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公开(公告)号：US09277594B2
公开(公告)日：2016-03-01
申请号：US13770235
申请日：2013-02-19
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Robert James Miller , Brian W. Smith , Geoffrey Allen Butler , Karl Marius Nelson
CPC classification number: H05B1/00 , B29C35/0227 , B29C35/0805 , B29C2035/0811 , B29C2035/0816
Abstract: The thermal cycle time for curing a thermoset composite part in an autoclave is reduced by placing a heating blanket in proximity to an area of the composite part that is slow-to-heat, and inductively heating the area of the composite part that is slow-to-heat using the heating blanket.
Abstract translation: 通过在加热缓慢的复合部件的区域附近放置加热毯来减少在高压釜中固化热固性复合部件的热循环时间，并感应加热复合部件的慢速加热区域， 使用加热毯进行加热。
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Patent Agency Ranking
公开(公告)号：US20140353305A1
公开(公告)日：2014-12-04
申请号：US13909491
申请日：2013-06-04
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Brian W. Smith , Robert James Miller
IPC: H05B6/10
CPC classification number: H05B6/108 , B29C35/0805 , B29C37/0075 , B29C65/362 , B29C65/4835 , B29C65/76 , B29C65/7826 , B29C66/112 , B29C66/131 , B29C66/301 , B29C66/524 , B29C66/543 , B29C66/721 , B29C66/7212 , B29C2035/0811 , B29L2011/0075 , B29L2031/3085 , B64C3/26 , B64C2001/0072 , B64F5/10 , H05B2206/023 , Y02T50/43 , B29K2307/04
Abstract: A method for forming a shim. A liquid shim material with a magnetically permeable material is applied in a location for the shim between a plurality of composite parts. A magnetic field is applied to the magnetically permeable material in the location. The magnetic field is configured to heat the liquid shim material to a temperature to cause the liquid shim material to become solid and form the shim.
Abstract translation: 一种形成垫片的方法。 将具有导磁材料的液体垫片材料施加在用于多个复合部件之间的垫片的位置。 在该位置将磁场施加到导磁材料上。 磁场被配置为将液体垫片材料加热到使液体垫片材料变得固体并形成垫片的温度。
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公开(公告)号：US09674899B2
公开(公告)日：2017-06-06
申请号：US13909491
申请日：2013-06-04
Applicant: The Boeing Company
Inventor： Marc Rollo Matsen , Brian W. Smith , Robert James Miller
IPC: H05B6/10 , B29C35/08 , B64C3/26 , B64F5/00 , B29C65/36 , B29C65/48 , B29C65/76 , B29C65/78 , B29C65/00 , B29L31/30 , B29L11/00 , B29C37/00 , B64C1/00
CPC classification number: H05B6/108 , B29C35/0805 , B29C37/0075 , B29C65/362 , B29C65/4835 , B29C65/76 , B29C65/7826 , B29C66/112 , B29C66/131 , B29C66/301 , B29C66/524 , B29C66/543 , B29C66/721 , B29C66/7212 , B29C2035/0811 , B29L2011/0075 , B29L2031/3085 , B64C3/26 , B64C2001/0072 , B64F5/10 , H05B2206/023 , Y02T50/43 , B29K2307/04
Abstract: A method for forming a shim. A liquid shim material with a magnetically permeable material is applied in a location for the shim between a plurality of composite parts. A magnetic field is applied to the magnetically permeable material in the location. The magnetic field is configured to heat the liquid shim material to a temperature to cause the liquid shim material to become solid and form the shim.
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公开(公告)号：US20140231402A1
公开(公告)日：2014-08-21
申请号：US13770235
申请日：2013-02-19
Applicant: THE BOEING COMPANY
Inventor： Marc Rollo Matsen , Robert James Miller , Brian W. Smith , Geoffrey Allen Butler , Karl Marius Nelson
IPC: H05B1/00
CPC classification number: H05B1/00 , B29C35/0227 , B29C35/0805 , B29C2035/0811 , B29C2035/0816
Abstract: The thermal cycle time for curing a thermoset composite part in an autoclave is reduced by placing a heating blanket in proximity to an area of the composite part that is slow-to-heat, and inductively heating the area of the composite part that is slow-to-heat using the heating blanket.
Abstract translation: 通过在加热缓慢的复合部件的区域附近放置加热毯来减少在高压釜中固化热固性复合部件的热循环时间，并感应加热复合部件的慢速加热区域， 使用加热毯进行加热。
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5.发明授权公开(公告)号：US10369679B2
公开(公告)日：2019-08-06
申请号：US15347485
申请日：2016-11-09
Applicant: The Boeing Company
Inventor： Bennett M. Moriarty , Phillip J. Crothers , Shane E. Arthur , Brian W. Smith
Abstract: A finishing apparatus for performing an automated finishing operation on a surface of a workpiece is disclosed. The finishing apparatus may include a platen fabricated from a magnetic material and having a platen surface, and a finishing module disposed on the platen surface and having a finishing operation end effector. The finishing module may generate a magnetic field that biases the finishing module toward the platen, and may be operable to generate a magnetic flux to control movement of the finishing module over the platen surface to perform the automated finishing operation on the surface of the workpiece.
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6.发明申请公开(公告)号：US20180126514A1
公开(公告)日：2018-05-10
申请号：US15347485
申请日：2016-11-09
Applicant: The Boeing Company
Inventor： Bennett M. Moriarty , Phillip J. Crothers , Shane E. Arthur , Brian W. Smith
CPC classification number: B24B51/00 , B05B13/005 , B05B13/0431 , B05B13/0436 , B24B19/26 , B25J5/00 , B64F5/10
Abstract: A finishing apparatus for performing an automated finishing operation on a surface of a workpiece is disclosed. The finishing apparatus may include a platen fabricated from a magnetic material and having a platen surface, and a finishing module disposed on the platen surface and having a finishing operation end effector. The finishing module may generate a magnetic field that biases the finishing module toward the platen, and may be operable to generate a magnetic flux to control movement of the finishing module over the platen surface to perform the automated finishing operation on the surface of the workpiece.
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