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公开(公告)号：US11117307B2
公开(公告)日：2021-09-14
申请号：US16255724
申请日：2019-01-23
Applicant: The Boeing Company
Inventor： Weidong Song , Daniel J. Perron , Stephen G. Moore , Jamie J. Langabeer , Jonathan D. Robbins , Jeffrey Olberg
IPC: B29C48/155 , B29C48/25 , B29C48/385 , B29C48/92 , B64C1/06 , B29D99/00 , B29C48/02 , B29L31/30 , B29K105/16 , B29K105/12 , B29C65/00 , B29C65/02 , B64C1/00 , B29C48/05 , B29C48/06 , B29C48/00 , B29C48/14 , B29C48/285 , B29C48/76 , B29C48/793 , B29C48/80
Abstract: A system for depositing a composite filler material into a channel of a composite structure includes an end-effector configured to extrude a bead of the filler material into the channel. The filler material can comprise a first group of relatively long fibers, a second group of relatively short fibers and a resin. A drive system is configured to move the end-effector relative to the channel, and a position sensor is configured to detect the position of the bead relative to the channel. A controller is configured to operate the drive system in response to the detected position and to operate the end-effector to heat and compress the filler material so as to orient the longer fibers in a substantially longitudinal direction relative to the channel and the shorter fibers in substantially random directions relative to the channel when the bead is extruded into the channel.
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公开(公告)号：US20200215790A1
公开(公告)日：2020-07-09
申请号：US16819592
申请日：2020-03-16
Applicant: The Boeing Company
Inventor： Stephen G. Moore , Alexandra K. Dillon , Alan G. Burg , Megan M. Petersen
Abstract: A fiber placement system including a compaction roller rotatable about an axis of rotation, the compaction roller including a reflective layer that includes a reflective material dispersed in a polymeric material, and a light source positioned to project a beam of electromagnetic radiation proximate the compaction roller, the beam having a wavelength, wherein the reflective material has a reflectance of at least 80 percent at the wavelength.
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公开(公告)号：US20180290388A1
公开(公告)日：2018-10-11
申请号：US16002536
申请日：2018-06-07
Applicant: The Boeing Company
Inventor： Stephen G. Moore , Alexandra K. Dillon
IPC: B29C65/14 , B29C65/00 , B29C70/38 , G02B13/22 , G02B26/10 , B29K101/12 , B29L9/00 , B29K105/08
CPC classification number: B29C65/1412 , B29C66/8362 , B29C66/952 , B29C70/386 , B29K2101/12 , B29K2105/0872 , B29L2009/00 , G02B13/22 , G02B26/101 , G02B26/105
Abstract: A fiber placement system including a compaction roller rotatable about an axis of rotation, the compaction roller at least partially defining a compaction nip region, and a laser heating assembly including a laser that emits a beam of electromagnetic radiation and a scan head defining a scan field, the scan field being aligned with the compaction nip region, wherein the scan head scans the beam within the scan field.
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公开(公告)号：US10071429B2
公开(公告)日：2018-09-11
申请号：US15710410
申请日：2017-09-20
Applicant: The Boeing Company
Inventor： Noel A. Spishak , Charles M. Richards , Jeffrey M. Hansen , Stephen G. Moore , Dan D. Day
IPC: B23B39/14 , B25J5/00 , B60B19/00 , G05D1/02 , G05B19/18 , G05D1/00 , B23Q9/00 , B23B35/00 , B23B49/00 , B23B41/00
Abstract: A magnet sensing portable autonomous device includes a platform. A plurality of wheel sets is coupled to the platform. A drive system is used for driving the plurality of wheels. An attachment mechanism is positioned on an underside of the platform for securing the device to a surface. A control board is used for controlling the operation of the device. In some embodiments, a drill spindle assembly is coupled to the platform. A drill feed assembly is coupled to the drill spindle assembly for raising and lowering the drill spindle assembly. A plurality of sensors are operable to sense one or more magnets disposed below the surface. A drive table is used for positioning the drill spindle assembly in an XY plane based on an output of said plurality of sensors.
