Browse Topic: Flexible manufacturing systems

Items (87)
Capability-Driven Adaptive Task Distribution for Flexible Multi-Human-Multi-Robot (MH-MR) Manufacturing Systems2020-01-13034/14/2020
Collaborative robots are more and more used in smart manufacturing because of their capability to work beside and collaborate with human workers. With the deployment of these robots, manufacturing tasks are more inclined to be accomplished by multiple humans and multiple robots (MH-MR) through teaming effort. In such MH-MR collaboration scenarios, the task distribution among the multiple humans and multiple robots is very critical to efficiency. It is also more challenging due to the heterogeneity of different agents. Existing approaches in task distribution among multiple agents mostly consider humans with assumed or known capabilities. However human capabilities are always changing due to various factors, which may lead to suboptimal efficiency. Although some researches have studied several human factors in manufacturing and applied them to adjust the robot task and behaviors. However, the real-time modeling and calculation of multiple human capabilities and real-time adaptive task distribution in flexible MH-MR manufacturing according to human capabilities are still challenging due to the complexity of human capabilities and heterogeneous multi-agent interactions. To address these issues, this paper first proposes a practical modeling approach to model and calculate the capabilities of different humans in real-time using some measurable performance indices. Based on these capabilities, this paper furthermore mathematically models the MH-MR manufacturing process and proposes a capability-driven adaptive task distribution approach with genetic algorithm based solutions to distribute different tasks to humans and robots online. The proposed adaptive approaches are validated through different MH-MR manufacturing tasks and the experimental results show that the approaches can significantly improve the manufacturing efficiency in terms of the time cost and the number of accomplished tasks than existing approaches in the presence of different time-varying human capabilities. Detailed results and statistical comparisons are presented to illustrate the effectiveness and advantages of the proposed solutions.
Zhang, ShaoboJia, Yunyi
Unsettled Technology Domains in Robotics for Automation in Aerospace ManufacturingEPR201901012/20/2019
Cost reduction and increasing production rates are driving automation of aerospace manufacturing. Articulated serial robots may replace bespoke gantry automation or human operations. Improved accuracy is key to enabling operations such as machining, additive manufacturing (AM), composite fabrication, drilling, automated program development, and inspection. New accuracy standards are needed to enable process-relevant comparisons between robotic systems. Accuracy can be improved through calibration of kinematic and joint stiffness parameters, joint output encoders, adaptive control that compensates for thermal expansion, and feedforward control that compensates for hysteresis and external loads. The impact of datuming could also be significantly reduced through modeling and optimization. Highly dynamic end effectors compensate high-frequency disturbances using inertial sensors and reaction masses. Global measurement feedback is a high-accuracy turnkey solution, but it is costly and has limited capability to compensate dynamic errors. Local measurement feedback is a mature, affordable, and highly accurate technology where the robot is required to position or align relative to some local feature. Locally clamped machine tools are an alternative approach that can utilize the flexibility of industrial robots while also enabling high-quality machined surfaces. Hybrid high-accuracy control strategies will be required for many processes. NOTE: SAE EDGE™ Research Reports are intended to identify and illuminate key issues in emerging, but still unsettled, technologies of interest to the mobility industry. The goal of SAE EDGE™ Research Reports is to stimulate discussion and work in the hope of promoting and speeding resolution of identified issues. SAE EDGE™ Research Reports are not intended to resolve the issues they identify or close any topic to further scrutiny.
Muelaner, Jody
Demonstration of Transformable Manufacturing Systems through the Evolvable Assembly Systems Project2019-01-13633/19/2019
Evolvable Assembly Systems is a five year UK research council funded project into flexible and reconfigurable manufacturing systems. The principal goal of the research programme has been to define and validate the vision and support architecture, theoretical models, methods and algorithms for Evolvable Assembly Systems as a new platform for open, adaptable, context-aware and cost effective production. The project is now coming to a close; the concepts developed during the project have been implemented on a variety of demonstrators across a number of manufacturing domains including automotive and aerospace assembly. This paper will show the progression of demonstrators and applications as they increase in complexity, specifically focussing on the Future Automated Aerospace Assembly Phase 1 technology demonstrator (FA3D). The FA3D Phase 1 demonstrated automated assembly of aerospace products using precision robotic processes in conjunction with low-cost reconfigurable fixturing supported by large volume metrology. This was underpinned by novel agent-based control for transformable batch-size-of-one production. The paper will conclude by introducing Phase 2 of the Future Automated Aerospace Assembly Demonstrator - currently in development - that will translate the Evolvable Assembly Systems research to a higher technology readiness level and address the challenges of scalable and transformable manufacturing systems.
