第一部分是一个或多个观察者座位下的空间，而第二部分是与所述座位相邻的无座位区域。 优选地设置帘幕以封闭睡眠区域的第二部分，以确保隐私并且如果需要保持睡眠区域变暗。 休息系统还可以包括一个迷你洗手间和一个在飞行甲板上的小厨房。

    Lightweight aircraft passenger seat with composite construction
    5.
    发明授权
    Lightweight aircraft passenger seat with composite construction 有权
    轻型飞机乘客座椅与复合建筑

    公开(公告)号：US07954762B2

    公开(公告)日：2011-06-07

    申请号：US11383867

    申请日：2006-05-17

    申请人： Kelly L. Boren ,  Max U. Kismarton ,  Kevin M. Retz

    发明人： Kelly L. Boren ,  Max U. Kismarton ,  Kevin M. Retz

    IPC分类号： B64D11/06

    CPC分类号： B64D11/06 ,  B60N2/682 ,  B60N2/686 ,  B60N2/914 ,  B60N2/995 ,  B64D11/0649 ,  Y02T50/46

    摘要： An aircraft seat assembly configured in accordance with an example embodiment of the invention utilizes composite materials to achieve significant weight savings relative to conventional seat designs. The seat assembly includes a lightweight composite support structure, a lightweight composite seat base, and a seat back assembly that employs a lightweight inner frame. The seat cushion and the seat back cushion may utilize a sealed pneumatic element that self-inflates to provide increased air cushioning during flight. The seat assembly can leverage inexpensive manufacturing techniques such that the seat assembly can be economically produced for use as an economy class seat.

    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。 座椅组件包括轻质复合支撑结构，轻质复合座椅底座和采用轻质内框架的座椅靠背组件。 座垫和座椅靠垫可以利用密封的气动元件，其自动充气以在飞行期间提供增加的空气缓冲。 座椅组件可以利用廉价的制造技术，使得座椅组件可经济地生产用作经济舱座椅。

    Fastner-Free Primary Structural Joint for Sandwich Panels
    6.
    发明申请
    Fastner-Free Primary Structural Joint for Sandwich Panels 有权
    三明治板无夹紧主结构接头

    公开(公告)号：US20100006702A1

    公开(公告)日：2010-01-14

    申请号：US11747475

    申请日：2007-05-11

    申请人： John H. Fogarty ,  Kevin M. Retz

    发明人： John H. Fogarty ,  Kevin M. Retz

    IPC分类号： B64C1/00 ,  E04B1/00 ,  F16B13/00 ,  B29C65/52 ,  B23P11/00

    CPC分类号： B64C1/12 ,  B29C65/483 ,  B29C65/4835 ,  B29C65/485 ,  B29C65/505 ,  B29C66/43 ,  B29C66/547 ,  B29C66/723 ,  B29C66/72525 ,  F16B5/01 ,  F16B11/006 ,  Y10T29/49826

    摘要： Techniques for providing fastener-free primary structural joint for sandwich panels are disclosed. In one embodiment, a technique includes positioning a first panel having a first edge portion proximate a second panel having a second edge portion such that the first and second edge portions cooperatively form an interior recess on an interior side of the first and second panels, applying adhesive to at least one of the recessed interior side of the panel assembly and a plug configured to occupy the interior recess, inserting the plug into the interior recess, the plug including a cap that extends beyond the interior recess and overlaps adjacent portions of the first and second panels, applying adhesive to at least one of a splice and an exterior side opposite from the interior side, and attaching the splice on the exterior side.

    摘要翻译： 公开了用于提供用于夹芯板的无紧固件初级结构接头的技术。 在一个实施例中，一种技术包括定位具有靠近具有第二边缘部分的第二面板的第一边缘部分的第一面板，使得第一和第二边缘部分协同地形成在第一和第二面板的内侧上的内部凹部， 粘合剂到面板组件的凹陷内侧中的至少一个和被构造成占据内部凹部的插头，将插头插入内部凹部中，插头包括延伸超过内部凹部并与第一部分的相邻部分重叠的帽 和第二面板，将粘合剂施加到与内侧相对的接头和外侧中的至少一个，以及将接合件附接到外侧。

    Fastner-free primary structural joint for sandwich panels
    9.
    发明授权
    Fastner-free primary structural joint for sandwich panels 有权
    夹芯板的无夹紧主结构接头

    公开(公告)号：US08016230B2

    公开(公告)日：2011-09-13

    申请号：US11747475

    申请日：2007-05-11

    申请人： John H. Fogarty ,  Kevin M. Retz

    发明人： John H. Fogarty ,  Kevin M. Retz

    IPC分类号： B64C7/00

    CPC分类号： B64C1/12 ,  B29C65/483 ,  B29C65/4835 ,  B29C65/485 ,  B29C65/505 ,  B29C66/43 ,  B29C66/547 ,  B29C66/723 ,  B29C66/72525 ,  F16B5/01 ,  F16B11/006 ,  Y10T29/49826

    摘要： Techniques for providing fastener-free primary structural joint for sandwich panels are disclosed. In one embodiment, a technique includes positioning a first panel having a first edge portion proximate a second panel having a second edge portion such that the first and second edge portions cooperatively form an interior recess on an interior side of the first and second panels, applying adhesive to at least one of the recessed interior side of the panel assembly and a plug configured to occupy the interior recess, inserting the plug into the interior recess, the plug including a cap that extends beyond the interior recess and overlaps adjacent portions of the first and second panels, applying adhesive to at least one of a splice and an exterior side opposite from the interior side, and attaching the splice on the exterior side.

    摘要翻译： 公开了用于提供用于夹芯板的无紧固件初级结构接头的技术。 在一个实施例中，一种技术包括定位具有靠近具有第二边缘部分的第二面板的第一边缘部分的第一面板，使得第一和第二边缘部分协同地形成在第一和第二面板的内侧上的内部凹部， 粘合剂到面板组件的凹陷内侧中的至少一个和被构造成占据内部凹部的插头，将插头插入内部凹部中，插头包括延伸超过内部凹部并与第一部分的相邻部分重叠的帽 和第二面板，将粘合剂施加到与内侧相对的接头和外侧中的至少一个，以及将接合件附接到外侧。

    INTEGRATED AIRCRAFT FLOOR WITH LONGITUDINAL BEAMS
    10.
    发明申请
    INTEGRATED AIRCRAFT FLOOR WITH LONGITUDINAL BEAMS 有权
    一体化飞机地板与长期床

    公开(公告)号：US20100243803A1

    公开(公告)日：2010-09-30

    申请号：US12411615

    申请日：2009-03-26

    申请人： Willard N. Westre ,  Kevin M. Retz

    发明人： Willard N. Westre ,  Kevin M. Retz

    IPC分类号： B64C1/18

    CPC分类号： B64C1/18

    摘要： An integrated floor for an aircraft fuselage includes a composite panel forming a floor surface and composite beams bonded to the floor panel. The beams extend longitudinally within the fuselage and support the floor.

    摘要翻译： 用于飞行器机身的集成地板包括形成地板表面的复合板和结合到地板镶板的复合梁。 梁在机身内纵向延伸并支撑地板。