Automatic assembly line for mattress spring

    公开(公告)号:US20250065457A1

    公开(公告)日:2025-02-27

    申请号:US18947509

    申请日:2024-11-14

    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.

    Edge trimming for moving-line fabrication of aircraft

    公开(公告)号:US12202164B2

    公开(公告)日:2025-01-21

    申请号:US17454304

    申请日:2021-11-10

    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.

    Autonomous robust assembly planning

    公开(公告)号:US12179362B2

    公开(公告)日:2024-12-31

    申请号:US18594139

    申请日:2024-03-04

    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.

    METHOD AND ASSEMBLY SYSTEM FOR AUTOMATED MACHINE BASED PRODUCT ASSEMBLING

    公开(公告)号:US20240345565A1

    公开(公告)日:2024-10-17

    申请号:US18294231

    申请日:2022-08-08

    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.”

    SYSTEMS AND METHODS FOR OPTIMIZING OPERATION AT A MANUFACTURING ASSEMBLY LINE

    公开(公告)号:US20240231327A1

    公开(公告)日:2024-07-11

    申请号:US18397459

    申请日:2023-12-27

    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.

    Aircraft assembly formed of mating half barrel sections and the method of assembling the same

    公开(公告)号:US11801576B2

    公开(公告)日:2023-10-31

    申请号:US17454280

    申请日:2021-11-10

    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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