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公开(公告)号：US10827566B2
公开(公告)日：2020-11-03
申请号：US16105766
申请日：2018-08-20
Applicant: The Boeing Company
Inventor： James M. Kestner , Robert James Miller , Marc Rollo Matsen , Cameron Kai-Ming Chen , Leah Gillian Glauber , Christopher John Hottes
Abstract: A susceptor wire array. The array includes a first susceptor wire comprising an alloy having a first Curie temperature point and a second susceptor wire comprising an alloy having a second Curie temperature point, the second Curie temperature point is different than the first Curie temperature point of the first susceptor wire. In one susceptor wire arrangement, the second Curie temperature point of the second susceptor wire is lower than the first Curie temperature point of the first susceptor wire. In another susceptor wire arrangement, the array further comprises a third susceptor wire, the third susceptor wire comprising an alloy having a third Curie temperature point. The third Curie temperature point of the third susceptor wire may be different than the first Curie temperature point of the first susceptor wire.
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公开(公告)号：US09868249B2
公开(公告)日：2018-01-16
申请号：US13942055
申请日：2013-07-15
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Robert James Miller , William C. Dykstra
IPC: H05B6/10 , B29C65/36 , B29C65/48 , B29C65/50 , B29C65/00 , B64F5/10 , B29L31/30 , B64C1/12 , B64C3/26
CPC classification number: B29C65/3668 , B29C65/3632 , B29C65/368 , B29C65/4815 , B29C65/5014 , B29C65/5021 , B29C65/5057 , B29C66/003 , B29C66/112 , B29C66/131 , B29C66/474 , B29C66/49 , B29C66/712 , B29C66/721 , B29C66/7212 , B29C66/73921 , B29C66/8122 , B29C66/8432 , B29C66/91411 , B29C66/91651 , B29C66/959 , B29L2031/3076 , B64C1/12 , B64C3/26 , B64F5/10 , B29K2309/08 , B29K2909/02
Abstract: A method and apparatus for performing induction welding. A number of protective layers are positioned between a susceptor layer and at least one of a plurality of workpieces at a weld location. An undesired current path is prevented from forming at the weld location during induction heating of the plurality of workpieces by the number of protective layers.
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公开(公告)号：US20170203497A1
公开(公告)日：2017-07-20
申请号：US15477723
申请日：2017-04-03
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Robert James Miller
CPC classification number: B29C65/02 , B23K13/04 , B29C65/3632 , B29C65/3668 , B29C65/368 , B29C66/00145 , B29C66/54 , B29C66/721 , B29C66/73921 , B29C66/73941 , B29C66/81455 , B29C66/81461 , B29L2031/3085 , B29L2031/711 , B64C3/26
Abstract: A method and apparatus for joining parts. A plurality of conformable induction coils embedded in a number of elastomeric sheets is positioned relative to a first composite part of the parts and a second composite part of the parts. A magnetic field is generated with the plurality of conformable induction coils. The magnetic field is configured to generate heat in a magnetically permeable material at a joint location. The heat joins the first composite part and the second composite part to each other.
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公开(公告)号：US20160105929A1
公开(公告)日：2016-04-14
申请号：US14512329
申请日：2014-10-10
Applicant: The Boeing Company
Inventor： John F. Spalding, JR. , Christopher John Hottes , Robert James Miller
CPC classification number: H05B3/04 , H01R13/5219 , H05B3/06 , H05B3/34 , H05B2203/003
Abstract: An apparatus may include a curing apparatus and an electrical coupler. The curing apparatus may include one or more electrical components related to curing a composite material inside a vacuum chamber at least partially defined by a flexible wall. The electrical coupler may be connected to the curing apparatus. The coupler may include a first set of one or more electrical contacts electrically connected to the one or more electrical components of the curing apparatus inside the vacuum chamber. The coupler may be configured to hermetically extend through a hole in the flexible wall. Such extension may dispose the first set of one or more electrical contacts in a space outside of the vacuum chamber for electrical interconnection of the one or more electrical components of the curing apparatus inside the vacuum chamber with circuitry disposed in the space outside of the vacuum chamber.
Abstract translation: 设备可以包括固化装置和电耦合器。 固化设备可以包括一个或多个电气部件，其涉及固化至少部分地由柔性壁限定的真空室内的复合材料。 电连接器可以连接到固化设备。 联接器可以包括电连接到真空室内的固化设备的一个或多个电气部件的一个或多个电触点的第一组。 联接器可以被配置为气密地延伸通过柔性壁中的孔。 这种延伸可以将第一组一个或多个电触点设置在真空室外部的空间中，用于将真空室内的固化设备的一个或多个电气部件与设置在真空室外部的空间的电路电互连 。
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公开(公告)号：US20150014304A1
公开(公告)日：2015-01-15
申请号：US13942055
申请日：2013-07-15
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Robert James Miller , William C. Dykstra
IPC: H05B6/10
CPC classification number: B29C65/3668 , B29C65/3632 , B29C65/368 , B29C65/4815 , B29C65/5014 , B29C65/5021 , B29C65/5057 , B29C66/003 , B29C66/112 , B29C66/131 , B29C66/474 , B29C66/49 , B29C66/712 , B29C66/721 , B29C66/7212 , B29C66/73921 , B29C66/8122 , B29C66/8432 , B29C66/91411 , B29C66/91651 , B29C66/959 , B29L2031/3076 , B64C1/12 , B64C3/26 , B64F5/10 , B29K2309/08 , B29K2909/02
Abstract: A method and apparatus for performing induction welding. A number of protective layers are positioned between a susceptor layer and at least one of a plurality of workpieces at a weld location. An undesired current path is prevented from forming at the weld location during induction heating of the plurality of workpieces by the number of protective layers.