Sanderson, DavidTurner, AlisonShires, EmmaChaplin, JackRatchev, Svetan
A Novel Fixturing Solution for Handling Complex-Shaped Components2017-01-20829/19/2017
Many components used in the aerospace industry are complex-shaped, without symmetric axes and parallel surfaces. Fabricating and repairing these components often require fixturing system to support manufacturing processes such as drilling, surface finishing, inspections and assembly. Currently available fixturing systems can be divided into dedicated and flexible fixtures. Among these, the flexible fixtures are suitable for rapidly changing fabricating processes and handling several complex-shaped components using same fixturing system. Background research suggested that the pin type fixturing system is the predominant design used in such applications to fix complex-shaped components. In pin type fixturing systems, force is applied to a single point of contact. This increases the pressure applied to the work piece and possibility of damaging these components. Further, conventional pins use rigid designs, which cannot adapt to the shape of the work piece. This reduces the applicable clamping force and the increases the possibility of slipping. This paper describes a fixturing system to address these problems by developing a distributed force fixing method with conformance to complex shapes. Proposed fixturing system uses jamming granular materials with negative pressure. A flexible rubber container fill with granular material is attached to the tip of a modified pin. When the container touches the work piece it conforms to the shape of the work piece. Then the rubber container vacuumed, which rigidifies the container and fix the shape, through granular jamming. Series of experiments were carried out to decide the best suited granular material in terms of highest holding force with best adaptability to a complex surface. Experiments were carried out using eight different low cost locally sourced materials. According to the experimental results proposed system successfully provide required holding forces to manipulate complex shaped components.
Jayaweera, NiroshKulasekera, AsithaMaduranga, PosinduKasun, ThilinaSeekkuarachchi, PrabodhSampath, Janaka
Manufacturing the Next Generation of Connected and Electrified Vehicle2016-01-02964/5/2016
Increasing electrification of the vehicle as well as the demands of increased connectivity presents automotive manufacturers with formidable challenges. Automakers and suppliers likely will encounter three practices that will influence how they develop and manufacture highly connected vehicles and future e-mobility platforms: 1) hierarchical production processes in fixed footprints that do not share data freely; 2) lack of real-time, in-line quality inspection and correction processes for complex miniaturized electronic components; and 3) floor to enterprise resource and execution systems that can collect, analyze and respond to rapidly changing production needs. While the automotive manufacturing industry has implemented sensors, robotics and computerized automation for decades, these systems largely are organized in a hierarchical fashion within individual data silos, and often in a closed, hard-wired network environment largely disconnected from IT and enterprise service-based networks. To complicate matters, automotive and industrial standard manufacturing equipment is still largely constrained by a large installed base of legacy workflow, equipment and standards. This paper explores some possible directions how automakers and suppliers will need to change and what considerations they will need to account for with respect to data into order to manufacture the next generation of connected and electrified vehicles.
Minarcin, Monika
Towards Self-Adaptive Fixturing Systems for Aircraft Wing Assembly2015-01-24939/15/2015
The aim of this work was to develop a new assembly process in conjunction with an adaptive fixturing system to improve the assembly process capability of specific aircraft wing assembly processes. The inherently complex aerospace industry requires a step change in its capability to achieve the production ramp up required to meet the global demand. This paper evaluates the capability of adaptive fixtures to identify their suitability for implementation into aircraft wing manufacturing and assembly. To understand the potential benefits of these fixtures, an examination of the current academic practices and an evaluation of the existing industrial solutions is highlighted. The proposed adaptive assembly process was developed to account for the manufacturing induced dimensional variation that causes significant issues in aircraft wing assembly. To test the effectiveness of the adaptive assembly process, an aircraft wing assembly operation was replicated on a demonstrator test rig. The experimental case study is described and positive initial test data is presented. The demonstrator achieved assemblies that were 0.129 mm and 0.114 mm from the actual target. These initial tests show that a repeatable process is obtainable, but a further increase in accuracy is required. Future work will be bring the system to a higher maturity level to allow for implementation into aircraft assembly processes.
