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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：US20180009136A1
公开(公告)日：2018-01-11
申请号：US15205460
申请日：2016-07-08
Applicant: The Boeing Company
Inventor： Diane C. Rawlings , Bruce K. Keough , Larry K. Olli , Alan G. Burg , James M. Kestner , George Michael Granger , James Charles McGarvey
CPC classification number: B29C39/146 , B29C39/148 , B29C39/16 , B29C39/18 , B29C39/38 , B29C41/30 , B29C41/32 , B29C41/46 , B29C65/7894 , B29D2009/00 , B29K2101/12 , B29L2007/00 , B29L2009/00 , B29L2031/3076 , B29L2031/756 , B32B3/30 , B32B27/283 , B32B37/0053 , B32B37/02 , B32B37/10 , B32B37/203 , B32B37/24 , B32B2037/243 , B32B2371/00 , B32B2375/00 , B32B2398/20 , B32B2605/18 , B64C21/10 , B64C2230/26
Abstract: Multilayer riblet applique and methods of producing the same are described herein. One disclosed example method includes applying a first high elongation polymer material to a web tool, where the web tool is to be provided from a first roll, and heating, via a first heating process, the first high elongation polymer material. The disclosed example method also includes applying a second high elongation polymer material to the first high elongation polymer material, and heating, via a second heating process, the second high elongation polymer material. The disclosed example method also includes applying, via a laminating roller, a support layer to the second high elongation polymer material.
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公开(公告)号：US20190283342A1
公开(公告)日：2019-09-19
申请号：US16432881
申请日：2019-06-05
Applicant: The Boeing Company
Inventor： James M. Kestner , Marc R. Matsen , Scott D. Billings , John A. Mittleider , Robert J. Miller
Abstract: A processing apparatus such as a heating and/or debulking apparatus that may be used to debulk a plurality of uncured composite layers to form an article such as an aircraft component may include a plurality of interconnected smart susceptor heater blankets. The plurality of smart susceptor heater blankets may be connected in series or in parallel, and may be controlled to uniformly heat the component during formation.
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公开(公告)号：US20160262216A1
公开(公告)日：2016-09-08
申请号：US14640227
申请日：2015-03-06
Applicant: The Boeing Company
Inventor： James M. Kestner , Robert James Miller , Marc Rollo Matsen , Cameron Kai-Ming Chen , Leah Gillian Glauber , Christopher John Hottes
CPC classification number: H05B6/105 , H05B6/40 , H05B2206/023
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.
Abstract translation: 感受器线阵列。 阵列包括第一基座线，其包括具有第一居里温度点的合金和包括具有第二居里温度点的合金的第二基座线，第二居里温度点不同于第一基座线的第一居里温度点。 在一个基座线布置中，第二基座线的第二居里温度点低于第一基座线的第一居里温度点。 在另一基座线布置中，阵列还包括第三基座线，第三基座线包括具有第三居里温度点的合金。 第三基座线的第三居里温度点可以不同于第一基座线的第一居里温度点。
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公开(公告)号：US20160143092A1
公开(公告)日：2016-05-19
申请号：US14548045
申请日：2014-11-19
Applicant: The Boeing Company
Inventor： Robert James Miller , Marc Rollo Matsen , Cameron Kai-Ming Chen , Leah Gillian Glauber , James M. Kestner , Christopher John Hottes
CPC classification number: H05B6/105 , C22C38/08 , H05B6/06 , H05B6/14 , H05B6/40 , H05B2206/023 , Y02P10/253
Abstract: A coaxially arranged smart susceptor conductor, comprising a smart susceptor core comprising an alloy having a first Curie temperature point and a first smart susceptor shell coaxially arranged around the smart susceptor core. The first smart susceptor shell comprising a second Curie temperature point that is different than the first Curie temperature point of the smart susceptor core. In one arrangement, the second Curie temperature point of the first smart susceptor shell is lower than the first Curie temperature point of the smart susceptor core. In another arrangement, the smart susceptor conductor further comprises a second smart susceptor shell disposed about the first smart susceptor shell. The second smart susceptor shell comprising a third Curie temperature point.
