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公开(公告)号：US20230364669A1
公开(公告)日：2023-11-16
申请号：US18356032
申请日：2023-07-20
Applicant: The Boeing Company
Inventor： Harinder S. Oberoi , Branko Sarh , Melissa Ann Findlay , Alan S. Draper , Jorge Alberto Arriaga , Richard Griffith Reese, IV , Alfredo Jose Gerosa , Kevin Marion Barrick , Michael J. Kozak , Quang T. Do , Jeffrey Lawrence Miller , Yuanxin Charles Hu
IPC: B21J15/28 , B64F5/10 , B21J15/02 , B21J15/10 , B21J15/14 , B60G3/14 , B25J5/00 , B29C65/70 , B25J9/16 , B25J11/00 , F16B19/06 , B23P19/10 , B60G7/00 , B21J15/32 , B21J15/40 , G05B19/418 , B25B5/16 , B29C39/12 , B29C39/22 , B64C1/06 , G05D1/00 , G05D3/12 , B29C45/14 , B29C39/02 , B29C39/10 , B64F5/50
CPC classification number: B21J15/28 , B64F5/10 , B21J15/02 , B21J15/10 , B21J15/142 , B60G3/145 , B25J5/007 , B29C65/70 , B25J9/1682 , B25J11/007 , F16B19/06 , B23P19/10 , B25J9/1687 , B25J9/1697 , B25J11/005 , B60G7/001 , B60G7/008 , B21J15/32 , B21J15/40 , G05B19/41805 , B25B5/163 , B29C39/123 , B29C39/22 , B64C1/06 , G05D1/0088 , G05D3/12 , B29C45/14336 , B29C39/026 , B29C39/10 , B64F5/50 , B23P2700/00 , B23P21/002
Abstract: A method and apparatus for building a fuselage assembly for an aircraft. A number of fixtures may be drive across a floor to an assembly area to form an assembly fixture. The fuselage assembly may be built on the assembly fixture.
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公开(公告)号：US20190388959A1
公开(公告)日：2019-12-26
申请号：US16563156
申请日：2019-09-06
Applicant: The Boeing Company
Inventor： Harinder S. Oberoi , Richard Griffith Reese, IV , Kevin Marion Barrick , Quang T. Do , Alan S. Draper , Yuanxin Charles Hu , Alfredo Jose Gerosa , Michael J. Kozak , Jeffrey Lawrence Miller
IPC: B21J15/28 , B64F5/10 , B21J15/02 , B21J15/10 , B21J15/14 , B60G3/14 , B25J5/00 , B25J9/16 , B25J11/00 , F16B19/06 , B23P19/10 , B60G7/00 , B21J15/32 , B21J15/40 , G05B19/418 , B25B5/16 , B29C39/12 , B29C39/22 , B64C1/06 , G05D1/00 , G05D3/12 , B29C45/14 , B29C39/02 , B29C39/10 , B64F5/50
Abstract: An apparatus for accessing an interior of a fuselage assembly. A tower having a number of platform levels may be driven into a selected tower position within an assembly area. The interior of the fuselage assembly may be accessed using the number of platform levels.
