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公开(公告)号：US09931702B2
公开(公告)日：2018-04-03
申请号：US15254418
申请日：2016-09-01
申请人： The Boeing Company
IPC分类号： B23B49/02
CPC分类号： B23B49/02 , B23B49/023 , B23B2215/04 , B23B2247/12 , B23B2260/004 , B23B2260/068 , B23B2260/088 , B23B2260/124 , B23B2270/20
摘要： A drill bushing for a drill unit. In one embodiment, the drill bushing includes a base member having an upper surface, a lower surface configured to rest on a workpiece having a pilot hole, and a retaining member that projects from the lower surface of the base member. The retaining member has a cylindrical outer diameter that fits within the pilot hole. The drill bushing further includes a drill hole that passes from the upper surface of the base member through the retaining member to provide a passage for a drill bit. The drill bushing further includes an expandable slit that passes through the base member and the retaining member to the drill hole, and an adjustment member configured to expand the expandable slit to increase the cylindrical outer diameter of the retaining member within the pilot hole.
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公开(公告)号：US20180126524A1
公开(公告)日：2018-05-10
申请号：US15347609
申请日：2016-11-09
申请人： The Boeing Company
CPC分类号： B25B23/141 , B25B13/08 , B25B13/488 , B25B23/0085 , B25B23/1427
摘要： A tool (100) for rotating a first component (210) of an assembly (200) relative to a second component (220) of the assembly (200) is disclosed. The tool (100) comprises a ring support (130), a first wrench (110), coupled to the ring support (130), a worm ring (140), rotationally coupled to the ring support (130), a second wrench (120), coupled to the worm ring (140), and a worm screw (150), rotationally coupled to the ring support (130) and in mesh with the worm ring (°).
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公开(公告)号：US09895750B2
公开(公告)日：2018-02-20
申请号：US15214139
申请日：2016-07-19
申请人： The Boeing Company
CPC分类号： B23B49/026 , B23B47/28 , B23B47/287 , B23B2215/04 , B23B2247/04 , B23B2247/08 , B23B2247/12 , B23B2260/136 , B23B2270/12 , F16B13/00 , Y10T408/558 , Y10T408/563
摘要： A fastener for fastening a drill jig to overlapping work pieces and clamping the overlapping work pieces for facilitating accurate drilling of the overlapping work pieces including a fastener body and a damper assembly operatively connected to the fastener body. The damper assembly is configured to enable application of a first load to the drill jig, and the fastener body is configured to enable application of a second load to the overlapping work pieces when the fastener fastens the drill jig to the overlapping work pieces. The first load is less than the second load. The first load is sufficient to hold the drill jig to the overlapping work pieces during drilling but without causing significant deformation of the drill jig. The second load is sufficient to reduce the formation of burrs during drilling of a hole through the overlapping working pieces.
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公开(公告)号：US20200122243A1
公开(公告)日：2020-04-23
申请号：US16167349
申请日：2018-10-22
申请人： The Boeing Company
摘要： An orbital drill bushing adapter for use with a drill unit. In one embodiment, the orbital drill bushing adapter comprises a main body and locking arms. The main body includes a base member having an upper surface, a lower surface, and an external side wall that extends between the upper surface and the lower surface. The main body further includes a cylindrical spacer that projects from the lower surface of the base member, and is configured to fit in a drill hole of an orbital drill bushing. The main body includes a cylindrical hole that passes through the base member and the cylindrical spacer. The locking arms are pivotally coupled to the base member, and are configured to clamp the main body onto the orbital drill bushing.
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公开(公告)号：US20180056402A1
公开(公告)日：2018-03-01
申请号：US15254418
申请日：2016-09-01
申请人： The Boeing Company
IPC分类号： B23B49/02
CPC分类号： B23B49/02 , B23B49/023 , B23B2215/04 , B23B2247/12 , B23B2260/004 , B23B2260/068 , B23B2260/088 , B23B2260/124 , B23B2270/20
摘要： A drill bushing for a drill unit. In one embodiment, the drill bushing includes a base member having an upper surface, a lower surface configured to rest on a workpiece having a pilot hole, and a retaining member that projects from the lower surface of the base member. The retaining member has a cylindrical outer diameter that fits within the pilot hole. The drill bushing further includes a drill hole that passes from the upper surface of the base member through the retaining member to provide a passage for a drill bit. The drill bushing further includes an expandable slit that passes through the base member and the retaining member to the drill hole, and an adjustment member configured to expand the expandable slit to increase the cylindrical outer diameter of the retaining member within the pilot hole.
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公开(公告)号：US10744572B2
公开(公告)日：2020-08-18
申请号：US16167349
申请日：2018-10-22
申请人： The Boeing Company
摘要： An orbital drill bushing adapter for use with a drill unit. In one embodiment, the orbital drill bushing adapter comprises a main body and locking arms. The main body includes a base member having an upper surface, a lower surface, and an external side wall that extends between the upper surface and the lower surface. The main body further includes a cylindrical spacer that projects from the lower surface of the base member, and is configured to fit in a drill hole of an orbital drill bushing. The main body includes a cylindrical hole that passes through the base member and the cylindrical spacer. The locking arms are pivotally coupled to the base member, and are configured to clamp the main body onto the orbital drill bushing.
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公开(公告)号：US10150207B2
公开(公告)日：2018-12-11
申请号：US15347609
申请日：2016-11-09
申请人： The Boeing Company
IPC分类号： B25B23/14 , B25B13/48 , B25B13/08 , B25B23/00 , B25B23/142
摘要： A tool for rotating a first component of an assembly relative to a second component of the assembly is disclosed. The tool comprises a ring support, a first wrench, coupled to the ring support, a worm ring, rotationally coupled to the ring support, a second wrench, coupled to the worm ring, and a worm screw, rotationally coupled to the ring support and in mesh with the worm ring.
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公开(公告)号：US20180021860A1
公开(公告)日：2018-01-25
申请号：US15214139
申请日：2016-07-19
申请人： The Boeing Company
IPC分类号： B23B49/02
CPC分类号： B23B49/026 , B23B47/28 , B23B47/287 , B23B2215/04 , B23B2247/04 , B23B2247/08 , B23B2247/12 , B23B2260/136 , B23B2270/12 , F16B13/00 , Y10T408/558 , Y10T408/563
摘要： A fastener for fastening a drill jig to overlapping work pieces and clamping the overlapping work pieces for facilitating accurate drilling of the overlapping work pieces including a fastener body and a damper assembly operatively connected to the fastener body. The damper assembly is configured to enable application of a first load to the drill jig, and the fastener body is configured to enable application of a second load to the overlapping work pieces when the fastener fastens the drill jig to the overlapping work pieces. The first load is less than the second load. The first load is sufficient to hold the drill jig to the overlapping work pieces during drilling but without causing significant deformation of the drill jig. The second load is sufficient to reduce the formation of burrs during drilling of a hole through the overlapping working pieces.
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