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1.
公开(公告)号:US20200164547A1
公开(公告)日:2020-05-28
申请号:US16201553
申请日:2018-11-27
Applicant: The Boeing Company
Inventor: Bret A. Voss , Marc R. Matsen , Jeffrey H. Olberg , John F. Spalding
Abstract: Heating apparatus and methods for forming a part with a non-planar shape include a table formed of a thermally conductive material and defining a table surface. A tool, also formed of a thermally conductive material, has a base surface configured to engage the table surface of the table and a tooling surface opposite the base surface, wherein the tooling surface has a contoured shape that is non-planar. A heating blanket is provided above the table and defines a heating surface. The tooling surface of the tool is configured to engage a first surface of the part and the heating surface of the heating blanket is configured to engage a second surface of the part opposite the first surface of the part. The table and the heating blanket are heated to a processing temperature so that the part at least partially conforms to the tooling surface of the tool.
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公开(公告)号:US09789747B2
公开(公告)日:2017-10-17
申请号:US14448305
申请日:2014-07-31
Applicant: The Boeing Company
Inventor: John Ralph Hull , Michael Strasik , Bret A. Voss , Mark A. Negley , William J. Sweet , Kevin R. Housen , Jason S. Damazo , Michael D. Gonzales , Michael Howard-Edward Ware , Lee Charles Firth
IPC: F16L57/00 , F16L9/14 , B60H1/00 , F16L57/02 , F17D5/02 , F16L59/14 , F16L55/17 , B32B1/08 , B32B3/26 , B32B5/02 , F16L57/04
CPC classification number: B60H1/00564 , B32B1/08 , B32B3/266 , B32B5/024 , B32B2262/101 , B32B2307/304 , B32B2307/558 , B32B2605/18 , F16L55/07 , F16L55/17 , F16L57/02 , F16L57/04 , F16L59/145 , F17D5/02
Abstract: Methods and systems for duct protection of a vehicle are provided. The methods and systems provided include an apparatus for containing a flow of fluid discharged from a fracture in a duct. The apparatus includes a ballistic containment layer and an insulation sheath coupled to the ballistic containment layer. The insulation sheath includes a first air containment layer, an insulation layer, and a second air containment layer.
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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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5.
公开(公告)号:US11440224B2
公开(公告)日:2022-09-13
申请号:US16201553
申请日:2018-11-27
Applicant: The Boeing Company
Inventor: Bret A. Voss , Marc R. Matsen , Jeffrey H. Olberg , John F. Spalding
Abstract: Heating apparatus and methods for forming a part with a non-planar shape include a table formed of a thermally conductive material and defining a table surface. A tool, also formed of a thermally conductive material, has a base surface configured to engage the table surface of the table and a tooling surface opposite the base surface, wherein the tooling surface has a contoured shape that is non-planar. A heating blanket is provided above the table and defines a heating surface. The tooling surface of the tool is configured to engage a first surface of the part and the heating surface of the heating blanket is configured to engage a second surface of the part opposite the first surface of the part. The table and the heating blanket are heated to a processing temperature so that the part at least partially conforms to the tooling surface of the tool.
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6.
公开(公告)号:US20200164548A1
公开(公告)日:2020-05-28
申请号:US16201612
申请日:2018-11-27
Applicant: The Boeing Company
Inventor: Bret A. Voss , Marc R. Matsen , Jeffrey H. Olberg , James R. Jones
Abstract: Heating apparatus and methods for thermally processing a part including improved control of temperature. A thermal management system is coupled to a back surface of a table thermally coupled to an inductive heating circuit. The thermal management system includes a chamber defining an interior space, at least one cooling fin disposed within the chamber, an inlet extending through the chamber and fluidly communicating with the interior space, and an outlet extending through the chamber and fluidly communicating with the interior space. In some applications, an air source fluidly communicates with the inlet and is selectively operable to generate an air flow through the chamber, so that the thermal management system may be selectively operated in an insulator mode and a cooling mode.
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公开(公告)号:US20160332501A1
公开(公告)日:2016-11-17
申请号:US14448305
申请日:2014-07-31
Applicant: The Boeing Company
Inventor: John Ralph Hull , Michael Strasik , Bret A. Voss , Mark A. Negley , William J. Sweet , Kevin R. Housen , Jason S. Damazo , Michael D. Gonzales , Michael Howard-Edward Ware , Lee Charles Firth
CPC classification number: B60H1/00564 , B32B1/08 , B32B3/266 , B32B5/024 , B32B2262/101 , B32B2307/304 , B32B2307/558 , B32B2605/18 , F16L55/07 , F16L55/17 , F16L57/02 , F16L57/04 , F16L59/145 , F17D5/02
Abstract: Methods and systems for duct protection of a vehicle are provided. The methods and systems provided include an apparatus for containing a flow of fluid discharged from a fracture in a duct. The apparatus includes a ballistic containment layer and an insulation sheath coupled to the ballistic containment layer. The insulation sheath includes a first air containment layer, an insulation layer, and a second air containment layer.
Abstract translation: 提供了用于车辆的风道保护的方法和系统。 提供的方法和系统包括用于容纳从管道中的裂缝排出的流体流的装置。 该装置包括弹道防护层和耦合到弹道防护层的绝缘护套。 绝缘护套包括第一空气容纳层,绝缘层和第二空气容纳层。
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公开(公告)号:US11284482B2
公开(公告)日:2022-03-22
申请号:US16123944
申请日:2018-09-06
Applicant: The Boeing Company
Inventor: Bret A. Voss , Marc R. Matsen
Abstract: A heating blanket includes an interlaced heating layer having a fabric thread and a heat-generating thread interlaced with the fabric thread to form the interlaced heating layer. The heat-generating thread includes a conductor wire configured to generate a magnetic field in response to an electrical current applied to the conductor wire, and a susceptor wire formed of a susceptor material configured to inductively generate heat in response to the magnetic field of the conductor wire when a temperature of the susceptor wire is below a Curie point of the susceptor wire. Methods of forming the heating blanket and methods of heating a contoured surface using the heating blanket are also disclosed.
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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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公开(公告)号:US20200084841A1
公开(公告)日:2020-03-12
申请号:US16123944
申请日:2018-09-06
Applicant: The Boeing Company
Inventor: Bret A. Voss , Marc R. Matsen
IPC: H05B6/10
Abstract: A heating blanket includes an interlaced heating layer having a fabric thread and a heat-generating thread interlaced with the fabric thread to form the interlaced heating layer. The heat-generating thread includes a conductor wire configured to generate a magnetic field in response to an electrical current applied to the conductor wire, and a susceptor wire formed of a susceptor material configured to inductively generate heat in response to the magnetic field of the conductor wire when a temperature of the susceptor wire is below a Curie point of the susceptor wire. Methods of forming the heating blanket and methods of heating a contoured surface using the heating blanket are also disclosed.
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