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公开(公告)号：US09937549B2
公开(公告)日：2018-04-10
申请号：US14559483
申请日：2014-12-03
Applicant: The Boeing Company
Inventor： Harinder S. Oberoi , Melissa Ann Findlay , Branko Sarh , Alan S. Draper , Jorge Alberto Arriaga
IPC: B21J15/02 , B21J15/28 , B21J15/10 , B21J15/14 , B60G3/14 , B25J9/16 , B25J11/00 , F16B19/06 , B23P19/10 , B60G7/00 , B21J15/32 , B21J15/40 , G05B19/418 , B25B5/16 , B29C39/12 , B29C39/22 , B64C1/06 , G05D1/00 , G05D3/12 , B29C45/14 , B29C39/02 , B29C39/10 , B25J5/00 , B64F5/10 , B64F5/50 , B23P21/00 , B29L31/00 , B60P3/025
CPC classification number: B21J15/28 , B21J15/02 , B21J15/10 , B21J15/142 , B21J15/32 , B21J15/40 , B23P19/10 , B23P21/002 , B23P2700/00 , B25B5/163 , B25J5/007 , B25J9/1682 , B25J9/1687 , B25J9/1697 , B25J11/005 , B25J11/007 , B29C39/026 , B29C39/10 , B29C39/123 , B29C39/22 , B29C45/14336 , B29C2045/14368 , B29C2793/0081 , B29K2715/00 , B29L2031/748 , B60G3/145 , B60G7/001 , B60G7/008 , B60G2204/143 , B60G2204/418 , B60G2206/8207 , B60G2300/60 , B60P3/025 , B64C1/06 , B64F5/10 , B64F5/50 , F16B19/06 , G05B19/41805 , G05B2219/45071 , G05D1/0088 , G05D3/12 , Y02P90/86 , Y10S901/01 , Y10S901/02 , Y10S901/41
Abstract: A method and apparatus for fastening two parts together. An initial interference fit may be created between a fastener and at least a portion of a hole extending through the two parts while maintaining a force equilibrium. A final interference fit may be created between the fastener and the hole, while maintaining a new force equilibrium.
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公开(公告)号：US11235375B2
公开(公告)日：2022-02-01
申请号：US16736376
申请日：2020-01-07
Applicant: The Boeing Company
Inventor： Harinder S. Oberoi , Richard Griffith Reese, IV , Quang T. Do , Alan S. Draper , Jeffrey Lawrence Miller , Michael J. Kozak , Vanco Stojanoski
IPC: B21J15/28 , B64F5/10 , B21J15/02 , B29C65/70 , F16B19/06 , B23P19/10 , G05D3/12 , G05B19/41 , B21J15/10 , B21J15/14 , B60G3/14 , B25J5/00 , B25J9/16 , B25J11/00 , B60G7/00 , B21J15/32 , B21J15/40 , G05B19/418 , B25B5/16 , B29C39/12 , B29C39/22 , B64C1/06 , G05D1/00 , B29C45/14 , B29C39/02 , B29C39/10 , B64F5/50 , B23P21/00 , B29L31/00 , B60P3/025
Abstract: A dual-interface coupler includes a utilities unit, a number of utility cables configured to provide a number of utilities to the utilities unit, a first coupling unit associated with the utilities unit, and a second coupling unit associated with the utilities unit. The first coupling unit is configured to mechanically couple the utilities unit to a first corresponding coupling unit and comprises a utility interface. The number of utilities are configured to flow from the utilities unit through the utilities interface. The second coupling unit is configured to mechanically couple the second coupling unit to a second corresponding coupling unit.
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公开(公告)号：US10960458B2
公开(公告)日：2021-03-30
申请号：US14559073
申请日：2014-12-03
Applicant: The Boeing Company
Inventor： Harinder S. Oberoi , Richard Griffith Reese, IV , Kevin Marion Barrick , Quang T. Do , Alan S. Draper , Jeffrey Lawrence Miller , Gregory Gudzinski
IPC: B23P19/10 , B25J11/00 , B21J15/02 , B21J15/10 , B21J15/14 , B21J15/28 , B21J15/32 , B21J15/40 , B25B5/16 , B25J5/00 , B25J9/16 , B29C39/02 , B29C39/10 , B29C39/12 , B29C39/22 , B29C45/14 , B60G3/14 , B60G7/00 , B64F5/10 , F16B19/06 , G05B19/418 , B64C1/06 , G05D1/00 , G05D3/12 , B64F5/50 , B23P21/00 , B29L31/00 , B60P3/025
Abstract: A method and apparatus for performing an assembly operation. A tool may be macro-positioned within an interior of a fuselage assembly. The tool may be micro-positioned relative to a particular location on a panel of the fuselage assembly. An assembly operation may be performed at the particular location on the panel using the tool.
