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    Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures
    2.
    发明授权
    Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures 有权
    用于将复合构件和其他结构构件连接在飞机机翼箱和其他结构中的装置和方法

    公开(公告)号：US07575194B2

    公开(公告)日：2009-08-18

    申请号：US11607333

    申请日：2006-11-30

    申请人： Stephen T. Brown ,  Max U. Kismarton

    发明人： Stephen T. Brown ,  Max U. Kismarton

    IPC分类号： B64C3/18 ,  B64C1/06

    CPC分类号： B64C1/26

    摘要： Apparatuses and methods for joining composite members and other structural members in aircraft wings and other structures. An aircraft wing box structure configured in accordance with one embodiment of the invention includes a first composite member having a first surface portion positioned at an angel relative to a second surface portion of a second composite member. The wing box structure of this embodiment further includes at least one metallic joining member having an upstanding leg portion extending from a base portion. The base portion of the joining member is bonded to the first surface portion of the first composite member with a first portion of adhesive, and the upstanding leg portion of the metallic joining member is bonded to the second surface portion of the second composite member with a second portion of adhesive.

    摘要翻译： 用于在飞机机翼和其他结构中连接复合构件和其他结构构件的装置和方法。 根据本发明的一个实施例构造的飞行器翼盒结构包括第一复合构件，其具有相对于第二复合构件的第二表面部分成一角度定位的第一表面部分。 本实施例的翼盒结构还包括至少一个金属接合构件，其具有从基部延伸的直立的腿部。 接合构件的基部用第一粘合剂部分粘合到第一复合构件的第一表面部分，并且金属接合构件的直立腿部分与第二复合构件的第二表面部分接合 粘合剂的第二部分。

    Reinforced elastomer attachment joint
    4.
    发明授权
    Reinforced elastomer attachment joint 失效
    增强弹性体附件接头

    公开(公告)号：US4507011A

    公开(公告)日：1985-03-26

    申请号：US374268

    申请日：1982-05-03

    申请人： Stephen T. Brown

    发明人： Stephen T. Brown

    IPC分类号： B29C65/00 ,  B29C65/56 ,  B29C70/88 ,  B31F7/00 ,  B64C1/12 ,  F16B5/00

    CPC分类号： B29C66/43 ,  B29C65/562 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C70/887 ,  B31F7/006 ,  B64C1/12 ,  B29K2083/00 ,  Y02T50/433 ,  Y10T403/45 ,  Y10T403/7123 ,  Y10T403/74 ,  Y10T403/75 ,  Y10T428/24256

    摘要： A reinforced elastomer attachment joint includes an elastomer section (304) butt bonded to a FIBERGLAS section (332), a boundary line (340) being defined therebetween. One or more fabric plies (338) are embedded within the elastomer (304) and FIBERGLAS (332) sections so as to be capable of transmitting loads from the elastomer section (304) to the FIBERGLAS section (332). The rigid FIBERGLAS section (332) is capable of being drilled and countersunk so as to accomodate fastening means (306) whereby the attachment joint can be secured to basic support structure (302).

    摘要翻译： 加强弹性体附接接头包括与FIBERGLAS部分（332）接合的弹性体部分（304），边界线（340）被限定在其间。 一个或多个织物层（338）嵌入在弹性体（304）和FIBERGLAS（332）部分内，以便能够将载荷从弹性体部分（304）传递到FIBERGLAS部分（332）。 刚性FIBERGLAS部分（332）能够被钻孔和埋头以便容纳紧固装置（306），由此附接接头可固定到基本支撑结构（302）上。

    Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
    5.
    发明授权
    Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods 有权
    飞机后缘装置，包括具有非平行运动路径的装置，以及相关方法

    公开(公告)号：US07744040B2

    公开(公告)日：2010-06-29

    申请号：US12264831

    申请日：2008-11-04

    申请人： Douglas S. Lacy ,  Kevin W. Beyer ,  Stephen T. Brown ,  Paul W. Dees ,  Neal V. Huynh ,  Jan A. Kordel ,  Clayton A. Prow ,  Seiya Sakurai

    发明人： Douglas S. Lacy ,  Kevin W. Beyer ,  Stephen T. Brown ,  Paul W. Dees ,  Neal V. Huynh ,  Jan A. Kordel ,  Clayton A. Prow ,  Seiya Sakurai

    IPC分类号： B64C3/50

    CPC分类号： B64C9/16 ,  B64C2009/143

    摘要： Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods are disclosed. A device in accordance with one embodiment includes a wing and an inboard trailing edge device coupled to the wing and movable relative to the wing between a first stowed position and a first deployed position along a first motion path. An outboard trailing edge device can be coupled to the wing outboard of the inboard trailing edge device, and can be movable relative to the wing along a second motion path that is non-parallel to the first motion path. An intermediate trailing edge device can be coupled between the inboard and outboard trailing edge devices and can be movable along a third motion path that is non-parallel to both the first and second motion paths. Each of the trailing edge devices can open a gap relative to the wing when moved to their respective deployed positions.

    摘要翻译： 公开了包括具有非平行运动路径的装置和相关方法的飞行器后缘装置。 根据一个实施例的装置包括机翼和内侧后缘装置，其联接到机翼并且可沿着第一运动路径在第一收起位置和第一展开位置之间相对于机翼移动。 外侧后缘装置可以联接到内侧后缘装置的翼外侧，并且可以沿着不平行于第一运动路径的第二运动路径相对于机翼移动。 中间后缘装置可以联接在内侧和后侧后缘装置之间，并且可以沿着不平行于第一和第二运动路径的第三运动路径移动。 每个后缘装置可以在移动到它们各自的展开位置时相对于机翼打开间隙。

    Flexible shape low volume autoclave
    10.
    发明授权
    Flexible shape low volume autoclave 有权
    柔性形状低容量高压釜

    公开(公告)号：US08876999B2

    公开(公告)日：2014-11-04

    申请号：US11761744

    申请日：2007-06-12

    申请人： Sergey D. Barmichev ,  Max U. Kismarton ,  Stephen T. Brown

    发明人： Sergey D. Barmichev ,  Max U. Kismarton ,  Stephen T. Brown

    IPC分类号： B32B37/10 ,  B29C70/44 ,  B29C35/02 ,  B29L31/30

    CPC分类号： B29C70/44 ,  B29C35/0227 ,  B29L2031/3076 ,  B29L2031/3085 ,  Y02T50/43

    摘要： Techniques and apparatus for providing a flexible shape low volume autoclave are disclosed. In one embodiment, an autoclave includes an elongated pressure vessel that is sealed on both ends and has a circumferential joint between a first portion and a second portion. The autoclave further includes the portions defining an interior configured for accepting an elongated part, the joint being configured to create an angle between the portions and further creating an opening with a seal, the opening facilitating an insertion of the part into the interior, and the seal enabling pressurization of the interior.

    摘要翻译： 公开了用于提供柔性形状的低容量高压釜的技术和设备。 在一个实施例中，高压釜包括细长的压力容器，其在两端被密封并且在第一部分和第二部分之间具有圆周接头。 高压釜还包括限定内部的部分，所述内部构造成用于接收细长部分，所述接头构造成在所述部分之间产生角度并进一步产生具有密封件的开口，所述开口有助于将部件插入内部， 密封能够使内部加压。