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公开(公告)号：US20170135156A1
公开(公告)日：2017-05-11
申请号：US14937472
申请日：2015-11-10
Applicant: THE BOEING COMPANY
Inventor： Robert J. Miller , Christopher J. Hottes
CPC classification number: H05B3/36 , H05B1/0202 , H05B1/0272 , H05B6/105 , H05B2206/023
Abstract: A heating blanket is disclosed. The heating blanket may include a conductor yarn configured to receive electrical current and generate a magnetic field in response to the electrical current, and a plurality of susceptor yarns composed of a magnetic material including a Curie point. The conductor yarn and the plurality of susceptor yarns may be interlaced to form a layer of fabric.
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公开(公告)号：US10814526B2
公开(公告)日：2020-10-27
申请号：US15713424
申请日：2017-09-22
Applicant: The Boeing Company
Inventor： Marc R. Matsen , Timothy J. Luchini , Bret A. Voss , Christopher J. Hottes
Abstract: A first tooling die and a second tooling die are movable with respect to each other. The first tooling die and the second tooling die form a die cavity. The first tooling die and the second tooling die comprise a plurality of stacked metal sheets. A plurality of air gaps is defined between adjacent stacked metal sheets. A first smart susceptor material is within the die cavity and connected to the first tooling die. The first smart susceptor material has a first Curie temperature. A second smart susceptor material is within the die cavity and associated with the second tooling die. The second smart susceptor material has a second Curie temperature lower than the first Curie temperature. A flexible membrane is between the second tooling die and the first smart susceptor material. The flexible membrane is configured to receive pressure.
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公开(公告)号：US20190091893A1
公开(公告)日：2019-03-28
申请号：US15713424
申请日：2017-09-22
Applicant: The Boeing Company
Inventor： Marc R. Matsen , Timothy J. Luchini , Bret A. Voss , Christopher J. Hottes
CPC classification number: B29C33/06 , B29C35/0805 , B29C70/44 , B29C70/46 , B29C2035/0811 , B29C2035/0816 , B29K2101/10 , B30B5/02
Abstract: A first tooling die and a second tooling die are movable with respect to each other. The first tooling die and the second tooling die form a die cavity. The first tooling die and the second tooling die comprise a plurality of stacked metal sheets. A plurality of air gaps is defined between adjacent stacked metal sheets. A first smart susceptor material is within the die cavity and connected to the first tooling die. The first smart susceptor material has a first Curie temperature. A second smart susceptor material is within the die cavity and associated with the second tooling die. The second smart susceptor material has a second Curie temperature lower than the first Curie temperature. A flexible membrane is between the second tooling die and the first smart susceptor material. The flexible membrane is configured to receive pressure.
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公开(公告)号：US11051368B2
公开(公告)日：2021-06-29
申请号：US14937472
申请日：2015-11-10
Applicant: The Boeing Company
Inventor： Robert J. Miller , Christopher J. Hottes
Abstract: A heating blanket is disclosed. The heating blanket may include a conductor yarn configured to receive electrical current and generate a magnetic field in response to the electrical current, and a plurality of susceptor yarns composed of a magnetic material including a Curie point. The conductor yarn and the plurality of susceptor yarns may be interlaced to form a layer of fabric.
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公开(公告)号：US20210001515A1
公开(公告)日：2021-01-07
申请号：US17026066
申请日：2020-09-18
Applicant: The Boeing Company
Inventor： Marc R. Matsen , Timothy J. Luchini , Bret A. Voss , Christopher J. Hottes
Abstract: A first tooling die and a second tooling die are movable with respect to each other. The first tooling die and the second tooling die form a die cavity. The first tooling die and the second tooling die comprise a plurality of stacked metal sheets. A plurality of air gaps is defined between adjacent stacked metal sheets. A first smart susceptor material is within the die cavity and connected to the first tooling die. The first smart susceptor material has a first Curie temperature. A second smart susceptor material is within the die cavity and associated with the second tooling die. The second smart susceptor material has a second Curie temperature lower than the first Curie temperature. A flexible membrane is between the second tooling die and the first smart susceptor material. The flexible membrane is configured to receive pressure.
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Patent Agency Ranking
公开(公告)号：US11452178B2
公开(公告)日：2022-09-20
申请号：US14937511
申请日：2015-11-10
Applicant: The Boeing Company
Inventor： Robert J. Miller , John F. Spalding, Jr. , Diane C. Rawlings , Darrell M. Storvick , Christopher J. Hottes
Abstract: A heating blanket is disclosed. The heating blanket may include a thermoplastic matrix configured to become conformable at a predetermined temperature, a conductor embedded in the thermoplastic matrix and configured to receive electrical current and generate a magnetic field in response to the electrical current, and a plurality of susceptors embedded in the thermoplastic matrix and composed of a magnetic material having a Curie point.
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公开(公告)号：US20180147794A1
公开(公告)日：2018-05-31
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
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：US20170246817A1
公开(公告)日：2017-08-31
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：US11541575B2
公开(公告)日：2023-01-03
申请号：US17026066
申请日：2020-09-18
Applicant: The Boeing Company
Inventor： Marc R. Matsen , Timothy J. Luchini , Bret A. Voss , Christopher J. Hottes
IPC: B29C33/06 , B29C35/08 , B29C70/44 , B30B5/02 , B29K101/10
Abstract: A first tooling die and a second tooling die are movable with respect to each other. The first tooling die and the second tooling die form a die cavity. The first tooling die and the second tooling die comprise a plurality of stacked metal sheets. A plurality of air gaps is defined between adjacent stacked metal sheets. A first smart susceptor material is within the die cavity and connected to the first tooling die. The first smart susceptor material has a first Curie temperature. A second smart susceptor material is within the die cavity and associated with the second tooling die. The second smart susceptor material has a second Curie temperature lower than the first Curie temperature. A flexible membrane is between the second tooling die and the first smart susceptor material. The flexible membrane is configured to receive pressure.
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公开(公告)号：US11220064B2
公开(公告)日：2022-01-11
申请号：US16132311
申请日：2018-09-14
Applicant: The Boeing Company
Inventor： Marc R. Matsen , Bret Alan McGinness Voss , Vincent C. Ku , Christopher J. Hottes
Abstract: A composite sandwich panel includes a first composite part and a second composite part. A plurality of stiffeners extend between the first and second composite parts. A fiberglass composite perimeter edge closeout is positioned along one or more edges of the first and second composite parts. The fiberglass composite perimeter edge closeout controls a magnetic flux to bond the first and second composite parts to the plurality of stiffeners.
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