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公开(公告)号：US10442010B2
公开(公告)日：2019-10-15
申请号：US15018159
申请日：2016-02-08
Applicant: The Boeing Company
Inventor： Wesley Edward Holleman , Mark Douglas Fuller
IPC: B23B49/00
Abstract: Provided are methods for verifying sequences of different operations and controlling processing order in accordance with these sequences. Also provided are apparatuses for executing these methods. A method may involve determining a current configuration of an indicator positioned on a part. This operation may be performed using a tester coupled to a processing portion. If the current configuration of the indicator corresponds to this particular processing portion, then the part is processed using this processing portion. The indicator is then changed to a new configuration corresponding to another processing portion for performing the next operation in the sequence. The processing is only performed if the indicator has the current configuration corresponding to the processing portion. Otherwise, the operation is not performed, and the current configuration of the indicator not changed retained. The indicator may be a mechanical device or an electronic device.
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公开(公告)号：US09884371B2
公开(公告)日：2018-02-06
申请号：US14942812
申请日：2015-11-16
Applicant: THE BOEING COMPANY
Inventor： Wesley Edward Holleman , Gary A. Lipczynski , Nicholas R. Farrell
CPC classification number: B23B45/00 , B23B49/00 , B23B49/02 , B23B2215/04 , B23B2226/27 , B23B2228/36 , B23B2260/128 , B23B2270/30 , B23B2270/48 , B23B2270/62 , B23Q11/0046 , B23Q15/22 , B23Q17/20 , Y10T408/56245
Abstract: Apparatus and methods for performing and controlling the sequence of steps in a multi-step machining process utilizing a plurality of drilling units, where each drilling unit is configured to perform at least one step of the multi-step machining process. Air pressure sensors in each drilling unit measure air pressures at the surface of a workpiece where the cutting tool of the drilling unit is engaged, which measured air pressures indicate air flow at the surface. These air flows in turn indicate the state of the machining at the surface of the workpiece, and based on the state of the machining, a machine control system will determine whether a drilling unit can perform its particular machining operation in the proper sequence on the workpiece.
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Patent Agency Ranking
公开(公告)号：US20170259355A1
公开(公告)日：2017-09-14
申请号：US15068636
申请日：2016-03-13
Applicant: The Boeing Company
Inventor： Nicholas Ryan Farrell , Branko Sarh , Michael L. Caldarera , Gary Lipczynski , Wesley Edward Holleman , James Darryl Gamboa
CPC classification number: B23C5/16 , B23B51/08 , B23B2220/445 , B23B2270/26 , B23C5/10 , B23C2215/04 , B23C2220/52 , B23C2220/605 , B24B39/02
Abstract: A combination cutting and burnishing orbital drilling tool may include an elongate tool body including a cutting end and extending along a longitudinal axis. The tool body may include a burnishing portion spaced from the cutting end and configured to induce residual stress in a side wall of a hole without removing material. The tool body may further include a cutting portion interposed between the cutting end and the burnishing portion. The cutting portion may be configured to remove material from a workpiece, thereby creating the hole, during an orbital drilling process.
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4.发明申请ORBITAL CUTTING TOOL HAVING CUTTING EDGES WITH AXIALLY VARYING CIRCUMFERENTIAL SPACING 审中-公开具有轴向变化的圆形间距的切割边的圆刀切割工具公开(公告)号：US20160288222A1
公开(公告)日：2016-10-06
申请号：US14678895
申请日：2015-04-03
Applicant: The Boeing Company
Inventor： Nicholas Ryan Farrell , Wesley Edward Holleman , Gary Alan Lipczynski , William P. Zanteson
IPC: B23C5/10
CPC classification number: B23C5/10 , B23B51/04 , B23C3/02 , B23C2210/0492 , B23C2210/246 , B23C2210/282 , B23C2220/52 , B23C2226/27
Abstract: A cutting tool for use in an orbital drilling machine may include a cutting-tool body having a longitudinal axis and a plurality of cutting edges supported on the cutting-tool body and distributed circumferentially around the cutting-tool body. Each cutting edge may extend along the longitudinal axis in a respective helix. A circumferential spacing may be defined between each pair of circumferentially adjacent cutting edges for each position of the longitudinal axis along which the cutting edges extend. The circumferential spacing between at least first and second cutting edges of the plurality of cutting edges may be different at spaced-apart first and second positions along the longitudinal axis.
Abstract translation: 用于轨道钻孔机的切割工具可以包括具有纵向轴线的切割工具主体和被支撑在切割工具主体上并分布在切割工具主体周围的多个切割边缘。 每个切削刃可以沿着纵向轴线在相应的螺旋中延伸。 可以在切割边缘延伸的纵向轴线的每个位置的每对周向相邻的切割边缘之间限定圆周间隔。 多个切割边缘的至少第一和第二切割边缘之间的周向间隔可以沿着纵向轴线间隔开的第一和第二位置不同。
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公开(公告)号：US10953481B2
公开(公告)日：2021-03-23
申请号：US15068636
申请日：2016-03-13
Applicant: The Boeing Company
Inventor： Nicholas Ryan Farrell , Branko Sarh , Michael L. Caldarera , Gary Lipczynski , Wesley Edward Holleman , James Darryl Gamboa
Abstract: A combination cutting and burnishing orbital drilling tool may include an elongate tool body including a cutting end and extending along a longitudinal axis. The tool body may include a burnishing portion spaced from the cutting end and configured to induce residual stress in a side wall of a hole without removing material. The tool body may further include a cutting portion interposed between the cutting end and the burnishing portion. The cutting portion may be configured to remove material from a workpiece, thereby creating the hole, during an orbital drilling process.
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公开(公告)号：US10058933B2
公开(公告)日：2018-08-28
申请号：US14678895
申请日：2015-04-03
Applicant: The Boeing Company
Inventor： Nicholas Ryan Farrell , Wesley Edward Holleman , Gary Alan Lipczynski , William P. Zanteson
CPC classification number: B23C5/10 , B23B51/04 , B23C3/02 , B23C2210/0492 , B23C2210/246 , B23C2210/282 , B23C2220/52 , B23C2226/27
Abstract: A cutting tool for use in an orbital drilling machine may include a cutting-tool body having a longitudinal axis and a plurality of cutting edges supported on the cutting-tool body and distributed circumferentially around the cutting-tool body. Each cutting edge may extend along the longitudinal axis in a respective helix. A circumferential spacing may be defined between each pair of circumferentially adjacent cutting edges for each position of the longitudinal axis along which the cutting edges extend. The circumferential spacing between at least first and second cutting edges of the plurality of cutting edges may be different at spaced-apart first and second positions along the longitudinal axis.
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公开(公告)号：US20170228567A1
公开(公告)日：2017-08-10
申请号：US15018159
申请日：2016-02-08
Applicant: The Boeing Company
Inventor： Wesley Edward Holleman , Mark Douglas Fuller
CPC classification number: B23B49/00 , B23B2215/04 , B23B2270/32
Abstract: Provided are methods for verifying sequences of different operations and controlling processing order in accordance with these sequences. Also provided are apparatuses for executing these methods. A method may involve determining a current configuration of an indicator positioned on a part. This operation may be performed using a tester coupled to a processing portion. If the current configuration of the indicator corresponds to this particular processing portion, then the part is processed using this processing portion. The indicator is then changed to a new configuration corresponding to another processing portion for performing the next operation in the sequence. The processing is only performed if the indicator has the current configuration corresponding to the processing portion. Otherwise, the operation is not performed, and the current configuration of the indicator not changed retained. The indicator may be a mechanical device or an electronic device.
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