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公开(公告)号：US10016932B2
公开(公告)日：2018-07-10
申请号：US14711133
申请日：2015-05-13
Applicant: The Boeing Company
Inventor： Stephen G. Moore , Alexandra K. Dillon
IPC: B29C65/14 , G02B26/10 , G02B13/22 , B29C65/00 , B29C70/38 , B29K101/12 , B29K105/08 , B29L9/00
CPC classification number: B29C65/1412 , B29C66/8362 , B29C66/952 , B29C70/386 , B29K2101/12 , B29K2105/0872 , B29L2009/00 , G02B13/22 , G02B26/101 , G02B26/105
Abstract: A fiber placement system including a compaction roller rotatable about an axis of rotation, the compaction roller at least partially defining a compaction nip region, and a laser heating assembly including a laser that emits a beam of electromagnetic radiation and a scan head defining a scan field, the scan field being aligned with the compaction nip region, wherein the scan head scans the beam within the scan field.
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Patent Agency Ranking
公开(公告)号：US09862175B2
公开(公告)日：2018-01-09
申请号：US14795209
申请日：2015-07-09
Applicant: The Boeing Company
Inventor： Marc R. Matsen , Mark A. Negley , Marc J. Piehl , Kay Y. Blohowiak , Alan E. Landmann , Richard H. Bossi , Robert L. Carlsen , Gregory Alan Foltz , Geoffrey A. Butler , Liam S. Cavanaugh Pingree , Stephen G. Moore , John Mark Gardner , Robert A. Anderson
IPC: B32B37/00 , B32B37/14 , B32B7/12 , B32B15/00 , B32B15/08 , B32B19/02 , B32B27/00 , B32B3/06 , B29C73/10
CPC classification number: B32B37/144 , B29C73/10 , B32B3/06 , B32B7/12 , B32B15/00 , B32B15/08 , B32B19/02 , B32B27/00 , B32B2250/42 , B32B2260/021 , B32B2305/08 , B32B2307/202 , B32B2307/204 , B32B2307/54 , B32B2307/558 , B32B2311/00 , B32B2398/00 , B32B2405/00 , B32B2605/18 , Y10T29/49208 , Y10T29/49885 , Y10T156/10 , Y10T428/24752 , Y10T428/31678
Abstract: A method of forming a molybdenum composite hybrid laminate is disclosed. The method includes treating a surface of each of a plurality of molybdenum foil layers. The method further includes interweaving the surface treated molybdenum foil layers with a plurality of composite material layers. The method further includes bonding with an adhesive layer each of the surface treated molybdenum foil layers to adjacent composite material layers to form a molybdenum composite hybrid laminate having improved yield strength.
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公开(公告)号：US09782836B2
公开(公告)日：2017-10-10
申请号：US15167706
申请日：2016-05-27
Applicant: The Boeing Company
Inventor： Noel A. Spishak , Charles M. Richards , Jeff Hansen , Stephen G. Moore , Dan D. Day
IPC: B23B39/14 , B23Q9/00 , B23B35/00 , B25J5/00 , B60B19/00 , G05D1/02 , G05B19/18 , G05D1/00 , B23B41/00 , B23B49/00
CPC classification number: B23B39/14 , B23B35/00 , B23B41/00 , B23B49/00 , B23B2215/04 , B23B2260/018 , B23B2260/10 , B23B2260/128 , B23Q9/0007 , B25J5/007 , B60B19/003 , B60Y2200/60 , B60Y2200/80 , G05B19/182 , G05B2219/33099 , G05B2219/45129 , G05D1/0088 , G05D1/0261 , Y10T29/53983 , Y10T408/03 , Y10T408/554 , Y10T408/556 , Y10T408/5612
Abstract: A portable device to drill holes has a platform. A plurality of wheel sets is coupled to the platform. A drive system is used for driving the plurality of wheels. An attachment mechanism is positioned on an underside of the platform for securing the device to a surface. A control board is used for controlling the operation of the device. A drill spindle assembly is coupled to the platform. A drill feed assembly is coupled to the drill spindle assembly for raising and lowering the drill spindle assembly. A plurality of sensors are operable to sense one or more magnets disposed below the surface. A drive table is used for positioning the drill spindle assembly in an XY plane based on an output of said plurality of sensors.
