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公开(公告)号：US20170369271A1
公开(公告)日：2017-12-28
申请号：US15190119
申请日：2016-06-22
Applicant: The Boeing Company
Inventor： Bradley J. Mitchell , Nick S. Evans , Damien O. Martin , Aphea Ann Thornton , Eerik J. Helmick
IPC: B65H59/10 , B65H51/005
CPC classification number: B65H59/10 , B65H51/005 , B65H2701/36 , H01R43/28 , H02G1/14
Abstract: A wire processing system includes a tray having at least one tray surface configured to sequentially receive a first wire and a second wire from a wire feed system of a wire processing machine. The tray surface has a surface feature configured to provide a wire-to-surface coefficient of friction between the tray surface and the first wire higher than a wire-to-wire coefficient of friction between the first wire and the second wire laying on top of the first wire. The wire-to-surface coefficient of friction reduces movement of at least a portion of the first wire relative to the tray surface during movement of the second wire relative to the first wire.
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22.发明申请公开(公告)号：US20170308068A1
公开(公告)日：2017-10-26
申请号：US15137556
申请日：2016-04-25
Applicant: The Boeing Company
Inventor： Eerik J. Helmick , Bradley J. Mitchell , Nick S. Evans
IPC: G05B19/418 , H01R43/20 , H01R107/00
CPC classification number: G05B19/41805 , B25J9/1687 , G05B2219/39183 , G05B2219/45033 , G05B2219/45064 , H01R43/20 , H01R2107/00 , Y10S901/02
Abstract: A method 500 of operating an automated machine 100 is provided for inserting wires into grommet cavity locations 110 of an electrical connector 112 to compensate for manufacturing tolerances associated with the electrical connector. The method comprises inserting wires into grommet cavity locations of the electrical connector based upon a plug map 300 having offset values to compensate for manufacturing tolerances associated with the electrical connector. The method may further comprise selecting from a plurality of pre-generated plug maps having offset values the closest matching pre-generated plug map for the electrical connector based upon offset values associated with each of the plurality of pre-generated plugs maps. The selected pre-generated plug map having offset values corresponds to the plug map used to insert wires into grommet cavity locations of the electrical connector.
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公开(公告)号：US20170028637A1
公开(公告)日：2017-02-02
申请号：US15063347
申请日：2016-03-07
Applicant: The Boeing Company
Inventor： Nick S. Evans , Faraón Torres , Ryan G. Ziegler , Samuel F. Harrison , Ciro J. Grijalva, III , Hayden S. Osborn
CPC classification number: B33Y70/00 , B05D1/265 , B05D1/34 , B05D3/06 , B05D3/067 , B05D3/068 , B05D3/12 , B29B11/00 , B29B11/16 , B29C35/0805 , B29C35/16 , B29C48/02 , B29C64/00 , B29C64/106 , B29C64/129 , B29C64/135 , B29C64/165 , B29C64/20 , B29C64/25 , B29C64/386 , B29C64/40 , B29C69/001 , B29C70/16 , B29C70/28 , B29C70/38 , B29C70/545 , B29C2035/0822 , B29C2035/0827 , B29C2035/0833 , B29C2035/0838 , B29C2035/0844 , B29K2063/00 , B29K2101/10 , B29K2105/0058 , B29K2105/06 , B29K2105/0872 , B29K2105/10 , B29K2105/101 , B29K2105/12 , B29K2105/25 , B29K2105/253 , B29K2995/005 , B29L2031/00 , B29L2031/3076 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02 , C09D5/00 , C09D201/00
Abstract: A system (700) for additively manufacturing a composite part (102) comprises a delivery guide (112), movable relative to a surface (114). The delivery guide (112) is configured to deposit at least a segment (120) of a continuous flexible line (106) along a print path (122). The continuous flexible line (106) comprises a non-resin component (108) and a thermosetting-resin component (110). The thermosetting-resin component (110) comprises a first part (253) and a second part (255). The non-resin component (108) comprises a first element (271) and a second element (273). The system (700) further comprises a first resin-part applicator (236), configured to apply the first part (253) to the first element (271), and a second resin-part applicator (237), configured to apply the second part (255) to the second element (273). The system (700) also comprises a feed mechanism (104), configured to pull the first element (271) through the first resin-part applicator (236), to pull the second element (273) through the second resin-part applicator (237), and to push the continuous flexible line (106) out of the delivery guide (112).