Abstract translation: 一种用于进行感应焊接的方法和装置。 多个保护层位于基座层和多个工件中的至少一个在焊接位置处。 在多个工件的感应加热期间，通过保护层的数量，防止在焊接位置处形成不期望的电流路径。
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Patent Agency Ranking
公开(公告)号：US08726737B2
公开(公告)日：2014-05-20
申请号：US13764866
申请日：2013-02-12
Applicant: The Boeing Company
Inventor： Gary E. Georgeson , Robert James Miller
IPC: G01B7/16
CPC classification number: G01L1/12 , B29C65/4855 , B29C65/4875 , B29C65/489 , B29C65/8284 , B29C66/721 , B29K2995/0008 , B29L2031/3076 , B64D2045/0085 , B64F5/60 , G01B7/24 , G01L1/125 , G01M5/0033 , G01M5/0066 , G01M5/0083 , G01M5/0091 , G01R33/098 , G01R33/1269 , G08C17/02 , Y10T428/31504
Abstract: A structural health monitoring system for multiple layer structures includes a plurality of strain-sensitive magnetic particles dispersed within a bonding area between at least two individual layers, at least one multiferroic sensor dispersed on a surface of the multiple layer structure, proximate to an area of the structure to be monitored, the at least one multiferroic sensor capable of monitoring strains experienced by the strain-sensitive magnetic particles, and analyzing changes in the strains experienced by said strain-sensitive magnetic particles that may indicate damage or degradation in the structure, and a controller configured for periodic interrogation of the at least one multiferroic sensor.
Abstract translation: 用于多层结构的结构健康监测系统包括分散在至少两个单独层之间的结合区域内的多个应变敏感磁性颗粒，分散在多层结构的表面上的至少一个多铁性传感器， 待监测的结构，所述至少一个能够监测应变敏感磁性颗粒经历的应变的多铁性传感器，以及分析所述应变敏感性磁性颗粒经历的可能指示结构的损伤或降解的变化，以及 控制器，被配置为周期性询问所述至少一个多铁性传感器。
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公开(公告)号：US20140116597A1
公开(公告)日：2014-05-01
申请号：US13665969
申请日：2012-11-01
Applicant: The Boeing Company
Inventor： Robert James Miller , Diane C. Rawlings
CPC classification number: B29C63/0065 , B29C2063/485 , H05B6/105 , H05B6/145 , H05B2206/023 , Y10T156/10
Abstract: Methods and an apparatus are provided for heating a material. The apparatus includes a roller that includes at least one susceptor contained therein, and at least one induction coil coupled to the roller. The induction coil is configured to induce a magnetic field in the susceptor to facilitate increasing a temperature of the roller.
Abstract translation: 提供了用于加热材料的方法和装置。 该装置包括一个包括至少一个包含在其中的基座的滚子，以及耦合到该滚筒的至少一个感应线圈。 感应线圈构造成在基座中引起磁场，以便于增加滚筒的温度。
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公开(公告)号：US10588177B2
公开(公告)日：2020-03-10
申请号：US15727804
申请日：2017-10-09
Applicant: The Boeing Company
Inventor： John F. Spalding, Jr. , Christopher John Hottes , Robert James Miller
Abstract: A method of supplying electricity to an electrical component inside a vacuum chamber may include positioning an electrical component inside a vacuum chamber, the electrical component having a first electrical connector portion. A second electrical connector portion may then be connected to the first electrical portion through a hole in a flexible wall of the vacuum chamber, the second electrical connector portion being electrically connected to circuitry disposed outside the vacuum chamber. The connecting step may include hermetically clamping the flexible wall of the vacuum chamber between the first and second electrical connector portions.
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公开(公告)号：US09986602B2
公开(公告)日：2018-05-29
申请号：US14640234
申请日：2015-03-06
Applicant: The Boeing Company
Inventor： Cameron Kai-Ming Chen , Robert James Miller , Marc Rollo Matsen , Leah Gillian Glauber , James M. Kestner , Christopher John Hottes , Wendi Lynn Pickett Otto
CPC classification number: H05B6/105 , B29C35/0805 , B29C2035/0811 , B29C2035/0816 , H05B6/40 , H05B2206/023
Abstract: An enclosure for heating a three dimensional structure. The enclosure comprising a body defining a cavity therein. The cavity sized to receive a three dimensional structure. A plurality of heating blankets configured to heat the three dimensional structure to a substantially uniform temperature. At least one of the plurality of heating blankets comprises a conductor for receiving current and generating a magnetic field in response thereto, a first susceptor wire comprising an alloy having a first Curie temperature point and a second susceptor wire. The second susceptor wire comprising a second Curie temperature point that is different than the first Curie temperature point of the first susceptor wire.
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公开(公告)号：US20180035489A1
公开(公告)日：2018-02-01
申请号：US15727804
申请日：2017-10-09
Applicant: The Boeing Company
Inventor： John F. Spalding, JR. , Christopher John Hottes , Robert James Miller
CPC classification number: H05B3/04 , H01R13/5219 , H05B3/06 , H05B3/34 , H05B2203/003
Abstract: A method of supplying electricity to an electrical component inside a vacuum chamber may include positioning an electrical component inside a vacuum chamber, the electrical component having a first electrical connector portion. A second electrical connector portion may then be connected to the first electrical portion through a hole in a flexible wall of the vacuum chamber, the second electrical connector portion being electrically connected to circuitry disposed outside the vacuum chamber. The connecting step may include hermetically clamping the flexible wall of the vacuum chamber between the first and second electrical connector portions.
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