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公开(公告)号：US20170028606A1
公开(公告)日：2017-02-02
申请号：US14812223
申请日：2015-07-29
Applicant: The Boeing Company
Inventor： Weidong Song , Daniel J. Perron , Stephen G. Moore , Jamie J. Langabeer , Jonathan D. Robbins , Jeffrey Olberg
CPC classification number: B29C47/92 , B29C47/0002 , B29C47/0014 , B29C47/0016 , B29C47/0064 , B29C47/0083 , B29C47/026 , B29C47/0866 , B29C47/1045 , B29C47/366 , B29C47/767 , B29C47/786 , B29C47/822 , B29C65/02 , B29C66/112 , B29C66/1122 , B29C66/131 , B29C66/43441 , B29C66/474 , B29C66/496 , B29C66/524 , B29C66/5326 , B29C66/54 , B29C66/636 , B29C66/721 , B29C66/73754 , B29C2791/006 , B29C2947/92076 , B29C2947/92104 , B29C2947/92114 , B29C2947/92209 , B29C2947/92514 , B29C2947/92571 , B29C2947/926 , B29C2947/92609 , B29C2947/92704 , B29C2947/92904 , B29D99/0003 , B29K2105/12 , B29K2105/16 , B29K2105/165 , B29L2031/3076 , B29L2031/3082 , B29L2031/3085 , B64C1/064 , B64C2001/0072 , Y02T50/43
Abstract: A system for depositing a composite filler material into a channel of a composite structure includes an end-effector configured to extrude a bead of the filler material into the channel. The filler material can comprise a first group of relatively long fibers, a second group of relatively short fibers and a resin. A drive system is configured to move the end-effector relative to the channel, and a position sensor is configured to detect the position of the bead relative to the channel. A controller is configured to operate the drive system in response to the detected position and to operate the end-effector to heat and compress the filler material so as to orient the longer fibers in a substantially longitudinal direction relative to the channel and the shorter fibers in substantially random directions relative to the channel when the bead is extruded into the channel.
Abstract translation: 用于将复合填料材料沉积到复合结构的通道中的系统包括构造成将填料材料的珠挤出到通道中的末端执行器。 填充材料可以包括第一组相对长的纤维，第二组相对短的纤维和树脂。 驱动系统被配置为相对于通道移动末端执行器，并且位置传感器被配置为检测胎圈相对于通道的位置。 控制器被配置为响应于检测到的位置来操作驱动系统，并且操作末端执行器以加热和压缩填充材料，以便使长纤维在相对于通道和较短纤维的基本纵向方向上定向 当胎圈被挤压到通道中时相对于通道的基本随机的方向。
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公开(公告)号：US20150306859A1
公开(公告)日：2015-10-29
申请号：US14795209
申请日：2015-07-09
Applicant: The Boeing Company
Inventor： Marc R. Matsen , Mark A. Negley , Marc J. Piehl , Kay Y. Blohowiak , Alan E. Landmann , Richard H. Bossi , Robert L. Carlsen , Gregory Alan Foltz , Geoffrey A. Butler , Liam S. Cavanaugh Pingree , Stephen G. Moore , John Mark Gardner , Robert A. Anderson
CPC classification number: B32B37/144 , B29C73/10 , B32B3/06 , B32B7/12 , B32B15/00 , B32B15/08 , B32B19/02 , B32B27/00 , B32B2250/42 , B32B2260/021 , B32B2305/08 , B32B2307/202 , B32B2307/204 , B32B2307/54 , B32B2307/558 , B32B2311/00 , B32B2398/00 , B32B2405/00 , B32B2605/18 , Y10T29/49208 , Y10T29/49885 , Y10T156/10 , Y10T428/24752 , Y10T428/31678
Abstract: A method of forming a molybdenum composite hybrid laminate is disclosed. The method includes treating a surface of each of a plurality of molybdenum foil layers. The method further includes interweaving the surface treated molybdenum foil layers with a plurality of composite material layers. The method further includes bonding with an adhesive layer each of the surface treated molybdenum foil layers to adjacent composite material layers to form a molybdenum composite hybrid laminate having improved yield strength.
Abstract translation: 公开了一种形成钼复合混合层压板的方法。 该方法包括处理多个钼箔层中的每一个的表面。 该方法还包括用多个复合材料层交织经表面处理的钼箔层。 该方法还包括将每个表面处理的钼箔层的粘合剂层粘合到相邻的复合材料层，以形成具有改进的屈服强度的钼复合混合层合物。
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公开(公告)号：US11066838B2
公开(公告)日：2021-07-20
申请号：US16033438
申请日：2018-07-12
Applicant: The Boeing Company
Inventor： Charles M. Richards , James J. Troy , Stephen G. Moore , Kurt F. Webster
Abstract: A mover system that moves a work platform relative to a target object. The mover system includes a drive vehicle configured to be attached to the work platform. Sensors are attached to the work platform that detect a distance between the sensors and the target object. Signals from the sensors are used to determine an alignment angle used for the operation of the drive vehicle to move the work platform into alignment and spacing relative to the work object.
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