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公开(公告)号：US20210253807A1
公开(公告)日：2021-08-19
申请号：US16718086
申请日：2019-12-17
Applicant: The Boeing Company
Inventor： Andrew K. Glynn , David Andrew Pook , Steve Georgiadis , Samuel James Meure , Max Marley Osborne
Abstract: A method and apparatus for manufacturing a filler for a composite structure. The apparatus may comprise a filler. The filler may comprise a fiber matrix that is uniform in all directions. The fiber matrix may comprise a first plurality of discontinuous filaments and a second plurality of discontinuous filaments. Each filament of the first plurality of discontinuous filaments may be comprised of a stiffening material. Each filament of the second plurality of discontinuous filaments may be comprised of a binding material. Discontinuous filaments of both the first plurality of discontinuous filaments and the second plurality of discontinuous filaments may be randomly oriented and entangled with each other.
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公开(公告)号：US10445873B2
公开(公告)日：2019-10-15
申请号：US15441082
申请日：2017-02-23
Applicant: The Boeing Company
Inventor： Martin Szarski , Phillip Haeusler , David Michael Bain , Richard Bain , Andrew K. Glynn , Peter Nathan Steele
IPC: G06T7/00
Abstract: A method and apparatus for performing an automated validation of a condition of assembly for a structure. A plurality of images of the structure are registered to a computer model of the structure in which an image in the plurality of images captures a portion of the structure. Each image in the plurality of images is segmented based on registration of the plurality of images to the computer model to form a plurality of image sections. A final score is generated for the condition of assembly of the structure based on whether each image section in the plurality of image sections meets a corresponding condition in which the final score indicates whether the condition of assembly is valid.
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3.发明申请METHOD OF MANUFACTURING RESIN INFUSED COMPOSITE PARTS USING A PERFORATED CAUL SHEET 有权使用执行材料制造树脂灌注复合材料部件的方法公开(公告)号：US20130264751A1
公开(公告)日：2013-10-10
申请号：US13905630
申请日：2013-05-30
Applicant: THE BOEING COMPANY
Inventor： Peter J. Lockett , David Pook , Andrew K. Glynn
IPC: B29C70/02
CPC classification number: B29C70/021 , B29C70/443 , B29C70/548
Abstract: Resin infused composite parts are fabricated using a caul sheet having perforations therein for optimizing the flow of resin through the parts. The method allows for a simplified tooling and consumable arrangement for complex parts while achieving a smooth, aerodynamic caul-side or bag-side finish. The component may be placed in direct contact with a tool, and the caul sheet may be placed in direct contact with the component thereby eliminating the necessity for consumables between these items.
Abstract translation: 使用其中具有穿孔的塞子片制造树脂注入的复合部件，以优化通过部件的树脂的流动。 该方法允许对复杂部件进行简化的加工和消耗性布置，同时实现平滑的空气动力学侧面或袋侧面的完成。 该部件可以放置在与工具直接接触的位置，并且可以将止动片与部件直接接触，从而消除了这些物品之间消耗品的必要性。
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4.发明授权公开(公告)号：US10059061B2
公开(公告)日：2018-08-28
申请号：US14877469
申请日：2015-10-07
Applicant: THE BOEING COMPANY
Inventor： Lauren A. Burns , Max M. Osborne , Martin A. Szarski , Ronnie K. Ligeti , David Pook , Andrew K. Glynn
CPC classification number: B29C64/386 , B29C35/0266 , B29C35/0288 , B29C70/44 , B29C2037/90 , B33Y50/02 , G05B19/182 , G05B2219/36039 , Y02T50/43
Abstract: A system for manufacturing a composite structure includes a tool with a surface for supporting component elements of the composite structure. The surface is divided into a multi-dimensional array of thermal zones for in-process control of the temperature of a component element (e.g. resin) of the composite structure. The sensors sense a characteristic of the component element and provide sensor data, which is applied to a machine-learning algorithm configured to generate control data to achieve a defined quality goal. A controller then independently controls the thermal zones to locally heat, cool or maintain the temperature of the component element according to the control data to advance the component element or composite structure to the defined quality goal. This may be performed over a plurality of instances during which the machine-learning algorithm learns to increase advancement of the component element or composite structure to the defined quality goal.
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公开(公告)号：US20180240226A1
公开(公告)日：2018-08-23
申请号：US15441082
申请日：2017-02-23
Applicant: The Boeing Company
Inventor： Martin Szarski , Phillip Haeusler , David Michael Bain , Richard Bain , Andrew K. Glynn , Peter Nathan Steele
CPC classification number: G06T7/001 , G06T7/0008 , G06T2207/10016 , G06T2207/30136
Abstract: A method and apparatus for performing an automated validation of a condition of assembly for a structure. A plurality of images of the structure are registered to a computer model of the structure in which an image in the plurality of images captures a portion of the structure. Each image in the plurality of images is segmented based on registration of the plurality of images to the computer model to form a plurality of image sections. A final score is generated for the condition of assembly of the structure based on whether each image section in the plurality of image sections meets a corresponding condition in which the final score indicates whether the condition of assembly is valid.