Abstract translation: 一种同轴布置的智能基座导体，包括智能基座芯，其包括具有第一居里温度点的合金和位于智能基座芯周围同轴布置的第一智能基座壳。 第一智能基座壳包括不同于智能感受体芯的第一居里温度点的第二居里温度点。 在一种布置中，第一智能基座壳的第二居里温度点低于智能感受体芯的第一居里温度点。 在另一种布置中，智能感受体导体还包括围绕第一智能基座壳布置的第二智能基座壳。 第二智能感受器壳包括第三居里温度点。
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Patent Agency Ranking
公开(公告)号：US11884055B2
公开(公告)日：2024-01-30
申请号：US16365431
申请日：2019-03-26
Applicant: The Boeing Company
Inventor： Kay Y. Blohowiak , Denise A. Blohowiak , James M. Kestner
CPC classification number: B32B7/12 , B32B15/08 , B32B37/12 , B32B38/00 , B32B38/162 , B64C1/00 , B32B2038/0064 , B32B2307/712 , B32B2605/18 , B64C2001/0072 , B64C2001/0081
Abstract: There is provided a laminated hybrid metallized polymer film for erosion protection of a composite structure. The laminated hybrid metallized polymer film includes a metal foil layer, a laminating adhesive layer underlying the metal foil layer, and a polymer film layer underlying the laminating adhesive layer. The polymer film layer is laminated to the metal foil layer with the laminating adhesive layer coupled between the metal foil layer and the polymer film layer. The laminated hybrid metallized polymer film further includes an adhesive layer underlying the polymer film layer. The adhesive layer adheres the polymer film layer to a substrate surface of the composite structure. The metal foil layer, the laminating adhesive layer, the polymer film layer, and the adhesive layer form the laminated hybrid metallized polymer film for application over and to the substrate surface of the composite structure.
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公开(公告)号：US10336013B2
公开(公告)日：2019-07-02
申请号：US15056297
申请日：2016-02-29
Applicant: The Boeing Company
Inventor： James M. Kestner , Marc R. Matsen , Scott D. Billings , John A. Mittleider , Robert J. Miller
IPC: B32B41/00 , B29C70/34 , H05B3/34 , B29K105/08 , B29L31/30
Abstract: A processing apparatus such as a heating and/or debulking apparatus that may be used to debulk a plurality of uncured composite layers to form an article such as an aircraft component may include a plurality of interconnected smart susceptor heater blankets. The plurality of smart susceptor heater blankets may be connected in series or in parallel, and may be controlled to uniformly heat the component during formation.
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公开(公告)号：US10220579B2
公开(公告)日：2019-03-05
申请号：US15884138
申请日：2018-01-30
Applicant: The Boeing Company
Inventor： Andrew M. Hopkins , Donald J. Sutkus , James M. Kestner , Jennifer S. Noel , Robert J. Miller , Marc R. Matsen , Christopher J. Hottes , Mark E. King , Darren R. Walker
Abstract: A processing apparatus such as a heating and/or debulking apparatus that may be used to debulk a plurality of uncured composite layers to form an article such as an aircraft component may include a plurality of interconnected smart susceptor heater blankets. The plurality of smart susceptor heater blankets may be connected in series or in parallel, and may be controlled to uniformly heat the component during formation.
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公开(公告)号：US09914269B2
公开(公告)日：2018-03-13
申请号：US15056783
申请日：2016-02-29
Applicant: The Boeing Company
Inventor： Andrew M. Hopkins , Donald J. Sutkus , James M. Kestner , Jennifer S. Noel , Robert J. Miller , Marc R. Matsen , Christopher J. Hottes , Mark E. King , Darren R. Walker
CPC classification number: B29C70/342 , B29C2035/0811 , B29C2035/0816 , B29K2105/089 , B29L2031/3076 , H05B3/34 , H05B6/105 , H05B2203/003 , H05B2203/007 , H05B2206/023 , Y02T50/43
Abstract: A processing apparatus such as a heating and/or debulking apparatus that may be used to debulk a plurality of uncured composite layers to form an article such as an aircraft component may include a plurality of interconnected smart susceptor heater blankets. The plurality of smart susceptor heater blankets may be connected in series or in parallel, and may be controlled to uniformly heat the component during formation.
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公开(公告)号：US20160325823A1
公开(公告)日：2016-11-10
申请号：US14705547
申请日：2015-05-06
Applicant: The Boeing Company
Inventor： Diane C. Rawlings , Timothy Leroy Williams , James C. McGarvey , James M. Kestner , Alan G. Burg
IPC: B64C21/10
CPC classification number: B64C21/10 , B32B3/30 , B41M3/00 , B42D25/324 , B44B5/0047 , B44B5/0095 , B44F1/02 , B64C23/00 , B64C2230/26 , B64D45/00 , F15D1/00 , G09F19/12 , G09F19/14 , G09F21/08 , Y02T50/166
Abstract: Aerodynamic microstructures having sub-microstructure are disclosed herein. One disclosed example apparatus includes an aerodynamic microstructure defining an external surface of a vehicle, and a pattern of sub-microstructures superimposed on the microstructure to convey a representation of an image.
Abstract translation: 本文公开了具有亚微观结构的气动微结构。 一个公开的示例性装置包括限定车辆的外表面的空气动力学微结构和叠加在微结构上以传送图像的表示的子微结构的图案。
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