Vaughan, DanBranson, DavidBakker, Otto JanRatchev, Svetan
Implementing the Hybrid Lean-Agile Manufacturing System Strategically in Automotive Sector2015-01-90835/1/2015
In order to strike a balance between cost and availability, the present study presents the strategic implementation of the hybrid lean-agile manufacturing system. The proposed implementation is based on literature review and statistical analysis. The study presents short term and long term proposed plans for implementing this newly developed system in a sustainable way. It shows how the strategic facet of the hybrid lean-agile manufacturing system addresses the key manufacturing competitive dimensions. The paper presents as well a cost-benefit analysis in comparison with the lean manufacturing system and agile manufacturing system based on the net present value. The study shows that the expectedly most efficient among the manufacturing systems is the Hybrid Lean-Agile Manufacturing System with normalized comparative improvement of about 58% and 42%, respectively. The study concludes through a statistical sample that about one third of the variation in successfully dealing with the sources of competitive advantage in automotive sector can be explained by adopting the strategic facet of the hybrid lean-agile manufacturing system. The study is limited to the automotive manufacturing sector. The paper would be of interest to the seekers for efficient manufacturing systems such as lean manufacturing practitioners and agile manufacturing practitioners.
Elmoselhy, Salah A.
Adaptive Manufacturing System2014-01-22739/16/2014
The ever increasing use of composites for aircraft components presents opportunities for new ways to process these parts. There are myriad benefits for use of composites in achieving aircraft performance goals. However, composites come with unique challenges as well. Some of these challenges impact the ability to produce accurate parts. Traditionally, such parts have been trimmed only while clamped in dedicated rigid tools that secure the part in the nominal shape. This results in significant investment in tooling design, production, maintenance, storage and, handling. As an alternative, PaR has developed its Adaptive Manufacturing System that incorporates a Robotic Fixture and Precision Motion Machine with an Integrated Process Head. The Robotic Fixture allows the entire family of parts to be managed with one fixture that remains within the machine footprint. The fixture is programmed to command 38 individual robots to assume appropriate poses and end effector configurations to accommodate over 400 different parts in the family that range in length from 0.5 to 20 meters. Once the part(s) is loaded in the fixture, the system automatically scans the part to determine the actual location and contour, as presented to the machine. The actual measurements are compared against reference data, which defines the nominal condition. This allows the machine to automatically develop adaptive tool paths that trim the part, so that the part will be the right size when constrained to its nominal condition. Trimming is done with abrasive waterjet, using multiple different catchers to accommodate different accessibility conditions. A spindle is also integrated into the same head as the waterjet and laser scanners, to accommodate hole drilling and edge chamfering. After the trimming operations are complete, the system washes and dries the part. A subsequent geometric inspection is performed using either a probe in the spindle, or the laser scanners. The inspection uses DMIS programming and results in an inspection report to go with the completed part. This paper will further describe the challenges and technology implemented in the development of this system.
Cunov, JamesHabermann, Charles J.
Automated Removal of Prepreg Backing Paper - A Sticky Problem2013-01-22899/17/2013
Automated solutions for manufacturing composite products based on prepreg often imply Automatic Fiber Placement or Automatic Tape Laying. These systems are generally associated with huge investments. For certain manufacturing applications it is interesting to investigate alternatives to find simpler and less costly automation. One example of an automated system could be the use of a standard industrial robot to pick single prepreg plies from an automated cutting machine and stack them to form a plane laminate. This paper is based on a case illustrating a product from the aircraft manufacturing industry. The case will demonstrate a pick and place concept on a general level and illustrate challenges that must be solved. The challenge selected to be the main focus for this paper is an automated process for backing paper removal. A literature review of different gripping technologies reveals several interesting technologies, and the most promising are tested for backing paper removal. The tests show that an automated removal process can be designed by using standard vacuum grippers in combination with mechanical clamping grippers. In order to lift the backing paper with a vacuum gripper an initial separation between the backing paper and prepreg is needed. This separation is most easily mechanically induced by bending the material. The proposed solution for automatic backing paper removal can be integrated in a manufacturing cell for manufacturing of the studied product.
Björnsson, AndreasLindback, Jan-ErikJohansen, Kerstin
Simulation at the Heart of an Automated Aerospace Manufacturing Process2006-01-31509/12/2006
The traditional use of simulation software in aerospace manufacturing applications has been as a pre-production tool for the validation of tool paths and the generation of robot programs. Once the process has been proven via simulation, the data is then transferred to the machine or robot and the production process executed. This is a linear approach in which the virtual and real systems are operated independently and in a serial manner. The current capabilities of offline programming (OLP) and simulation systems when combined with appropriate hardware in a flexible manufacturing environment now allow them to be used right at the heart of a manufacturing process, as an integral part of the manufacturing route. In a flexible manufacturing cell such as that developed at the University of Nottingham for the automated assembly and riveting of large aerostructures, a key driver is the need to reduce or eliminate complex and costly jigs and fixtures for part positioning. The use of simple non-precise support structures results in variation in the spatial relationship between the robot and the part or assembly. These variations are inherent in the nature of the parts, as a result of the additive manufacturing process and from the use of robots. The part position and orientation variation must be measured and accounted for in the robot program and the combination of a non-contact real-time metrology system and an OLP system linked together in a flexible cell allows this to happen as part of the manufacturing process. This results in a much closer coupling between the virtual part of the manufacturing process and the real part. This paper will describe the embedding of the simulation system at the heart of the robotic assembly and riveting cell at the University of Nottingham and will outline the ways in which the capabilities of the simulation system can be utilized to produce an innovative and highly flexible manufacturing system for the production of aerospace assemblies with significant geometrical variations.
