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公开(公告)号：US09510398B1
公开(公告)日：2016-11-29
申请号：US13663150
申请日：2012-10-29
Applicant: The Boeing Company
Inventor： Robert James Miller , Marc R. Matsen
CPC classification number: H05B6/1209 , H05B6/062 , H05B2206/022 , H05B2206/023
Abstract: Induction heating apparatus are disclosed herein. An example induction heating apparatus disclosed herein includes a housing and a susceptor wire positioned in the housing. The susceptor wire is composed of a material having a relatively high magnetic permeability and a relatively high electrical resistivity sufficient to induce an eddy current in the susceptor wire when a magnetic field is applied to the susceptor wire via an induction source. The magnetic field generates the eddy current in the susceptor wire when a temperature of the susceptor wire is below a Curie point of the material of the susceptor wire. The susceptor wire limits heating to a temperature that is equal to or less than a Curie temperature associated with the material of the susceptor wire.
Abstract translation: 本文公开了感应加热装置。 本文公开的示例感应加热装置包括壳体和定位在壳体中的基座线。 感应线由具有较高磁导率的材料和相当高的电阻率构成，当通过感应源将磁场施加到基座线时，该电阻足以在基座线中感应出涡流。 当基座线的温度低于基座线材料的居里点时，磁场在基座线中产生涡流。 基座线将加热限制在等于或小于与基座线材料相关的居里温度的温度。
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公开(公告)号：US20160339647A1
公开(公告)日：2016-11-24
申请号：US14718893
申请日：2015-05-21
Applicant: The Boeing Company
Inventor： Marc R. Matsen , Mark A. Negley , Jeffery L. Marcoe , Stephen G. Moore , Brice A. Johnson , Alexandra K. Dillon , Megan M. Petersen
CPC classification number: B29C70/382 , B29C65/02 , B29C65/08 , B29C65/1416 , B29C65/1419 , B29C65/1432 , B29C65/1616 , B29C65/1619 , B29C65/1622 , B29C65/1632 , B29C65/18 , B29C65/22 , B29C65/30 , B29C65/32 , B29C66/1122 , B29C66/45 , B29C66/723 , B29C66/7392 , B29C66/8322 , B29C66/8362 , B29C70/38 , B29K2101/12
Abstract: A fiber placement system including a fiber placement station at a first location, the fiber placement station including a tool and a fiber placement assembly configured to construct a reinforcement layup on the tool, the first fiber placement assembly including a compaction roller rotatable about an axis of rotation, the compaction roller at least partially defining a nip, a thermoplastic composite ply extending through the nip and a heating unit positioned to heat the thermoplastic composite ply proximate the nip, and a consolidation station at a consolidation location, the consolidation location being different from the first location, the consolidation station including a consolidation tool and a consolidation system configured to consolidate a reinforcement layup assembly that includes the reinforcement layup.
Abstract translation: 一种光纤放置系统，包括在第一位置处的光纤放置台，所述光纤放置台包括工具和配置成在所述工具上构造加强层的光纤放置组件，所述第一光纤放置组件包括压缩辊， 至少部分地限定压区的压实辊，延伸穿过压区的热塑性复合层，以及定位成加热邻近压区的热塑性复合层的加热单元，以及固结位置处的固结位置， 所述第一位置，所述合并工位包括固结工具和被配置为整合包括所述加固层的加强层叠组件的合并系统。
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公开(公告)号：US20160316522A1
公开(公告)日：2016-10-27
申请号：US14697418
申请日：2015-04-27
Applicant: The Boeing Company
Inventor： Marc R. Matsen , Mark A. Negley
CPC classification number: H05B6/101 , B21D21/00 , B22F3/03 , B22F3/087 , B22F3/105 , B22F3/14 , B22F3/16 , B22F2003/1053 , B22F2202/05 , B22F2202/07 , B22F2203/00 , C21D1/18 , C21D1/42 , C21D6/00 , C21D9/42 , H05B6/06 , H05B6/08 , H05B6/105 , H05B2206/023 , Y02P10/253
Abstract: Described herein is a method of forming a heat-treated material includes positioning the heat-treated material between first and second susceptors. Each of the first and second susceptors includes a tool face shaped according to a desired shape of the heat-treated material. The method also includes applying a low-strength magnetic field to the first and second susceptors to heat the first and second susceptors. Further, the method includes compressing the heat-treated material between the first and second susceptors to form the heat-treated material into the desired shape. The method additionally includes applying a high-strength magnetic field to the heat-treated material before compressing the heat-treated material between the first and second susceptors.
