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Patent Agency Ranking
公开(公告)号：US10016820B2
公开(公告)日：2018-07-10
申请号：US15019930
申请日：2016-02-09
Applicant: The Boeing Company
Inventor： Jake A. Wilson , Andrew M. Huckey , Mark E. Nestleroad , Craig A. Charlton
CPC classification number: B23B49/02 , B23B51/06 , B23B2215/04 , B23B2250/12 , B23B2260/126 , B23Q11/0075 , Y02P70/171 , Y10T408/455 , Y10T408/569
Abstract: 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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2.发明申请公开(公告)号：US20190100333A1
公开(公告)日：2019-04-04
申请号：US15723471
申请日：2017-10-03
Applicant: The Boeing Company
Inventor： Jake A. Wilson , Craig A. Charlton , Andrew M. Huckey , Mark E. Nestleroad
Abstract: A system for moving first and second fuselage structures into assembly alignment, the system including a first transmitter indexed to a first seat track of the first fuselage structure, a first reflector target indexed to a first seat track of the second fuselage structure, a second transmitter indexed to a second seat track of the first fuselage structure, a second reflector target indexed to a second seat track of the second fuselage structure, wherein the first and second transmitters and the first and second reflector targets cooperate to provide first and second measurements indicative of position of the first fuselage structure relative to the second fuselage structure, and a manipulator system including at least one assembly actuator coupled to the first fuselage structure to move the first fuselage structure into assembly alignment with the second fuselage structure based upon the first and second measurements.
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3.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
Applicant: The Boeing Company
Inventor： Mark E. Nestleroad , Craig A. Charlton , Jake A. Wilson , Andrew M. Huckey
CPC classification number: B23B47/287 , B23B2215/04 , B23B2247/12 , B25H7/02
Abstract: 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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4.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
Applicant: The Boeing Company
Inventor： Mark E. Nestleroad , Craig A. Charlton , Jake A. Wilson , Andrew M. Huckey
Abstract: 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
Applicant: The Boeing Company
Inventor： Jake A. Wilson , Andrew M. Huckey , Mark E. Nestleroad , Craig A. Charlton
CPC classification number: B23B49/02 , B23B51/06 , B23B2215/04 , B23B2250/12 , B23B2260/126 , B23Q11/0075 , Y02P70/171 , Y10T408/455 , Y10T408/569
Abstract: 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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