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Patent Agency Ranking
6.发明授权Composite structures having integrated stiffeners with smooth runouts and method of making the same 有权具有集成的具有平滑跳动的加强件的复合结构及其制造方法公开(公告)号：US09440402B2
公开(公告)日：2016-09-13
申请号：US14141433
申请日：2013-12-27
Applicant: The Boeing Company
Inventor： David A. Pook , Peter J. Lockett , Andrew K. Glynn
IPC: B29C70/48 , B29C70/06 , B29B11/04 , B29C65/50 , B29C65/56 , B29C65/00 , B29C70/44 , B29C70/86 , B29D99/00 , B64C1/12 , B64C1/14 , B64C3/26 , B29C65/48 , B29K101/10 , B29K105/08 , B29L9/00 , B29L31/30
CPC classification number: B29C70/48 , B29B11/04 , B29C65/4835 , B29C65/5057 , B29C65/564 , B29C66/112 , B29C66/1122 , B29C66/131 , B29C66/472 , B29C66/4722 , B29C66/474 , B29C66/532 , B29C66/61 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/723 , B29C66/7394 , B29C66/81455 , B29C70/06 , B29C70/443 , B29C70/865 , B29D99/0014 , B29D99/0017 , B29K2101/10 , B29K2105/0827 , B29L2009/00 , B29L2031/3076 , B29L2031/3082 , B64C1/12 , B64C1/1446 , B64C3/26 , Y02T50/43 , Y10T156/10 , Y10T428/24488 , Y10T428/24521 , Y10T428/2457 , Y10T428/24612 , B29K2307/04 , B29K2309/08 , B29K2301/00
Abstract: A unitized composite structure comprises a composite member having at least one integrally formed composite stiffener. At least one end of the stiffener includes a runout forming a substantially smooth transition between the stiffener and the composite structure.
Abstract translation: 组合复合结构包括具有至少一个整体形成的复合加强件的复合构件。 加强件的至少一端包括在加强件和复合结构之间形成基本上平滑的过渡的跳动。
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公开(公告)号：US20140117159A1
公开(公告)日：2014-05-01
申请号：US14146923
申请日：2014-01-03
Applicant: The Boeing Company
Inventor： Andrew K. Glynn , Steve Georgiadis , David Andrew Pook
CPC classification number: B64C1/061 , B32B37/1284 , B32B37/18 , B64C2001/0072 , B64C2001/0081 , Y02T50/43 , Y10T29/49622 , Y10T428/24669
Abstract: A composite frame includes a plurality of truss elements covered by a cap. The truss elements are flexibly coupled with each other and with the cap. The frame flexes to conform to a contoured surface to which it is attached. Once attached, the installed frame provides the required rigidity to the structure.
Abstract translation: 复合框架包括被盖覆盖的多个桁架元件。 桁架元件彼此柔性地连接并与盖子相连。 框架弯曲以符合与其连接的轮廓表面。 一旦连接，安装的框架为结构提供了所需的刚性。
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公开(公告)号：US20170029577A1
公开(公告)日：2017-02-02
申请号：US14812458
申请日：2015-07-29
Applicant: The Boeing Company
Inventor： Andrew K. Glynn , David Andrew Pook , Steve Georgiadis , Samuel James Meure , Max Marley Osborne
CPC classification number: C08J5/04 , B29C43/003 , B29C70/081 , B29C70/46 , B29C70/508 , B29K2105/12 , C08J2300/22 , C08J2300/24
Abstract: A method and apparatus for manufacturing a filler for a composite structure. The apparatus may comprise a filler. The filler may comprise a fiber matrix that is uniform in all directions. The fiber matrix may comprise a first plurality of discontinuous filaments and a second plurality of discontinuous filaments. Each filament of the first plurality of discontinuous filaments may be comprised of a stiffening material. Each filament of the second plurality of discontinuous filaments may be comprised of a binding material. Discontinuous filaments of both the first plurality of discontinuous filaments and the second plurality of discontinuous filaments may be randomly oriented and entangled with each other.
Abstract translation: 一种复合结构填料的制造方法和装置。 该装置可以包括填充物。 填料可以包括在所有方向上均匀的纤维基质。 纤维基质可以包括第一多个不连续长丝和第二多个不连续长丝。 第一多个不连续长丝中的每根细丝可以由加强材料构成。 第二多个不连续长丝中的每根细丝可以由粘结材料构成。 第一多个不连续长丝和第二多个不连续长丝两者的不连续长丝可以是随机取向的并且彼此缠结。
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公开(公告)号：US20150125565A1
公开(公告)日：2015-05-07
申请号：US14594129
申请日：2015-01-11
Applicant: The Boeing Company
Inventor： Peter J. Lockett , David Pook , Andrew K. Glynn
IPC: B29C70/42
CPC classification number: B29C70/42 , B29C37/0085 , B29C70/443 , B29L2031/00 , B29L2031/06
Abstract: Resin infused composite parts are fabricated using a caul sheet having perforations therein for optimizing the flow of resin through the parts and allowing a simplified tooling and consumable arrangement for complex parts while achieving a smooth, aerodynamic caul-side or bag-side finish.
Abstract translation: 树脂注入的复合部件使用其中具有穿孔的密封片制造，以优化通过部件的树脂流动，并且允许简单的工具和消耗性配置用于复杂部件，同时实现平滑的空气动力学侧面或袋侧面。
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公开(公告)号：US09682516B2
公开(公告)日：2017-06-20
申请号：US14594129
申请日：2015-01-11
Applicant: The Boeing Company
Inventor： Peter J. Lockett , David Pook , Andrew K. Glynn
CPC classification number: B29C70/42 , B29C37/0085 , B29C70/443 , B29L2031/00 , B29L2031/06
Abstract: Resin infused composite parts are fabricated using a caul sheet having perforations therein for optimizing the flow of resin through the parts and allowing a simplified tooling and consumable arrangement for complex parts while achieving a smooth, aerodynamic caul-side or bag-side finish.
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