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Patent Agency Ranking
公开(公告)号：US10406593B2
公开(公告)日：2019-09-10
申请号：US14559234
申请日：2014-12-03
Applicant: The Boeing Company
Inventor： Harinder S. Oberoi , Richard Griffith Reese, IV , Kevin Marion Barrick , Quang T. Do , Alan S. Draper , Yuanxin Charles Hu , Alfredo Jose Gerosa , Michael J. Kozak , Jeffrey Lawrence Miller
IPC: B25B5/16 , B25J5/00 , B25J9/16 , B64F5/10 , B64F5/50 , B23P21/00 , B25J11/00 , B60G3/14 , B60G7/00 , B64C1/06 , G05D1/00 , G05D3/12 , B21J15/02 , B21J15/10 , B21J15/14 , B21J15/28 , B21J15/32 , B21J15/40 , B23P19/10 , B29C39/02 , F16B19/06 , G05B19/418 , B29C39/12 , B29C39/22 , B29C45/14 , B29C39/10 , B29L31/00 , B60P3/025
Abstract: A method and apparatus for accessing an interior of a fuselage assembly. A tower having a number of platform levels may be driven into a selected tower position within an assembly area. The interior of the fuselage assembly may be accessed using the number of platform levels.
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公开(公告)号：US20190176213A1
公开(公告)日：2019-06-13
申请号：US16272916
申请日：2019-02-11
Applicant: The Boeing Company
Inventor： Harinder S. Oberoi , Melissa Ann Findlay , Jorge Alberto Arriaga , Branko Sarh , Alan S. Draper
IPC: B21J15/28 , B21J15/40 , B29C39/02 , B29C39/10 , B60G7/00 , B29C39/22 , B29C39/12 , B64F5/50 , B25J9/16 , B25J11/00 , F16B19/06 , B23P19/10 , B21J15/32 , B64F5/10 , B25J5/00 , B60G3/14 , B21J15/14 , B21J15/10 , B21J15/02 , G05D3/12 , G05D1/00 , B64C1/06 , B25B5/16 , G05B19/418 , B29C45/14
Abstract: An attachment for an end effector. The attachment may include a clamp and a foot adhesively bonded to an edge of the clamp and having a set of interlocking features that form a mechanical interlock with the clamp.
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公开(公告)号：US20160009422A1
公开(公告)日：2016-01-14
申请号：US14559518
申请日：2014-12-03
Applicant: The Boeing Company
Inventor： Harinder S. Oberoi , Branko Sarh , Melissa Ann Findlay , Alan S. Draper , Jorge Alberto Arriaga , Richard Griffith Reese, IV , Alfredo Jose Gerosa , Kevin Marion Barrick , Michael J. Kozak , Quang T. Do , Jeffrey Lawrence Miller , Yuanxin Charles Hu
IPC: B64F5/00
CPC classification number: B21J15/28 , B21J15/02 , B21J15/10 , B21J15/142 , B21J15/32 , B21J15/40 , B23P19/10 , B23P21/002 , B23P2700/00 , B25B5/163 , B25J5/007 , B25J9/1682 , B25J9/1687 , B25J9/1697 , B25J11/005 , B25J11/007 , B29C39/026 , B29C39/10 , B29C39/123 , B29C39/22 , B29C45/14336 , B29C2045/14368 , B29C2793/0081 , B29K2715/00 , B29L2031/748 , B60G3/145 , B60G7/001 , B60G7/008 , B60G2204/143 , B60G2204/418 , B60G2206/8207 , B60G2300/60 , B60P3/025 , B64C1/06 , B64F5/10 , B64F5/50 , F16B19/06 , G05B19/41805 , G05B2219/45071 , G05D1/0088 , G05D3/12 , Y02P90/86 , Y10S901/01 , Y10S901/02 , Y10S901/41
Abstract: A method and apparatus for building a fuselage assembly for an aircraft. A number of fixtures may be drive across a floor to an assembly area to form an assembly fixture. The fuselage assembly may be built on the assembly fixture.
