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公开(公告)号:US20250065457A1
公开(公告)日:2025-02-27
申请号:US18947509
申请日:2024-11-14
Applicant: Dekui Intelligent Equipment(Suzhou) Co.,Ltd.
Inventor: Wende Sun , Jiugang Zhang , Lili Yao , Yunlong Cheng
Abstract: The present invention discloses an automatic assembly line for mattress spring, comprising a mattress spring conveying mechanism for conveying mattress springs; It also comprises a mattress spring frame assembly mechanism for installing frames on the mattress spring; It also comprises a mattress spring butterfly spring nailing mechanism for installing butterfly springs on the side of the mattress spring; This proposal designs an automatic assembly line for mattress spring, wherein the mattress spring frame assembly mechanism can automatically complete the loading of the frame, the transportation of the mattress spring frame assembly mechanism, the installation between the mattress spring and the frame, and the folding of non-woven fabric after the installation of the mattress spring frame; The entire automatic assembly line for mattress spring presents a high degree of automation without manual operation, which features high assembly efficiency and high assembly accuracy, thereby effectively improving the production process of products.
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公开(公告)号:US12202164B2
公开(公告)日:2025-01-21
申请号:US17454304
申请日:2021-11-10
Applicant: The Boeing Company
Inventor: Darrell D. Jones , Daniel R. Smith
Abstract: Systems and methods are provided for inspecting a structure. One embodiment is a method for inspecting a structure. The method includes advancing a structure along a track in a process direction, aligning a Non-Destructive Inspection (NDI) station at the track with an edge of the structure that was trimmed upstream of the cleaning station, imaging the edge via the Non-Destructive Inspection (NDI) station, characterizing the edge based on the imaging, and advancing the structure further in the process direction via the track.
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公开(公告)号:US12179362B2
公开(公告)日:2024-12-31
申请号:US18594139
申请日:2024-03-04
Applicant: FANUC CORPORATION
Inventor: Yu Zhao , Tetsuaki Kato
Abstract: A method for tuning the force control parameters for a general robotic assembly operation. The method uses numerical optimization to evaluate different combinations of the parameters for a robot force controller in a simulation environment that is built based on a real-world robotic setup. This method performs autonomous tuning for assembly tasks based on closed loop force control simulation, where random samples from a distribution of force control parameter values are evaluated, and the optimization routine iteratively redefines the parameter distribution to find optimal values of the parameters. Each simulated assembly is evaluated using multiple simulations including random part positioning uncertainties. The performance of each simulated assembly is evaluated by the average of the simulation results, thus ensuring that the selected control parameters will perform well in most possible conditions. Once the parameters have been optimized, they are applied to real robots to perform the actual assembly operation.
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公开(公告)号:US20240345565A1
公开(公告)日:2024-10-17
申请号:US18294231
申请日:2022-08-08
Applicant: Siemens Aktiengesellschaft
Inventor: Kai Wurm , Vincent Dietrich , Philipp Sebastian Schmitt , Andreas Kindl
IPC: G05B19/4155 , B23P21/00
CPC classification number: G05B19/41805 , B25J9/1669 , B25J9/1687 , G05B19/4155 , G05B2219/50391
Abstract: It is proposed to assemble a product on a modular basis from product parts to be assembled, wherein the product assembling being split into two separate operations, by (i) automated machine fetching as well as automated machine placing the product parts part-by-part from a delivery area on optically localized distribution fixtures at a hand-over area in the course of a logistic distribution operation and a distribution fixture placed product part from optically localized distribution fixtures at the hand-over area on optically localized assembly fixtures at an assembly workspace in the course of an assembly operation, (ii) computing and executing by automated machine motion generation primary kinematic machine-motion-sequences and secondary kinematic machine-motion-sequences, (iii) providing an automated machine architecture to enable or ensure, based on a “world model for automated machines”, a three-dimensional model of an assembly environment, information ANG, of the product and the product parts and an “automated machine workflow.”
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5.
公开(公告)号:US12103649B2
公开(公告)日:2024-10-01
申请号:US18580772
申请日:2022-07-14
CPC classification number: B63B73/10 , B63B73/30 , B23P21/004 , E02B2017/0069 , E02B17/025
Abstract: Topside modules are fabricated at a production site using as a foundation for installation a gravity-based structure (GBS), which can stay afloat during water transportation. Modules fabrication includes: Stage I, fabrication of components; Stage II, fabrication of nodes from the components; Stage III, fabrication of sub-assemblies from the nodes; Stage IV, shotblasting and painting of assemblies; and Stage V, assembling modules from the assemblies. Then modules transportation, movement to their seats on the GBS and their integration include: Stage VI, moving the modules to an area near the dock using self-propelled vehicles. Stage VII, moving each module onto guides of a lifting system installed in a dry dock. Stage VIII, lifting each module until lifting system guides are connected with GBS top slab guides. Stage IX, moving each module to its seat on the GBS, installed on the GBS and integrated with other modules and the GBS.