Abstract translation: 用于相加地制造复合部件（102）的系统（700）包括可相对于表面（114）移动的输送引导件（112）。 输送引导件（112）被配置成沿着打印路径（122）沉积连续柔性线（106）的至少一段（120）。 连续柔性管线（106）包括非树脂部件（108）和热固性树脂部件（110）。 热固性树脂组分（110）包括第一部分（253）和第二部分（255）。 非树脂部件（108）包括第一元件（271）和第二元件（273）。 所述系统（700）还包括构造成将第一部分（253）施加到第一元件（271）的第一树脂部分施加器（236）和第二树脂部分施加器（237），其被配置为施加第二部分 部分（255）到第二元素（273）。 系统（700）还包括进给机构（104），其构造成通过第一树脂部分施加器（236）拉动第一元件（271），以将第二元件（273）拉过第二树脂部分施加器 并且将连续柔性线（106）推出输出导向件（112）。
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公开(公告)号：US20170028636A1
公开(公告)日：2017-02-02
申请号：US14995620
申请日：2016-01-14
Applicant: The Boeing Company
Inventor： Nick S. Evans , Faraón Torres , Ryan G. Ziegler , Samuel F. Harrison , Ciro J. Grijalva, III , Hayden S. Osborn
CPC classification number: B33Y70/00 , B05D1/265 , B05D1/34 , B05D3/06 , B05D3/067 , B05D3/068 , B05D3/12 , B29B11/00 , B29B11/16 , B29C35/0805 , B29C35/16 , B29C47/0002 , B29C64/00 , B29C64/106 , B29C64/129 , B29C64/135 , B29C64/165 , B29C64/20 , B29C64/25 , B29C64/386 , B29C64/40 , B29C69/001 , B29C70/16 , B29C70/28 , B29C70/38 , B29C70/545 , B29C2035/0822 , B29C2035/0827 , B29C2035/0833 , B29C2035/0838 , B29C2035/0844 , B29K2063/00 , B29K2101/10 , B29K2105/0058 , B29K2105/06 , B29K2105/0872 , B29K2105/10 , B29K2105/101 , B29K2105/12 , B29K2105/25 , B29K2105/253 , B29K2995/005 , B29L2031/00 , B29L2031/3076 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02 , C09D5/00 , C09D201/00
Abstract: A method (300) of additively manufacturing a composite part (102) is disclosed. The method (300) comprises depositing a segment (120) of a continuous flexible line (106) along a print path (122). The continuous flexible line (106) comprises a non-resin component (108) and a thermosetting resin component (110) that is not fully cured. The method (300) further comprises, while advancing the continuous flexible line (106) toward the print path (122), delivering a predetermined or actively determined amount of curing energy (118) at least to a portion (124) of the segment (120) of the continuous flexible line (106) at a controlled rate after the segment (120) of the continuous flexible line (106) is deposited along the print path (122) to at least partially cure at least the portion (124) of the segment (120) of the continuous flexible line (106).
Abstract translation: 公开了一种叠加制造复合部件（102）的方法（300）。 方法（300）包括沿着打印路径（122）沉积连续柔性线（106）的段（120）。 连续柔性管线（106）包括未完全固化的非树脂部件（108）和热固性树脂部件（110）。 所述方法（300）还包括在将连续柔性管线（106）朝向打印路径（122）推进的同时，将至少预定或主动确定量的固化能量（118）输送到所述段的一部分（124） 在所述连续柔性管线（106）的段（120）沿着所述打印路径（122）沉积以至少部分地固化所述连续柔性管线（106）的所述部分（124）的部分 所述连续柔性线（106）的所述段（120）。
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公开(公告)号：US20170028635A1
公开(公告)日：2017-02-02
申请号：US14995507
申请日：2016-01-14
Applicant: The Boeing Company
Inventor： Nick S. Evans , Faraón Torres , Ryan G. Ziegler , Samuel F. Harrison , Ciro J. Grijalva, III , Hayden S. Osborn
CPC classification number: B29C70/545 , B29C64/106 , B29C64/165 , B29C64/20 , B29C64/386 , B29C69/001 , B29C70/16 , B29C70/38 , B29C70/384 , B29K2101/10 , B29K2105/0058 , B29K2105/101 , B29K2105/25 , B29K2995/005 , B29L2031/3076 , B33Y10/00 , B33Y30/00 , B33Y40/00 , B33Y50/02
Abstract: A system (100) for additively manufacturing a composite part (102) is disclosed. The system (100) comprises a delivery guide (112), movable relative to a surface (114). The delivery guide (112) is configured to deposit at least a segment (120) of a continuous flexible line (106) along a print path (122). The continuous flexible line (106) comprises a non-resin component (108) and a thermosetting resin component (110) that comprises a first part (253) and a second part (255) of a thermosetting resin (252). The print path (122) is stationary relative to the surface (114). The delivery guide (112) comprises a first inlet (170) configured to receive the non-resin component (108), and a second inlet (250) configured to receive at least the first part (253) of the thermosetting resin (252). The delivery guide (112) is further configured to apply the first part (253) and the second part (255) of the thermosetting resin (252) to the non-resin component (108). The system 100 further comprises a feed mechanism (104), configured to push the continuous flexible line (106) out of the delivery guide (112).