Abstract translation: 一种用于建造飞机机身组件的方法和装置。 许多夹具可以穿过地板驱动到组装区域以形成组装夹具。 机身组件可以构建在组装夹具上。
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公开(公告)号：US09205933B2
公开(公告)日：2015-12-08
申请号：US14794925
申请日：2015-07-09
Applicant: The Boeing Company
Inventor： Harinder S. Oberoi , Blair P. Nelson , Alan S. Draper , Charles Y. Hu , Randall Matthewson , Branko Sarh
IPC: B64F5/00
CPC classification number: B64F5/0009 , B64C1/18 , B64F5/10 , B64F5/50 , Y10T29/49622 , Y10T29/53004 , Y10T29/534 , Y10T29/53417 , Y10T29/53974
Abstract: A facility for assembling aircraft fuselages comprises a plurality of movable cradles. Each cradle is configured to support a fuselage keel structure and assemble a panelized fuselage from the keel structure to obtain a full fuselage contour in a single upright build position.
Abstract translation: 用于组装飞机机身的设备包括多个可移动托架。 每个支架被配置为支撑机身龙骨结构，并从龙骨结构组装一个镶板机身，以在单个直立构造位置获得完整的机身轮廓。
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公开(公告)号：US11724305B2
公开(公告)日：2023-08-15
申请号：US16284417
申请日：2019-02-25
Applicant: The Boeing Company
Inventor： Harinder S. Oberoi , Branko Sarh , Melissa Ann Findlay , Alan S. Draper , Jorge Alberto Arriaga , Richard Griffith Reese, IV , Alfredo Jose Gerosa , Kevin Marion Barrick , Michael J. Kozak , Quang T. Do , Jeffrey Lawrence Miller , Yuanxin Charles Hu
IPC: B64F5/10 , B25J9/16 , B25J11/00 , B21J15/28 , B21J15/02 , B21J15/10 , B21J15/14 , B60G3/14 , B25J5/00 , B29C65/70 , F16B19/06 , B23P19/10 , B60G7/00 , B21J15/32 , B21J15/40 , G05B19/418 , B25B5/16 , B29C39/12 , B29C39/22 , B64C1/06 , G05D1/00 , G05D3/12 , B29C45/14 , B29C39/02 , B29C39/10 , B64F5/50 , B23P21/00 , B29L31/00 , B60P3/025
CPC classification number: B21J15/28 , B21J15/02 , B21J15/10 , B21J15/142 , B21J15/32 , B21J15/40 , B23P19/10 , B25B5/163 , B25J5/007 , B25J9/1682 , B25J9/1687 , B25J9/1697 , B25J11/005 , B25J11/007 , B29C39/026 , B29C39/10 , B29C39/123 , B29C39/22 , B29C45/14336 , B29C65/70 , B60G3/145 , B60G7/001 , B60G7/008 , B64C1/06 , B64F5/10 , B64F5/50 , F16B19/06 , G05B19/41805 , G05D1/0088 , G05D3/12 , B23P21/002 , B23P2700/00 , B23P2700/01 , B29C2045/14368 , B29C2793/0081 , B29K2715/00 , B29L2031/748 , B60G2204/143 , B60G2204/418 , B60G2206/8207 , B60G2300/60 , B60P3/025 , G05B2219/45071 , Y02P90/80 , Y10S901/01 , Y10S901/02 , Y10S901/41
Abstract: A method and apparatus for building a fuselage assembly for an aircraft. A number of fixtures may be drive across a floor to an assembly area to form an assembly fixture. The fuselage assembly may be built on the assembly fixture.
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