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公开(公告)号:US20190389099A1
公开(公告)日:2019-12-26
申请号:US16563093
申请日:2019-09-06
Applicant: The Boeing Company
Inventor: Marc R. Matsen , David S. Nansen , Lee C. Firth , Carey E. Wilkinson , Gregory J. Hickman , William C. Dykstra
IPC: B29C43/52
Abstract: Provided are induction heating cells including pressure bladders used for supporting dies and methods of using these induction heating cells. A pressure bladder may be disposed between a die and a bolster of the cell. Even when the bolster is deformed during operation of the cell, the pressure bladder continues to provide uniform support to the die thereby preserving integrity of the die and prevents its cracking or braking. As such, the cell may be operated at a higher processing pressure inside the cavity formed by the die without further strengthening the bolster. The bolster is allowed to deform without compromising the integrity of the die. The deformation of the bolster is compensated by the shape change of the pressure bladder. The number and/or position of the bladders in the cell may depend on the shape of processed parts.
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公开(公告)号:US20190239292A1
公开(公告)日:2019-08-01
申请号:US15884976
申请日:2018-01-31
Applicant: The Boeing Company
Inventor: Landon K. Henson , Marc R. Matsen , John R. Hull , Lee C. Firth , Tunde A. Olaniyan
Abstract: A smart susceptor assembly including an electromagnetic flux source such as one or more inductors, a geometrically complex-shaped susceptor having one or more contours, and a cladding on or over the susceptor. The cladding can alter both the thermal performance and the electrical operation of the smart susceptor assembly. With regard to thermal performance, the cladding can function as a passive heat exchanger to dissipate thermal energy across the surface of the susceptor. With regard to electrical operation, the cladding can provide a current path after portions of the susceptor heat and become low or non-magnetic.
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93.
公开(公告)号:US20190191495A1
公开(公告)日:2019-06-20
申请号:US15841964
申请日:2017-12-14
Applicant: The Boeing Company
Inventor: Marc R. Matsen , Lee C. Firth , Mark A. Negley
Abstract: Disclosed herein are induction heating cells and methods of using these cells for processing. An induction heating cell may be used for processing (e.g., consolidating and/or curing a composite layup having a non-planar portion. The induction heating cell comprises a caul, configured to position over and conform to this non-planar portion. Furthermore, the cell comprises a mandrel, configured to position over the caul and force the caul again the surface of the feature. The CTE of the caul may be closer to the CTE of the composite layup than to the CTE of the mandrel. As such, the caul isolates the composite layup from the dimensional changes of the mandrel, driven by temperature fluctuations. At the same time, the caul may conform to the surface of the mandrel, which can be used to define the shape and transfer pressure to the non-planar portion.
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公开(公告)号:US10219329B2
公开(公告)日:2019-02-26
申请号:US14530826
申请日:2014-11-02
Applicant: The Boeing Company
Inventor: Marc R. Matsen , Mark A. Negley
IPC: H05B6/04 , F27D3/00 , C21D9/54 , H05B6/44 , B29C35/02 , B29C35/08 , F03D1/06 , B29C33/06 , B29C35/00 , H05B6/40 , B29C65/18 , B29C65/32 , B29C65/36 , B29C65/00 , B29K71/00 , B29K101/12 , B29K105/06 , B29K305/00 , B29K307/00 , B29K307/02 , B29L31/08 , B29L31/00
Abstract: A method of fabricating a thermoplastic component using inductive heating is described. The method includes positioning a plurality of induction heating coils to define a process area for the thermoplastic component, wherein the plurality of induction heating coils comprises a first set of coils and a second set of coils. The method also includes controlling a supply of electricity provided to the plurality of inductive heating coils to intermittently activate the coils. The intermittent activation is configured to facilitate prevention of electromagnetic interference between adjacent coils.
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公开(公告)号:US20180290402A1
公开(公告)日:2018-10-11
申请号:US16008660
申请日:2018-06-14
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 , B29C65/16 , 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 , B29C66/87 , 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.
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公开(公告)号:US20180244016A1
公开(公告)日:2018-08-30
申请号:US15443235
申请日:2017-02-27
Applicant: The Boeing Company
Inventor: Marc R. Matsen , Lee C. Firth , David S. Nansen , Michael R. Zolnowski , Carey E. Wilkinson , Gregory A. Foltz
Abstract: A panel comprises a first face sheet and a second face sheet spaced apart from the first face sheet. The panel further comprises a core sheet intercoupled between the first face sheet and the second face sheet. Each of the first and second face sheets is made of a material having a thermal expansion that is different from the thermal expansion of the other face sheet.
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公开(公告)号:US20180229463A1
公开(公告)日:2018-08-16
申请号:US15431413
申请日:2017-02-13
Applicant: The Boeing Company
Inventor: John R. Hull , Marc R. Matsen
Abstract: A method includes a first electrode exhibiting a first Seebeck coefficient, a second electrode exhibiting a second Seebeck coefficient greater than the first Seebeck coefficient, and particles between the first and second electrodes exhibiting a third Seebeck coefficient between the first and second Seebeck coefficients. Heat is generated due to the Peltier effect at a junction between the first electrode and the particles and at a junction between the second electrode and the particles. Heat is removed due to the Peltier effect at the junction between the first electrode and the particles and at the junction between the second electrode and the particles. The particles are densified due to heating and cooling phase transitions between a higher-temperature solid phase and a lower-temperature solid phase while compressing the particles. An apparatus includes the first and second electrodes and an alternating current power supply electrically connected to the first and second electrodes.
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公开(公告)号:US10016947B2
公开(公告)日:2018-07-10
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
IPC: B29C70/38 , B29C65/16 , B29C65/00 , B29C65/32 , B29K101/12
CPC classification number: B29C70/382 , B29C65/02 , B29C65/08 , B29C65/1416 , B29C65/1419 , B29C65/1432 , B29C65/16 , 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 , B29C66/87 , 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.
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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:US20180080495A1
公开(公告)日:2018-03-22
申请号:US15268983
申请日:2016-09-19
Applicant: The Boeing Company
Inventor: William J. Koch , Marc R. Matsen
Abstract: A shim assembly includes a shim material configured to be positioned between a first component and a second component. A wire is in contact with the shim material. The wire is configured to heat the shim material to above a predetermined temperature, and the shim material becomes moldable above the predetermined temperature such that the shim material is able to conform to the first component and the second component.
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