Abstract translation: 公开了一种用于相加地制造复合部件（102）的系统（100）。 系统（100）包括可相对于表面（114）移动的输送引导件（112）。 输送引导件（112）被配置成沿着打印路径（122）沉积连续柔性线（106）的至少一段（120）。 连续柔性线（106）包括非树脂组分（108）和热固性树脂组分（110），其包含热固性树脂（252）的第一部分（253）和第二部分（255）。 打印路径（122）相对于表面（114）是静止的。 输送引导件（112）包括构造成接收非树脂部件（108）的第一入口（170）和构造成容纳至少热固性树脂（252）的第一部分（253）的第二入口（250） 。 输送引导件（112）进一步构造成将热固性树脂（252）的第一部分（253）和第二部分（255）施加到非树脂部件（108）上。 系统100还包括进给机构（104），其构造成将连续柔性管线（106）推出输送引导件（112）。
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Patent Agency Ranking
公开(公告)号：US20170028628A1
公开(公告)日：2017-02-02
申请号：US14931573
申请日：2015-11-03
Applicant: The Boeing Company
Inventor： Nick S. Evans , Faraón Torres , Ryan G. Ziegler , Samuel F. Harrison , Ciro J. Grijalva, III , Hayden S. Osborn
IPC: B29C67/00
CPC classification number: B29C64/106 , B29C64/141 , B29C64/386 , B29C70/382 , B29K2063/00 , B29K2105/08 , B29L2031/3076 , B33Y30/00 , B33Y50/02
Abstract: A system (100) for additively manufacturing a composite part (102) is disclosed. The system (100) comprises a delivery guide (112), movable relative to a surface (114). The delivery guide (112) is configured to deposit at least a segment (120) of a continuous flexible line (106) along a print path (122). The print path (122) is stationary relative to the surface (114). The continuous flexible line (106) comprises a non-resin component (108) and a thermosetting-epoxy-resin component (110) that is partially cured. The system (100) also comprises a feed mechanism (104), configured to push the continuous flexible line (106) through the delivery guide (112). The system (100) further comprises a cooling system (234), configured to maintain the thermosetting-epoxy-resin component (110) of the continuous flexible line (106) below a threshold temperature prior to depositing the segment (120) of the continuous flexible (106) along the print path (122) via the delivery guide (112).
Abstract translation: 公开了一种用于相加地制造复合部件（102）的系统（100）。 系统（100）包括可相对于表面（114）移动的输送引导件（112）。 输送引导件（112）被配置成沿着打印路径（122）沉积连续柔性线（106）的至少一段（120）。 打印路径（122）相对于表面（114）是静止的。 连续柔性线（106）包括部分固化的非树脂组分（108）和热固性环氧树脂组分（110）。 系统（100）还包括进给机构（104），其构造成推动连续柔性管线（106）穿过输送引导件（112）。 该系统（100）还包括冷却系统（234），其被配置为在连续柔性管线（106）的段（120）沉积之前将连续柔性管线（106）的热固性环氧树脂组分（110）维持在阈值温度以下 通过输送引导件（112）沿着打印路径（122）弹性（106）。
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公开(公告)号：US20250124796A1
公开(公告)日：2025-04-17
申请号：US18484855
申请日：2023-10-11
Applicant: The Boeing Company
Inventor： Zachary P. Stock , Hannah G. Gillespie , Nick S. Evans
Abstract: An airport object location system comprising a number of vehicle location units, a sensor system, and a model generator. The number of vehicle location units is connected to a number of vehicles. The number of vehicle location units generate vehicle location information for the number of vehicles in an area including an operations surface at an airport and vehicle timestamps for the vehicle location information. The sensor system is connected to a reference vehicle. The sensor system is configured to generate sensor data for the area, wherein reference timestamps and reference location information are associated with the sensor data. The model generator is configured to correlate the vehicle location information for the vehicles with the sensor data using the vehicle timestamps, the reference location information, and the reference timestamps to form a dataset.
