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公开(公告)号：US10016820B2
公开(公告)日：2018-07-10
申请号：US15019930
申请日：2016-02-09
申请人： The Boeing Company
CPC分类号： B23B49/02 , B23B51/06 , B23B2215/04 , B23B2250/12 , B23B2260/126 , B23Q11/0075 , Y02P70/171 , Y10T408/455 , Y10T408/569
摘要： Drill plate assemblies are disclosed in the examples herein. An example method includes positioning an absorbent material between a drill plate and a surface to be drilled; performing a drilling operation on the surface including flowing coolant through the drill; and capturing at least some of coolant in the absorbent material.
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公开(公告)号：US20180208328A1
公开(公告)日：2018-07-26
申请号：US15415172
申请日：2017-01-25
申请人： The Boeing Company
CPC分类号： B64F5/10 , B23B35/00 , B23B49/00 , B23B2215/04 , B23P21/00 , B23P2700/01 , B64C1/065 , B64C1/10
摘要： A method includes making a first structure with a first plurality of pre-drilled holes at pre-defined locations, making a second structure with a second plurality of pre-drilled holes at pre-defined locations, making a third structure without pre-drilled full-size holes, measuring the location and orientation of the first and second plurality of pre-drilled holes in the first and second structures, determining the location of a third plurality of holes to be drilled in the third structure that correspond to first and second plurality of pre-drilled holes measured in the first and second structures, creating a program to drill the third plurality of holes in the third structure that align with the measured location and orientation of the first and second plurality of pre-drilled holes in the first and second structures based on the measure location and orientation of the first and second plurality of pre-drilled holes in the first and second structure, drilling the third plurality of holes in the third structure based on the program, positioning the third structure on the first and second structures such that the third plurality of holes in the third structure are aligned with the first and second plurality of pre-drilled holes in the first and second structures, and inserting fasteners through the third plurality of holes and the first and second plurality of predrilled holes that are aligned with the third plurality of holes to secure the second structure to the first structure using the third structure.
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公开(公告)号：US20180153308A1
公开(公告)日：2018-06-07
申请号：US15372223
申请日：2016-12-07
申请人： The Boeing Company
CPC分类号： B32B3/26 , B32B5/024 , B32B2307/546 , B32B2437/00 , B32B2571/00
摘要： Ergonomic puncture-resistant pads are disclosed. An example disclosed herein includes a first layer configured to be adjacent a person and to conform to the person; a second layer coupled to the first layer, the second layer configured to resist puncture; and a third layer coupled to the second layer, the third layer including a flexible support structure extending away from the second layer, the third layer configured to support the person and to conform to a shape of a surface supporting the person, the flexible support structure configured to contact the surface, the flexible support structure including cavities to receive at least one object protruding from the surface to isolate the person from the at least one protruding object.
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公开(公告)号：US10934020B2
公开(公告)日：2021-03-02
申请号：US15415172
申请日：2017-01-25
申请人： The Boeing Company
摘要： A method includes making a first structure with a first plurality of pre-drilled holes at pre-defined locations, making a second structure with a second plurality of pre-drilled holes at pre-defined locations, making a third structure without pre-drilled full-size holes, measuring the location and orientation of the first and second plurality of pre-drilled holes in the first and second structures, determining the location of a third plurality of holes to be drilled in the third structure that correspond to first and second plurality of pre-drilled holes measured in the first and second structures, creating a program to drill the third plurality of holes in the third structure that align with the measured location and orientation of the first and second plurality of pre-drilled holes in the first and second structures based on the measure location and orientation of the first and second plurality of pre-drilled holes in the first and second structure, drilling the third plurality of holes in the third structure based on the program, positioning the third structure on the first and second structures such that the third plurality of holes in the third structure are aligned with the first and second plurality of pre-drilled holes in the first and second structures, and inserting fasteners through the third plurality of holes and the first and second plurality of predrilled holes that are aligned with the third plurality of holes to secure the second structure to the first structure using the third structure.
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5.发明申请公开(公告)号：US20180043440A1
公开(公告)日：2018-02-15
申请号：US15236469
申请日：2016-08-14
申请人： The Boeing Company
CPC分类号： B23B47/287 , B23B2215/04 , B23B2247/12 , B25H7/02
摘要： There is provided a tool assembly for transferring locations and dimensions of a pattern of holes from a first structure to a second structure. The tool assembly has a transfer plate with a transfer plate pattern of transfer plate holes that include a plurality of oversize holes and two transfer plate index holes. The transfer plate pattern is substantially identical to the pattern in the first structure. The tool assembly has one or more alignment elements installed in the plurality of oversize holes. Each alignment element has a through opening in a coaxial alignment with the oversize hole. The oversize hole allows formation of an alignment variation gap between an exterior of the alignment element and an inner wall of the oversize hole. The tool assembly has one or more holding elements coupled to the transfer plate, each with a central through opening in coaxial alignment with the oversize hole.
