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    TOOL ASSEMBLY, SYSTEM, AND METHOD FOR TRANSFERRING LOCATIONS AND DIMENSIONS OF A PATTERN OF HOLES
    4.
    发明申请
    TOOL ASSEMBLY, SYSTEM, AND METHOD FOR TRANSFERRING LOCATIONS AND DIMENSIONS OF A PATTERN OF HOLES 审中-公开

    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

    IPC: B23B47/28 ,  B25H7/02

    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.

    ALIGNMENT SYSTEMS AND METHODS FOR MOVING FUSELAGE STRUCTURES OF AN AEROSPACE VEHICLE INTO ASSEMBLY ALIGNMENT
    5.
    发明申请
    ALIGNMENT SYSTEMS AND METHODS FOR MOVING FUSELAGE STRUCTURES OF AN AEROSPACE VEHICLE INTO ASSEMBLY ALIGNMENT 审中-公开

    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

    IPC: B64F5/10 ,  B64C1/06 ,  B23P19/10 ,  B25J13/08

    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.

    MEMBRANE ASSEMBLY FOR VACUUM BAGGING AND METHOD OF VACUUM BAGGING
    8.
    发明申请
    MEMBRANE ASSEMBLY FOR VACUUM BAGGING AND METHOD OF VACUUM BAGGING 有权

    公开(公告)号：US20210316928A1

    公开(公告)日：2021-10-14

    申请号：US16846841

    申请日：2020-04-13

    Applicant: The Boeing Company

    Inventor： James R. Kendall ,  Santiago M. Mejia ,  Andrew M. Huckey ,  Raviendra S. Suriyaarachchi

    IPC: B65D81/20 ,  B65B31/04

    Abstract: A membrane assembly for vacuum bagging includes an elongate sheet of flexible material capable of being rolled up into a cylindrical configuration and unrolled from the cylindrical configuration into a flattened-out configuration, a bistable tape spring attached to or captured by the elongate sheet, and an inflatable tube attached to or captured by the elongate sheet. The bistable tape spring has a first stable state which is a straightened-out state, a second stable state which is a rolled-up state, and a transition state between the first and second stable states. The inflatable tube is sealed at one end and has an orifice at the other end for admission of a fluid therethrough for inflation of the inflatable tube.

    Tool assembly, system, and method for transferring locations and dimensions of a pattern of holes
    9.
    发明授权
    Tool assembly, system, and method for transferring locations and dimensions of a pattern of holes 有权

    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

    IPC: B23B47/28 ,  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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