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公开(公告)号：US12061256B2
公开(公告)日：2024-08-13
申请号：US17988001
申请日：2022-11-16
Applicant: The Boeing Company
Inventor： Tyler C. Staudinger , Nick S. Evans
IPC: G01S13/00 , G01M15/14 , G01S13/86 , G01S13/934 , G01S17/10 , G01S17/894 , G01S17/933 , G01S19/14 , G01W1/00
CPC classification number: G01S13/934 , G01M15/14 , G01S13/862 , G01S13/867 , G01S17/10 , G01S17/894 , G01S17/933 , G01S19/14 , G01W1/00
Abstract: In an example, a method is described. The method includes causing one or more sensors arranged on an aircraft to acquire, over a window of time, first data associated with a first object that is within an environment of the aircraft, where the one or more sensors include one or more of a light detection and ranging (LIDAR) sensor, a radar sensor, or a camera, causing an array of microphones arranged on the aircraft to acquire, over approximately the same window of time as the first data is acquired, first acoustic data associated with the first object, and training a machine learning model by using the first acoustic data as an input value to the machine learning model and by using an azimuth, a range, an elevation, and a type of the first object identified from the first data as ground truth output labels for the machine learning model.
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公开(公告)号：US11783575B2
公开(公告)日：2023-10-10
申请号：US17364038
申请日：2021-06-30
Applicant: THE BOEING COMPANY
Inventor： Cullen Billhartz , Mary Karroqe , Eric R. Muir , Tyler Staudinger , Nick S. Evans
IPC: G06K9/00 , G06V20/10 , G06T7/11 , G06T7/73 , G06N20/00 , B64D45/08 , B64D47/08 , G06T3/40 , G06F18/2431 , G06F18/2433
CPC classification number: G06V20/176 , B64D45/08 , B64D47/08 , G06F18/2431 , G06F18/2433 , G06N20/00 , G06T3/40 , G06T7/11 , G06T7/73 , G06T2207/10016 , G06T2207/10032 , G06T2207/20081 , G06T2207/20132 , G06T2207/20164 , G06T2207/30181 , G06T2207/30204 , G06T2207/30244
Abstract: A method of supporting an aircraft approaching a runway is provided. Example implementations involve receiving a sequence of images, captured by a camera onboard the aircraft. Example implementations involve applying a received image to a machine learning model trained to detect the runway or a runway marking in the image, and to produce a mask that includes a segment of pixels of the image assigned to an object class for the runway or marking. Example implementations may also involve applying the mask to a corner detector to detect interest points on the mask and match the interest points to corresponding points on the runway or the marking that have known runway-framed local coordinates. Example implementations may also involve performing a perspective-n-point estimation to determine a current pose estimate of the aircraft relative to the runway or the marking and outputting the current pose estimate for use during final approach.
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公开(公告)号：US20220238031A1
公开(公告)日：2022-07-28
申请号：US17552138
申请日：2021-12-15
Applicant: The Boeing Company
Inventor： Nick S. Evans , Eric R. Muir , Tyler C. Staudinger , Michelle D. Warren
Abstract: Solutions are provided for auto-labeling sensor data for machine learning (ML). An example includes: determining a platform's own position; recording, from a sensor aboard the platform, sensor data comprising a sensor image; receiving position data for at least one intruder object (e.g., a nearby airborne object); based at least on the position data for the intruder object and the platform's position, determining a relative position and a relative velocity of the intruder object; based at least on the relative position and a relative velocity of the intruder object and a field of view of the sensor, determining an expected position of the intruder object in the sensor image; labeling the sensor image, wherein the labeling comprises annotating the sensor image with a region of interest and an object identification; and training an artificial intelligence (AI) model using the labeled sensor image.
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