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公开(公告)号：US20150027629A1
公开(公告)日：2015-01-29
申请号：US13953456
申请日：2013-07-29
Applicant: The Boeing Company
Inventor： Geoffrey Allen Butler , Justin Honshune Lan , Noel T. Gerken , Garry M. Duschl , Benjamin Julius Day
IPC: B32B1/06
CPC classification number: B32B37/146 , B29D99/0021 , B29L2031/7504 , B32B3/12 , B32B3/266 , B32B7/12 , B32B15/02 , B32B27/06 , B32B37/12 , B32B2605/00 , B32B2605/18 , B64D2033/0206 , F02C7/045 , F02K1/827 , F05D2220/323 , F05D2230/23 , F05D2250/283 , F05D2260/963 , G10K11/168 , G10K11/172 , Y02T50/672
Abstract: An acoustic liner having a honeycomb core is fabricated by forming septa in a sheet of material, and assembling the sheet of material and the core. During the assembly process, the septa are respectively inserted as a group into cells of the core.
Abstract translation: 具有蜂窝芯的声学衬垫通过在一片材料中形成隔片并组装材料片和芯来制造。 在组装过程中，将隔片分别插入到芯的单元中。
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公开(公告)号：US10927543B2
公开(公告)日：2021-02-23
申请号：US15626173
申请日：2017-06-19
Applicant: The Boeing Company
Inventor： Geoffrey Allen Butler , Justin Honshune Lan
IPC: E04B1/00 , B32B3/00 , B32B27/00 , F02C7/00 , G10K11/00 , E04B1/84 , B32B3/12 , B32B27/28 , F02C7/045 , G10K11/172 , G10K11/168
Abstract: An acoustic attenuation structure comprises a gas permeable composite facesheet, a cellular core, and an impermeable backing. The gas permeable composite facesheet has a designated porosity. The designated porosity causes the permeability of the gas permeable composite facesheet. The gas permeable composite facesheet comprises a carbon fiber fabric. The cellular core is bonded to the gas permeable composite facesheet using a resin of the gas permeable composite facesheet without any additional adhesive. The impermeable backing is connected to the cellular core.
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公开(公告)号：US20190003177A1
公开(公告)日：2019-01-03
申请号：US15626173
申请日：2017-06-19
Applicant: The Boeing Company
Inventor： Geoffrey Allen Butler , Justin Honshune Lan
Abstract: An acoustic attenuation structure comprises a gas permeable composite facesheet, a cellular core, and an impermeable backing. The gas permeable composite facesheet has a designated porosity. The designated porosity causes the permeability of the gas permeable composite facesheet. The gas permeable composite facesheet comprises a carbon fiber fabric. The cellular core is bonded to the gas permeable composite facesheet using a resin of the gas permeable composite facesheet without any additional adhesive. The impermeable backing is connected to the cellular core.
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公开(公告)号：US20190030839A1
公开(公告)日：2019-01-31
申请号：US15662969
申请日：2017-07-28
Applicant: The Boeing Company
Inventor： Max U. Kismarton , Karl Marius Nelson , Geoffrey Allen Butler
CPC classification number: B29C70/54 , B29C70/30 , B29C70/345 , B29D99/001 , B29L2031/3085
Abstract: A method and an apparatus are presented. The method locally compensates for cure related deformations in a composite skin by laying up a composite material on a compensation surface of a slip sheet designed to form a modified outer mold line different from a designed shape, wherein the slip sheet is held against a forming surface of a layup tool, wherein the forming surface is designed to form an outer mold line of the designed shape.
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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：US10828851B2
公开(公告)日：2020-11-10
申请号：US15662969
申请日：2017-07-28
Applicant: The Boeing Company
Inventor： Max U. Kismarton , Karl Marius Nelson , Geoffrey Allen Butler
Abstract: A method and an apparatus are presented. The method locally compensates for cure related deformations in a composite skin by laying up a composite material on a compensation surface of a slip sheet designed to form a modified outer mold line different from a designed shape, wherein the slip sheet is held against a forming surface of a layup tool, wherein the forming surface is designed to form an outer mold line of the designed shape.
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公开(公告)号：US09643392B2
公开(公告)日：2017-05-09
申请号：US13953456
申请日：2013-07-29
Applicant: The Boeing Company
Inventor： Geoffrey Allen Butler , Justin Honshune Lan , Noel T. Gerken , Garry M. Duschl , Benjamin Julius Day
IPC: B32B37/00 , B32B37/14 , B32B3/12 , F02C7/045 , G10K11/168 , F02K1/82 , B29D99/00 , G10K11/172 , B32B7/12 , B32B15/02 , B32B27/06 , B32B3/26 , B32B37/12 , B64D33/02 , B29L31/00
CPC classification number: B32B37/146 , B29D99/0021 , B29L2031/7504 , B32B3/12 , B32B3/266 , B32B7/12 , B32B15/02 , B32B27/06 , B32B37/12 , B32B2605/00 , B32B2605/18 , B64D2033/0206 , F02C7/045 , F02K1/827 , F05D2220/323 , F05D2230/23 , F05D2250/283 , F05D2260/963 , G10K11/168 , G10K11/172 , Y02T50/672
Abstract: An acoustic liner having a honeycomb core is fabricated by forming septa in a sheet of material, and assembling the sheet of material and the core. During the assembly process, the septa are respectively inserted as a group into cells of the core.
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8.发明申请Composite Laminates Having Hole Patterns Produced by Controlled Fiber Placement 审中-公开具有由受控纤维布置产生的孔型的复合层压板公开(公告)号：US20150030803A1
公开(公告)日：2015-01-29
申请号：US13953392
申请日：2013-07-29
Applicant: The Boeing Company
Inventor： Geoffrey Allen Butler , Brice A. Johnson , Jessica R. Hughes , Justin Honshune Lan
IPC: B32B3/12
CPC classification number: B32B5/024 , B29C70/224 , B29C70/386 , B32B3/02 , B32B3/266 , B32B5/022 , B32B5/12 , B32B5/26 , B32B2260/023 , B32B2260/046 , B32B2262/106 , B32B2305/024 , B32B2307/102 , B32B2605/00 , Y10T428/24074
Abstract: A composite laminate has a pattern of holes therein. The holes are formed by laying down plies of unidirectional pre-preg material having varying fiber orientations. The tows are spaced apart and located to form holes through the laminate.
Abstract translation: 复合层压板具有孔的图案。 孔通过铺设具有变化的纤维取向的单向预浸材料的层而形成。 丝束间隔开并定位成通过层压板形成孔。
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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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公开(公告)号：US10363726B2
公开(公告)日：2019-07-30
申请号：US15345708
申请日：2016-11-08
Applicant: The Boeing Company
Inventor： Geoffrey Allen Butler , Justin Honshune Lan , Noel T. Gerken , Garry M. Duschl , Benjamin Julius Day
IPC: B32B3/12 , B32B3/26 , F02K1/82 , B29D99/00 , B32B37/14 , F02C7/045 , B32B37/12 , G10K11/168 , G10K11/172 , B32B7/12 , B32B15/02 , B32B27/06 , B64D33/02 , B29L31/00
Abstract: An acoustic liner having a honeycomb core is fabricated by forming septa in a sheet of material, and assembling the sheet of material and the core. During the assembly process, the septa are respectively inserted as a group into cells of the core.
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