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    Aircraft window heating system
    42.
    发明授权
    Aircraft window heating system 有权
    飞机窗加热系统

    公开(公告)号：US09578686B2

    公开(公告)日：2017-02-21

    申请号：US14248782

    申请日：2014-04-09

    Applicant: The Boeing Company

    Inventor： Sahrudine Apdalhaliem ,  Kimberly D. Meredith ,  Morteza Safai

    IPC: B60L1/02 ,  H05B1/02 ,  B64C1/14 ,  H05B3/84

    CPC classification number: H05B1/0236 ,  B64C1/1484 ,  B64C1/1492 ,  H05B3/84

    Abstract: A method and apparatus for managing heating of a window system. The apparatus comprises a dimmable window panel and a heating system. The dimmable window panel has an inner portion and an outer portion around the inner portion. The heating system is thermally connected to the outer portion of the dimmable window panel.

    Abstract translation: 一种用于管理窗系统的加热的方法和装置。 该装置包括可调光窗板和加热系统。 可调光窗板具有围绕内部部分的内部部分和外部部分。 加热系统热连接到可调光窗板的外部。

    THERMAL BARRIER APPARATUS
    43.
    发明申请
    THERMAL BARRIER APPARATUS 有权
    热障碍装置

    公开(公告)号：US20160368587A1

    公开(公告)日：2016-12-22

    申请号：US14746127

    申请日：2015-06-22

    Applicant: The Boeing Company

    Inventor： Sahrudine Apdalhaliem ,  Waeil M. Ashmawi

    IPC: B64C1/14

    CPC classification number: B64C1/1484 ,  B64C1/1492

    Abstract: A thermal barrier apparatus for a window system includes a closed curve-shaped plate having a via in a central portion of the closed curve-shaped plate. The closed curve-shaped plate includes a plurality of concentric channels formed on a first surface of the closed curve-shaped plate; a plurality of walls, each of the plurality of walls defining adjacent concentric channels of the plurality of concentric channels, each of the plurality of walls including a plurality of openings between adjacent concentric channels; an outer wall formed on an outer peripheral edge of the closed curve-shaped plate, the outer wall including a plurality of openings; and an inner wall formed on an inner peripheral edge of the closed curve-shaped plate, the inner wall including a plurality of openings. Alternatively, a thermal barrier apparatus includes a frame; a closed curve-shaped plate provided in the frame having a first thermal barrier layer provided between the frame and a second surface of the closed curve-shaped plate; a closed curve-shaped pane provided at a portion of the first surface of the closed curve-shaped plate; and a seal provided between the pane and the first surface of the closed curve-shaped plate.

    Abstract translation: 一种用于窗户系统的隔热装置包括一封闭曲线形的板，该板在封闭曲线形板的中心部分具有通孔。 闭合曲线形板包括形成在封闭曲线形板的第一表面上的多个同心通道; 多个壁，所述多个壁中的每一个限定所述多个同心通道的相邻同心通道，所述多个壁中的每一个包括相邻的同心通道之间的多个开口; 形成在所述封闭曲线形板的外周边缘上的外壁，所述外壁包括多个开口; 以及形成在所述封闭曲线形板的内周边缘上的内壁，所述内壁包括多个开口。 或者，热障设备包括框架; 设置在所述框架中的闭合曲线形板具有设置在所述框架与所述封闭曲线形板的第二表面之间的第一热障层; 封闭的曲线形玻璃板，设置在封闭曲线形板的第一表面的一部分处; 以及设置在所述窗格与所述封闭曲线形板的所述第一表面之间的密封件。

    Local light attenuation for improving reliability of electronic dimmable windows
    44.
    发明授权
    Local light attenuation for improving reliability of electronic dimmable windows 有权
    局部光衰，用于提高电子可调光窗口的可靠性

    公开(公告)号：US09470828B1

    公开(公告)日：2016-10-18

    申请号：US14744795

    申请日：2015-06-19

    Applicant: The Boeing Company

    Inventor： Sahrudine Apdalhaliem ,  Waeil M. Ashmawi ,  Kimberly Dawn Meredith

    IPC: G02F1/03 ,  G02B5/23 ,  G02B5/20 ,  G02F1/01 ,  B64C1/14

    CPC classification number: G02B5/23 ,  B64C1/1484 ,  B64D2011/0061 ,  G02B5/208 ,  G02F1/0126 ,  G02F1/153 ,  G02F2202/14

    Abstract: A window system and method of attenuating light in a window system for improving usefulness and reliability of an electronic dimmable window in the window system. An automatically adjusting photochromatic material is integrated into a window pane of the window system such that the electronic dimmable window is positioned between the automatically adjusting photochromatic material in the window pane and a dust cover of the window system. The automatically adjusting photochromatic material is formulated to attenuate incoming light in a local area of the photochromatic material in response to a solar flux intensity of the incoming light in the local area being greater than or equal to a threshold intensity while areas outside the local area of the photochromatic material that are subjected to solar flux intensity less than the threshold intensity do not attenuate incoming light.