Eastwood, S.Webb, P.
Use of Electromagnetic and Vacuum Forces on Aircraft Assembly2002-01-263010/1/2002
Decades ago our innovative grandfathers developed the first automated riveting machines based on hard automation using kinematics and tools attached to a C-frame. The C-frame serves multiple functions: First, it holds the upper and lower tools in fixed positions relative to each other; second, it translates upper active tooling forces to the lower tool; and third, it embraces the part placed between the upper and lower tool. C-frames and newly developed yoke, ring and gantry machines, used for low level (first, second) fuselage and wing assembly are growing in size to exorbitant proportions to satisfy requirements of larger and larger structures. High costs are dictated by massive kinematics and complex controls that provide stability, precision, and process speed. All this is mainly needed because we have to carry mechanical forces around the part, from upper to lower tool along the C-frame, gantry, yoke, bridge, etc. There are several other forces in nature (i.e. gravity, electricity, magnetism, pressure, vacuum, heat, atomic, friction, etc.) which can be considered and applied to machine design to achieve optimum and reliable results for minimal investments in machinery and floorspace. Analyzing alternative forces in search of more innovative assembly systems specifically for high level assembly where “embracing” parts (fuselage barrels, wing boxes) is no alternative, electromagnetic and vacuum forces were down-selected as the most promising option. The specific characteristics of magnetic flux capable of penetrating a part provides an ideal technique for generating clamping forces during drilling, fastener feeding, and the upsetting process. Electromagnet generating clamping force is easily integrated with a multi-function end effector moving on rails along structural joints performing fastening in sync with an internal tool. Vacuum systems capable of generating forces on part surfaces using suction cups and/or vacuum chambers, have the capability to attach/hold assembly systems on aircraft structures by part non intrusive means. Utilization of these new technologies in aircraft assembly enables the development of new innovative light-weight, flexible assembly systems, targeting high level fuselage and wing assembly. Principles and technologies needed for generating electromagnetic and vacuum forces for a prototype assembly system are discussed in this paper.
Sarh, Branko
Wing Manufacturing: Next Generation9856017/31/1998
Due to the part size and technological limitations of the available assembly equipment, traditional wing manufacturing has consisted of a three stage process. Parts are first manually tacked together in an assembly jig, They are then removed from the jig, rotated horizontally and craned into an automated fastening machine. Finally they are removed from the fastening machines and craned to a third station where the manual tacks are removed and the parts are prepped for final wing box assembly. With the advent of electromagnetic riveting (EMR) and the traveling yoke assembly machine this traditional approach has been replaced with single station processing. Wing panels and spars can now be automatically tacked together under continuous clamp up in their assembly jigs using EMR. This eliminates the requirement for disassembly, debur and cleaning required with the manual process. While the wing panels and spars remain rigidly held in their flying configuration by the assembly jig they are fastened with an articulated yoke. Tool tables are mounted to the bottom of a solid yoke to insure opposing head alignment. Assembly jigs are lined end to end to allow one machine to service multiple stations and further enhance productivity. In addition to efficiency improvements this new process improves product quality. The elimination of multiple crane moves and the manual tracking process greatly reduces the potential in process damage to the components. Since the parts are held rigidly in their assembly jigs during the entire fastening process, final panel and spar definitions are improved. Further, the use of EMR riveting has been demonstrated to provide superior fatigue to conventional process. Two recent case studies of this approach are presented. The E4000 assembly system went into production on the A320 program in early 1998. The E5000 spar assembly system, ASAT4, goes into production in mid 1998. These two system are evolutions of earlier systems introduced on the Airbus A340 and Boeing 767 programs respectively. These two systems include a number of new enhancements over past systems and demonstrate approaches to both high and low rate aircraft production.
Hartmann, JohnZieve, Peter
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