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公开(公告)号:US20240231327A1
公开(公告)日:2024-07-11
申请号:US18397459
申请日:2023-12-27
Applicant: ATS Corporation
Inventor: Graham KNAP , Anton DOLGOVYKH , Albert KLEINIKKINK , Stanley Wellington KLEINIKKINK
IPC: G05B19/418 , B23P21/00
CPC classification number: G05B19/418 , B23P21/004 , G05B2219/31054
Abstract: Various systems and methods for optimizing operation at a manufacturing assembly line are disclosed. A method for optimizing operation at a manufacturing assembly line having a track on which a plurality of shuttles travel, the track including one or more stations at which a production task occurs and one or more track areas defined relative to the one or more stations, includes monitoring shuttle operation data associated with the plurality of shuttles on the track, and track sensor data associated with an operation state of the track; detecting an operation variation at the manufacturing assembly line based on the shuttle operation data; in response to detecting the operation variation, analyzing the shuttle operation data and the track sensor data to determine one or more degradation causes resulting in the operation variation; and generating an operation recommendation for resolving at least one degradation cause of the one or more degradation causes.
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公开(公告)号:US11959515B2
公开(公告)日:2024-04-16
申请号:US16968770
申请日:2019-02-13
Applicant: NSK LTD.
Inventor: Nobuyuki Hagiwara , Atsuhiro Ishii , Tokumasa Kikuchi , Tsuyoshi Kamoda
IPC: B21J13/08 , B21D39/00 , B21J5/02 , B21J9/02 , B21K19/00 , B21K25/00 , B21K27/00 , B23P19/00 , B23P21/00 , B65G35/00 , F16C19/18 , B62D65/12 , F16C35/063
CPC classification number: F16C19/186 , B21D39/00 , B21J5/02 , B21J9/02 , B21J9/025 , B21J13/08 , B21J13/085 , B21K25/00 , B23P19/00 , B23P21/00 , B65G35/00 , B62D65/12 , F16C35/063 , F16C2326/02
Abstract: A moving element (21) holding a workpiece (a hub unit bearing (1)) is horizontally loaded into an internal space (23) of an exterior (17) from an external space of the outer package (17), while being guided by a guide member (20) through an opening portion (a front surface side opening portion (25)) provided in the exterior (17) constituting a rotary forging apparatus (16). After completion of the loading process, the workpiece is subjected to rotary forging, using a forming die (18).
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公开(公告)号:US11845566B2
公开(公告)日:2023-12-19
申请号:US17454301
申请日:2021-11-10
Applicant: The Boeing Company
Inventor: Daniel R. Smith , Darrell D. Jones
CPC classification number: B64F5/10 , B23P23/06 , B23P21/004 , B23P2700/01
Abstract: Systems and methods are provided for fabrication of frames for aircraft.
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9.
公开(公告)号:US20230356337A1
公开(公告)日:2023-11-09
申请号:US18246053
申请日:2021-07-09
Applicant: AECC SHANGHAI COMMERCIAL AIRCRAFT ENGINE MANUFACTURING CO., LTD. , AECC COMMERCIAL AIRCRAFT ENGINE CO., LTD.
Inventor: Yiting HU , Wenxing MU , Fei PAN , Yuqian ZHOU
CPC classification number: B23P21/004 , B23P19/06
Abstract: A fastening tool. In the fastening tool, a top part guiding matching portion engages a top part guiding portion in a sliding fit; a pressing part guiding matching portion engages a pressing part guiding portion in a sliding fit; a lever hinged to a base part; a transmission part engages a transmission part guiding slot in a sliding fit; the transmission part is driven to slide by the pressing part, and the lever is driven to rotate by the transmission part, then the top part is driven to slide out, due to a reaction force acting on the pressing part by the transmission part and the friction between the pressing part and the base part, the pressing part remains to be self-locked by friction, which can constrain the pressing part and the top part is locked.
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10.
公开(公告)号:US11801576B2
公开(公告)日:2023-10-31
申请号:US17454280
申请日:2021-11-10
Applicant: The Boeing Company
Inventor: Darrell D. Jones , Daniel R. Smith , Jeremy Evan Justice
CPC classification number: B23P21/004 , B64F5/10 , B23P2700/01
Abstract: Systems and methods are provided for assembling an airframe of an aircraft, including receiving a half barrel section of fuselage, advancing the half barrel section in a process direction across multiple stations to separately and simultaneously perform work on the half barrel sections, and subsequently joining the half barrel segments to form a section of the airframe. Each pair of half barrel sections, such as upper and lower half barrels, are progressed through assembly line processes to be delivered to a joining station for joining the half barrels together to form a circumferential section of the fuselage. Multiple joined circumferential sections are joined together to form an elongated extent of the fuselage. Indexing features are provided in the assembly process to monitor and control the progression of the half barrel sections in the work stations of the assembly line process.
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