Abstract translation: 这里描述的是形成热处理材料的方法，包括将热处理材料定位在第一和第二基座之间。 第一和第二基座中的每一个包括根据热处理材料的期望形状成形的工具面。 该方法还包括将低强度磁场施加到第一和第二感受器以加热第一和第二感受体。 此外，该方法包括在第一和第二基座之间压缩经热处理的材料，以将热处理的材料形成为期望的形状。 该方法还包括在将第一和第二感受器之间的热处理材料压缩之前，向热处理材料施加高强度磁场。
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公开(公告)号：US09463879B2
公开(公告)日：2016-10-11
申请号：US14195091
申请日：2014-03-03
Applicant: The Boeing Company
Inventor： Vyacheslav Khozikov , Robert J. Miller , Rangasamy Elangovan , Marc R. Matsen , Stephen R. Amorosi , Robert G. Albers , Michael Strasik , John R. Hull
Abstract: A system and method for operating an ice detection and deicing system are provided herein. The ice detection and deicing system may use changing magnetic properties of various components caused by temperature changes to detect conditions conducive to, or indicating, ice formation. The ice detection and deicing system may further use eddy currents induced in one or more layers of the system to increase the temperature of the one or more layers to reduce the amount of ice formation or reduce the probability of ice being formed.
Abstract translation: 本文提供了一种用于操作冰检测和除冰系统的系统和方法。 冰检测和除冰系统可以使用由温度变化引起的各种部件的变化的磁性，以检测有利于或指示冰的形成。 冰检测和除冰系统可以进一步使用在系统的一个或多个层中感应的涡流来增加一个或多个层的温度，以减少冰的形成量或降低形成冰的可能性。
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公开(公告)号：US20160068922A1
公开(公告)日：2016-03-10
申请号：US14942997
申请日：2015-11-16
Applicant: The Boeing Company
Inventor： Brad L. Kirkwood , Marc R. Matsen , Tony Shen , Wesley B. Crow
IPC: C21D1/42 , C22F1/18 , C21D6/00 , B23F17/00 , C21D1/60 , C21D1/613 , C21D1/74 , B21K29/00 , C22F1/10 , C21D1/62
CPC classification number: C21D1/42 , B21K29/00 , B23F17/006 , C21D1/10 , C21D1/60 , C21D1/613 , C21D1/62 , C21D1/74 , C21D6/00 , C21D6/02 , C21D9/32 , C21D10/005 , C21D2211/004 , C22F1/10 , C22F1/183 , C23C14/06 , Y02P10/253 , Y10T29/4948
Abstract: A method and apparatus are present for manufacturing a part. The part is comprised of a metal alloy and is positioned to form a positioned part. An electromagnetic field is generated that heats the positioned part. A surface of the positioned part is exposed to an inert gas, while the electromagnetic field is generated to create an inverse thermal gradient between an exterior of the positioned part and an interior section of the positioned part to form a heat treated part.
Abstract translation: 存在用于制造零件的方法和装置。 该部件由金属合金构成，并且定位成形成定位部件。 产生加热定位部件的电磁场。 定位部件的表面暴露于惰性气体中，同时产生电磁场以在定位部件的外部和定位部件的内部部分之间产生反向热梯度，以形成热处理部分。
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Patent Agency Ranking
公开(公告)号：US20150217508A1
公开(公告)日：2015-08-06
申请号：US14171779
申请日：2014-02-04
Applicant: The Boeing Company
Inventor： Angelo Rossi , Waeil M. Ashmawi , Sahrudine Apdalhaliem , Jeffery L. Marcoe , Marc R. Matsen , Aaron W. Bartel , Adriana Willempje Blom , David Reusch
CPC classification number: B29C65/72 , B29B11/16 , B29C33/448 , B29C65/62 , B29C70/24 , B29C70/504 , B29D99/0003 , B29D99/0007 , B29D99/0014 , D04C1/06 , Y02T50/43
Abstract: A method of manufacturing a radius filler may include providing a plurality of fibers, braiding the plurality of fibers into a braided preform, shaping the braided preform into a braided radius filler, and cutting the braided radius filler to a desired length.