    Abstract translation: 一种在窗系统中衰减光的窗口系统和方法，用于提高窗系统中电子可调光窗的有用性和可靠性。 将自动调节的色素材料集成到窗系统的窗格中，使得电子可调光窗口位于窗玻璃中的自动调节的光色材料和窗系统的防尘罩之间。 配置自动调整的色素材料以响应于局部区域中的入射光的太阳能通量强度大于或等于阈值强度而衰减光色材料的局部区域中的入射光，而局部区域外的区域 经受太阳能通量强度小于阈值强度的光色材料不会衰减入射光。

    APPARATUS AND METHOD FOR A SHAPE MEMORY ALLOY MANDREL
    45.
    发明申请
    APPARATUS AND METHOD FOR A SHAPE MEMORY ALLOY MANDREL 有权
    形状记忆合金手册的装置和方法

    公开(公告)号：US20160023406A1

    公开(公告)日：2016-01-28

    申请号：US14340914

    申请日：2014-07-25

    Applicant: THE BOEING COMPANY

    Inventor： Moushumi Shome ,  Sahrudine Apdalhaliem ,  Frederick T. Calkins ,  Waeil M. Ashmawi ,  Kimberly Meredith

    IPC: B29C70/34 ,  B32B37/10 ,  B32B37/18 ,  B29C70/54 ,  B32B37/00

    CPC classification number: B32B37/1036 ,  B29C33/38 ,  B29C33/485 ,  B29C70/446 ,  B29C70/54 ,  B29K2905/00 ,  B29L2031/3076 ,  B32B37/0046 ,  B32B37/18 ,  B32B2605/18 ,  Y02T50/43

    Abstract: In one or more aspects of the present disclosure, a mandrel is disclosed. The mandrel having a shape memory alloy (SMA) shell having a longitudinal axis, an interior extending along the longitudinal axis and an exterior contour, the SMA shell being configured to interface with a structure to be cured, and at least one SMA actuation member disposed within the interior and connected to the SMA shell, where the at least one SMA actuation member is configured to exert pressure against the SMA shell effecting an interface pressure between the exterior contour of the SMA shell and the structure to be cured where the exterior contour has a predetermined actuated shape that corresponds to a predetermined cured shape of the structure to be cured.

    Abstract translation: 在本公开的一个或多个方面，公开了一种心轴。 心轴具有具有纵向轴线的形状记忆合金（SMA）壳体，沿着纵向轴线延伸的内部和外部轮廓，SMA壳体被配置为与要固化的结构相接触，并且至少一个SMA致动构件设置在 在内部并且连接到SMA壳体，其中至少一个SMA致动构件构造成对SMA壳施加压力，从而影响SMA外壳的外部轮廓与外部轮廓具有的待固化结构之间的界面压力 对应于要固化的结构的预定固化形状的预定的致动形状。

    THERMOPLASTIC COMPOSITE STRUCTURES EMBEDDED WITH AT LEAST ONE LOAD FITTING AND METHODS OF MANUFACTURING SAME
    46.
    发明申请
    THERMOPLASTIC COMPOSITE STRUCTURES EMBEDDED WITH AT LEAST ONE LOAD FITTING AND METHODS OF MANUFACTURING SAME 有权
    具有至少一个负载配件的热塑复合结构及其制造方法

    公开(公告)号：US20150321441A1

    公开(公告)日：2015-11-12

    申请号：US14465911

    申请日：2014-08-22

    Applicant: The Boeing Company

    Inventor： Jeffery Lee Marcoe ,  Marc Rollo Matsen ,  Waeil M. Ashmawi ,  Jaime C. Garcia ,  Sahrudine Apdalhaliem ,  John B. Moser ,  Brett I. Lyons ,  Moushumi Shome ,  Kay Y. Blohowiak

    IPC: B32B1/08 ,  B29C70/20 ,  B32B5/02 ,  B29C70/46

    CPC classification number: B32B1/08 ,  B29C33/52 ,  B29C70/205 ,  B29C70/462 ,  B29C2035/0811 ,  B32B5/024 ,  B32B2262/106 ,  B32B2605/08 ,  B32B2605/12 ,  B32B2605/18 ,  D04C1/06

    Abstract: Manufacturing a thermoplastic composite tubular structure embedded with a first load fitting comprising the steps of braiding a first plurality of inner layers of thermoplastic composite material around a soluble, expandable mandrel. A first load fitting is positioned on the first plurality of inner layers of thermoplastic composite material. A second plurality of outer layers of thermoplastic composite material is braided around the first load fitting and the mandrel so as to form an overbraided mandrel embedded with the first load fitting. The overbraided mandrel is installed into a matched tooling assembly and heated at a specified heating profile in order to consolidate the first plurality of inner layers of thermoplastic composite material and the second plurality of outer layers of thermoplastic composite material with the first load fitting so as to form a thermoplastic composite tubular structure embedded with the first load fitting. A second load fitting may be positioned on the first plurality of inner layers of thermoplastic composite material.

