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21.发明授权公开(公告)号：US09718248B2
公开(公告)日：2017-08-01
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
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.
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公开(公告)号：US09457494B2
公开(公告)日：2016-10-04
申请号：US14481851
申请日：2014-09-09
Applicant: The Boeing Company
Inventor： Moushumi Shome , Janet Mary Layng , Waeil M. Ashmawi , Sahrudine Apdalhaliem
CPC classification number: B29C35/0805 , B29C35/02 , B29C70/44 , B29C2035/0855 , B29L2031/3055 , B29L2031/3067 , B29L2031/3076
Abstract: Method and apparatus for curing a composite laminate. The apparatus comprising an electromagnetic radiation source creating electromagnetic microwave energy in an enclosed volume and a heating source for providing a convective airflow in the enclosed volume. A composite laminate assembly comprising a composite laminate is placed in the enclosed volume, wherein the composite laminate of the composite laminate assembly is cured by both the electromagnetic microwave energy created by the electromagnetic radiation source, and the convective airflow provided by the heating source. A vacuum bag may be placed over the composite laminate assembly. A source may be activated such that a vacuum within the vacuum bag is created according to design specifications.
Abstract translation: 固化复合层压板的方法和装置。 该装置包括在封闭容积中产生电磁微波能量的电磁辐射源和用于在封闭容积中提供对流气流的加热源。 包括复合层压材料的复合层压组件放置在封闭的体积中，其中复合层压组件的复合叠层体由电磁辐射源产生的电磁微波能量和由加热源提供的对流气流两者固化。 真空袋可以放置在复合层压组件上。 源可以被激活，使得根据设计规范创建真空袋内的真空。
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公开(公告)号：US20160067888A1
公开(公告)日：2016-03-10
申请号：US14481851
申请日：2014-09-09
Applicant: The Boeing Company
Inventor： Moushumi Shome , Janet Mary Layng , Waeil M. Ashmawi , Sahrudine Apdalhaliem
CPC classification number: B29C35/0805 , B29C35/02 , B29C70/44 , B29C2035/0855 , B29L2031/3055 , B29L2031/3067 , B29L2031/3076
Abstract: Method and apparatus for curing a composite laminate. The apparatus comprising an electromagnetic radiation source creating electromagnetic microwave energy in an enclosed volume and a heating source for providing a convective airflow in the enclosed volume. A composite laminate assembly comprising a composite laminate is placed in the enclosed volume, wherein the composite laminate of the composite laminate assembly is cured by both the electromagnetic microwave energy created by the electromagnetic radiation source, and the convective airflow provided by the heating source. A vacuum bag may be placed over the composite laminate assembly. A source may be activated such that a vacuum within the vacuum bag is created according to design specifications.
Abstract translation: 固化复合层压板的方法和装置。 该装置包括在封闭容积中产生电磁微波能量的电磁辐射源和用于在封闭容积中提供对流气流的加热源。 包括复合层压材料的复合层压组件放置在封闭的体积中，其中复合层压组件的复合叠层体由电磁辐射源产生的电磁微波能量和由加热源提供的对流气流两者固化。 真空袋可以放置在复合层压组件上。 源可以被激活，使得根据设计规范创建真空袋内的真空。
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公开(公告)号：US11407486B2
公开(公告)日：2022-08-09
申请号：US16683848
申请日：2019-11-14
Applicant: THE BOEING COMPANY
Inventor： Waeil M. Ashmawi , Sahrudine Apdalhaliem , Jaime C. Garcia
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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公开(公告)号：US20210339843A1
公开(公告)日：2021-11-04
申请号：US16866193
申请日：2020-05-04
Applicant: The Boeing Company
Inventor： Forouzan Behzadpour , Waeil M. Ashmawi
Abstract: Described herein are stringer assemblies, such as blade stringers, and methods of forming thereof. A stringer assembly comprises a first fabric composite stiffener, a second fabric composite stiffener, and an intermediate tape composite stiffener, disposed between and connected to each of the first and second stiffeners. Using three separate components allows forming sharp bends, eliminating voids and gap fillers, and adding new features, such as edge reinforcements. Each of the first and second fabric composite stiffeners comprises a web portion, a flange portion, and a curved portion, positioned between the web and flange portions. The web portions surround and are attached to the intermediate tape composite stiffener and, in some examples, include tapered-out edges for additional rigidity. The flange portions are attached to the composite base. The curved portions conform to the flared-out edges of the intermediate tape composite stiffener, which extends and connects to the composite base.