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6.发明授权公开(公告)号：US10207333B2
公开(公告)日：2019-02-19
申请号：US15236469
申请日：2016-08-14
申请人： The Boeing Company
摘要： There is provided a tool assembly for transferring locations and dimensions of a pattern of holes from a first structure to a second structure. The tool assembly has a transfer plate with a transfer plate pattern of transfer plate holes that include a plurality of oversize holes and two transfer plate index holes. The transfer plate pattern is substantially identical to the pattern in the first structure. The tool assembly has one or more alignment elements installed in the plurality of oversize holes. Each alignment element has a through opening in a coaxial alignment with the oversize hole. The oversize hole allows formation of an alignment variation gap between an exterior of the alignment element and an inner wall of the oversize hole. The tool assembly has one or more holding elements coupled to the transfer plate, each with a central through opening in coaxial alignment with the oversize hole.
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公开(公告)号：US20170225240A1
公开(公告)日：2017-08-10
申请号：US15019930
申请日：2016-02-09
申请人： The Boeing Company
CPC分类号： B23B49/02 , B23B51/06 , B23B2215/04 , B23B2250/12 , B23B2260/126 , B23Q11/0075 , Y02P70/171 , Y10T408/455 , Y10T408/569
摘要： Drill plate assemblies are disclosed in the examples herein. An example method includes positioning an absorbent material between a drill plate and a surface to be drilled; performing a drilling operation on the surface including flowing coolant through the drill; and capturing at least some of coolant in the absorbent material.
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公开(公告)号：US11370563B2
公开(公告)日：2022-06-28
申请号：US17149980
申请日：2021-01-15
申请人： The Boeing Company
摘要： A method includes making a first structure with a first plurality of pre-drilled holes at pre-defined locations, making a second structure with a second plurality of pre-drilled holes at pre-defined locations, making a third structure without pre-drilled full-size holes, measuring the location and orientation of the first and second plurality of pre-drilled holes in the first and second structures, determining the location of a third plurality of holes to be drilled in the third structure that correspond to first and second plurality of pre-drilled holes measured in the first and second structures, creating a program to drill the third plurality of holes in the third structure that align with the measured location and orientation of the first and second plurality of pre-drilled holes in the first and second structures based on the measure location and orientation of the first and second plurality of pre-drilled holes in the first and second structure, drilling the third plurality of holes in the third structure based on the program, positioning the third structure on the first and second structures such that the third plurality of holes in the third structure are aligned with the first and second plurality of pre-drilled holes in the first and second structures, and inserting fasteners through the third plurality of holes and the first and second plurality of predrilled holes that are aligned with the third plurality of holes to secure the second structure to the first structure using the third structure.
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公开(公告)号：US20210130010A1
公开(公告)日：2021-05-06
申请号：US17149980
申请日：2021-01-15
申请人： The Boeing Company
摘要： A method includes making a first structure with a first plurality of pre-drilled holes at pre-defined locations, making a second structure with a second plurality of pre-drilled holes at pre-defined locations, making a third structure without pre-drilled full-size holes, measuring the location and orientation of the first and second plurality of pre-drilled holes in the first and second structures, determining the location of a third plurality of holes to be drilled in the third structure that correspond to first and second plurality of pre-drilled holes measured in the first and second structures, creating a program to drill the third plurality of holes in the third structure that align with the measured location and orientation of the first and second plurality of pre-drilled holes in the first and second structures based on the measure location and orientation of the first and second plurality of pre-drilled holes in the first and second structure, drilling the third plurality of holes in the third structure based on the program, positioning the third structure on the first and second structures such that the third plurality of holes in the third structure are aligned with the first and second plurality of pre-drilled holes in the first and second structures, and inserting fasteners through the third plurality of holes and the first and second plurality of predrilled holes that are aligned with the third plurality of holes to secure the second structure to the first structure using the third structure.
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公开(公告)号：US10427376B2
公开(公告)日：2019-10-01
申请号：US15372223
申请日：2016-12-07
申请人： The Boeing Company
摘要： Ergonomic puncture-resistant pads are disclosed. An example disclosed herein includes a first layer configured to be adjacent a person and to conform to the person; a second layer coupled to the first layer, the second layer configured to resist puncture; and a third layer coupled to the second layer, the third layer including a flexible support structure extending away from the second layer, the third layer configured to support the person and to conform to a shape of a surface supporting the person, the flexible support structure configured to contact the surface, the flexible support structure including cavities to receive at least one object protruding from the surface to isolate the person from the at least one protruding object.
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