Abstract translation: 制造半径填料的方法可以包括提供多根纤维，将多根纤维编织到编织预成型件中，将编织的预制件成形为编织半径填料，并将编织的半径填料切割成所需的长度。
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公开(公告)号：US20140099477A1
公开(公告)日：2014-04-10
申请号：US13644628
申请日：2012-10-04
Applicant: THE BOEING COMPANY
Inventor： Marc R. Matsen , Mark A. Negley
CPC classification number: B29C70/34 , B29C70/543 , Y02T50/43 , Y10T156/10 , Y10T428/24562
Abstract: A composite structure may include a laminate and a stabilizing element. The laminate may have a plurality of composite plies. The composite structure may include a geometric discontinuity that may be associated with the laminate. The stabilizing element may be included with the composite plies and may be located proximate the geometric discontinuity.
Abstract translation: 复合结构可以包括层压板和稳定元件。 层压板可以具有多个复合层。 复合结构可以包括可以与层压板相关联的几何不连续性。 稳定元件可以包括在复合层中，并且可以位于几何不连续处附近。
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公开(公告)号：US20240269942A1
公开(公告)日：2024-08-15
申请号：US18166926
申请日：2023-02-09
Applicant: The Boeing Company
Inventor： John F. Spalding , Marc R. Matsen , Gwendolyn Marie Janda
CPC classification number: B29C70/44 , B29C70/30 , B29C70/545 , B29C2793/0081 , B29L2031/3076
Abstract: Methods of forming a composite structure from a preform with a vent are presented. A preform comprises a plurality of sets of full length plies, a plurality of sets of partial plies alternating with the plurality of sets of full length plies, and a vent extending through the plurality of sets of partial plies.
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公开(公告)号：US11987389B2
公开(公告)日：2024-05-21
申请号：US16718733
申请日：2019-12-18
Applicant: The Boeing Company
Inventor： Jeffery Lee Marcoe , Marc R. Matsen
CPC classification number: B64F5/10 , B29C35/0805 , B29C70/44 , B29C2035/0811 , B29L2031/3082
Abstract: A method and apparatus for forming a composite structure. An inner tooling, a stackup, and an outer tooling are held in place together using a load constraint. A bladder and a plurality of stringer bladders in the stackup are pressurized to cause expansion of the bladder and the plurality of stringer bladders, thereby pushing together an overbraided thermoplastic skin and a plurality of overbraided thermoplastic members in the stackup. The overbraided thermoplastic skin and the plurality of overbraided thermoplastic members are co-consolidated while the bladder and the plurality of stringer bladders are pressurized to form the composite structure.
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公开(公告)号：US20240157660A1
公开(公告)日：2024-05-16
申请号：US18348131
申请日：2023-07-06
Applicant: The Boeing Company
Inventor： John F. Spalding , Marc R. Matsen , Gwendolyn Marie Janda
CPC classification number: B29C70/443 , B29C70/544
Abstract: Methods and a double vacuum processing system are presented. A double vacuum processing system comprises a first vacuum zone; a second vacuum zone encompassing the first vacuum zone; a first vacuum pump connected to the first vacuum zone and configured to draw a vacuum within the first vacuum zone; a second vacuum pump connected to the second vacuum zone and configured to draw a vacuum within the second vacuum zone; and a diverter valve. The diverter valve is configured to alternate between pneumatically connecting the first vacuum zone to the second vacuum pump or connecting the first vacuum zone to the first vacuum pump.
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