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Patent Agency Ranking
公开(公告)号：US10774858B2
公开(公告)日：2020-09-15
申请号：US15630745
申请日：2017-06-22
Applicant: The Boeing Company
Inventor： Waeil M. Ashmawi , Jaime C. Garcia , Sahrudine Apdalhaliem , Jeffery L. Marcoe , Moushumi Shome
IPC: F16B1/00
Abstract: Provided are assemblies having composite structures interlocked with shape memory alloy structures and methods of fabricating such assemblies. Interlocking may involve inserting an interlocking protrusion of a shape memory alloy structure into an interlocking opening of a composite structure and heating at least this protrusion of the shape memory alloy structure to activate the alloy and change the shape of the protrusion. This shape change engages the protrusion in the opening such that the protrusion cannot be removed from the opening. The shape memory alloy structure may be specifically trained prior to forming an assembly using a combination of thermal cycling and deformation to achieve specific pre-activation and post-activation shapes. The pre-activation shape allows inserting the interlocking protrusion into the opening, while the post-activation shape engages the interlocking protrusion within the opening. As such, activation of the shape memory alloy interlocks the two structures.
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公开(公告)号：US09682766B2
公开(公告)日：2017-06-20
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 plurality of concentric channels, a plurality of walls each defining adjacent concentric channels, each of the 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 including a plurality of openings. The plurality of openings and concentric channels are configured to provide an air flow path for conduction of air through the thermal barrier apparatus to an exterior of the thermal barrier apparatus.
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28.发明授权公开(公告)号：US09664183B2
公开(公告)日：2017-05-30
申请号：US14593106
申请日：2015-01-09
Applicant: THE BOEING COMPANY
Inventor： Sahrudine Apdalhaliem , Moushumi Shome , Kimberly D. Meredith , Waeil M. Ashmawi , Morteza Safai , Frederick T. Calkins
Abstract: Aspects of the present disclosure generally relate to an SMA actuator that includes a cooling device disposed within a torque tube. In one aspect, the cooling device includes a sliding sleeve, an expandable sleeve, and plurality of cooling fins coupled to the expandable sleeve. Axial movement of the sliding sleeve relative to the expandable sleeve facilitates radial expansion of the expandable sleeve and urges the cooling fins into contact with the torque tube. The cooling fins function as heat sinks when in contact with the torque tube to facilitate the removal of heat from the torque tube to increase the cooling rate of the torque tube. During heating of the torque tube, the cooling fins may be spaced apart from the torque tube to reduce the thermal mass that is heated, thus increasing the heating rate of the torque tube.
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公开(公告)号：US20170120512A1
公开(公告)日：2017-05-04
申请号：US15407216
申请日：2017-01-16
Applicant: The Boeing Company
Inventor： Moushumi Shome , Adriana Willempje Blom , Sahrudine Apdalhaliem , Waeil M. Ashmawi
IPC: B29C65/00 , B32B37/00 , B29C65/48 , B29C65/50 , B32B37/06 , B29C65/14 , B29C73/10 , B29C73/12 , B29C73/34 , B32B41/00 , B29C35/08
CPC classification number: B29C66/9141 , B29C35/08 , B29C35/0805 , B29C65/1425 , B29C65/1467 , B29C65/1496 , B29C65/4835 , B29C65/5021 , B29C65/5028 , B29C65/5057 , B29C65/5078 , B29C66/0342 , B29C66/12463 , B29C66/5326 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/72323 , B29C66/73941 , B29C66/843 , B29C66/8742 , B29C66/91216 , B29C66/91221 , B29C66/91411 , B29C66/91443 , B29C66/9161 , B29C66/919 , B29C66/91951 , B29C66/949 , B29C66/961 , B29C66/9672 , B29C66/9674 , B29C73/10 , B29C73/12 , B29C73/34 , B29C2035/0855 , B29K2063/00 , B29K2101/10 , B29K2105/0097 , B29L2031/30 , B29L2031/3076 , B29L2031/3082 , B29L2031/3085 , B29L2031/3091 , B29L2031/5254 , B29L2031/7692 , B32B37/0046 , B32B37/06 , B32B37/18 , B32B38/0008 , B32B41/00 , B32B43/00 , Y10T156/10 , B29K2307/04
Abstract: A method of bonding materials may comprise defining a bond interface between two materials in a cure zone on a surface of an object, and non-conductively heating the bond interface without directly heating the surface outside of the cure zone. Non-conductively heating the bond interface may involve applying microwave radiation to the bond interface.
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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。
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