    Abstract translation: 制造嵌入有第一负载配件的热塑性复合管状结构，其包括在可溶性可扩张心轴周围编织第一组多个热塑性复合材料内层的步骤。 第一负载配件位于热塑性复合材料的第一多个内层上。 围绕第一负载配件和心轴编织第二多个热塑性复合材料外层，以便形成嵌入第一负载配件的外包芯。 将所覆盖的心轴安装到匹配的模具组件中并以特定的加热轮廓加热，以便将第一多个热塑性复合材料的内层和第二多个热塑性复合材料的外层与第一负载配件固结，以便 形成嵌入第一负载配件的热塑性复合管状结构。 第二负载配件可以被定位在热塑性复合材料的第一多个内层上。

    Variable camber airfoil system
    47.
    发明授权
    Variable camber airfoil system 有权
    可变外倾翼型系统

    公开(公告)号：US09145198B1

    公开(公告)日：2015-09-29

    申请号：US13734421

    申请日：2013-01-04

    Applicant: The Boeing Company

    Inventor： Moushumi Shome ,  Frederick T. Calkins ,  Sahrudine Apdalhaliem

    IPC: B64C3/48 ,  B64C3/14

    CPC classification number: B64C3/48 ,  B64C3/14 ,  B64C2003/142 ,  Y02T50/14

    Abstract: A system for varying a camber of an airfoil may include an airfoil having an upper surface and a lower surface meeting to form a leading edge and a trailing edge, the lower surface having a first actuator including shape memory alloy sheet, a controller including a plurality of heating elements attached to the shape memory alloy sheet for selectively heating the sheet to a temperature above ambient to deform the upper and lower surfaces to morph a geometry of a camber of the airfoil thereby, a computer control connected to selectively control individual activation of the heating elements to heat the shape memory alloy sheet to a selected temperature to effect a selected deflection, and a cooling device to allow ambient air to enter the wing and exit over the actuator to resume a non-morphed state.

    Abstract translation: 用于改变翼型的弯度的系统可以包括具有上表面和下表面的翼面，以形成前缘和后缘，所述下表面具有包括形状记忆合金薄片的第一致动器，包括多个 附接到形状记忆合金薄片的加热元件，用于选择性地将薄片加热到高于环境温度的温度，以使上表面和下表面变形，从而变形翼型件的曲面的几何形状，计算机控制器连接以选择性地控制 加热元件以将形状记忆合金薄片加热到所选择的温度以实现所选择的偏转;以及冷却装置，以允许环境空气进入机翼并离开致动器以恢复非变形状态。

    THREE-DIMENSIONAL TEXTILE PREFORMS AND COMPOSITE PARTS COMPRISING TEXTILE PREFORMS
    48.
    发明申请
    THREE-DIMENSIONAL TEXTILE PREFORMS AND COMPOSITE PARTS COMPRISING TEXTILE PREFORMS 有权

    公开(公告)号：US20220402590A1

    公开(公告)日：2022-12-22

    申请号：US17805795

    申请日：2022-06-07

    Applicant: The Boeing Company

    Inventor： Waeil M. Ashmawi ,  Zayd I. Abdel-Kamel ,  Sahrudine Apdalhaliem

    IPC: B64C3/18 ,  B29C70/68

    Abstract: Examples are disclosed herein that relate to vehicles, composite parts, and three-dimensional (3D) textile preforms for composite parts. In one example, a 3D textile preform for a composite part comprises a flange portion and a stiffener portion extending upwardly from the flange portion. The stiffener portion comprises a first wall portion that extends from the flange portion and a second wall portion that extends from the flange portion at a location spaced from the first wall portion. A connecting portion connects the first wall portion and the second wall portion at a location spaced from the flange portion.

    WINDOW CLAMP SYSTEM FOR A VEHICLE
    50.
    发明申请
    WINDOW CLAMP SYSTEM FOR A VEHICLE 有权

    公开(公告)号：US20210147058A1

    公开(公告)日：2021-05-20

    申请号：US16683848

    申请日：2019-11-14

    Applicant: The Boeing Company

    Inventor： Waeil M. Ashmawi ,  Sahrudine Apdalhaliem ,  Jaime C. Garcia

    IPC: B64C1/14

    Abstract: A window clamp system and method are to secure a window pane to a window frame of a vehicle. The window clamp system includes a mounting bracket configured to be secured to the window frame, one or more ratchets coupled to the mounting bracket, and a spring clip configured to move in relation to the mounting bracket and the one or more ratchets. The spring clip is configured to engage a seal positioned around the window pane.

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