Browse Topic: Stamping

Items (225)
Bake Hardening Behavior of DP, TBF, and PHS Steels with Ultimate Tensile Strengths Exceeding 1 GPa2020-01-05364/14/2020
Third generation advanced high strength steels (AHSS) have been developed combining high strength and formability, allowing for lightweighting of vehicle structural components. These AHSS components are exposed to paint baking operations ranging in time and temperature to cure the applied paint. The paint baking treatment, combined with straining induced from part forming, may lead to increased in-service component performance due to a strengthening mechanism known as bake hardening. This study aims to quantify the bake hardening behavior of select AHSS grades. Materials investigated were press hardenable steels (PHS) 1500 and 2000; transformation induced plasticity (TRIP) aided bainitic ferrite (TBF) 1000 and 1200; and dual phase (DP) 1000. The number designations of these grades refer to minimum as-received ultimate tensile strengths in MPa. Paint baking was simulated using industrially relevant times and temperatures from 15 to 60 min and 120 to 200 °C, respectively. Samples were prestrained 0, 2, or 5 pct to replicate part forming. Bake hardening values ranging from 90 to 140 MPa were observed for DP and TBF grades that were prestrained 2 pct and baked at 170 °C for 20 min. However, ductility diminished for these steels when subjected to 5 pct prestrain with uniform elongations after baking decreasing to 1 pct in some instances. PHS steels, on the other hand, showed substantial increases in yield strength without prestrain. Increases of 122 and 175 MPa were recorded for PHS 1500 and PHS 2000, respectively, following baking at 160 °C for 60 min. However, ultimate tensile strengths decreased due to reduced strain hardening, while total elongations decreased slightly.
Blesi, Brandon W.Smith, CharlesMatlock, David K.De Moor, Emmanuel
A Non-Contact Overload Identification Method Based on Vehicle Dynamics2019-01-04904/2/2019
The vehicle overload seriously jeopardizes traffic safety and affects traffic efficiency. At present, the static weighing station and weigh-in-motion station are both relatively fixed, so the detection efficiency is not high and the traffic efficiency is affected; the on-board dynamic weighing equipment is difficult to be popularized because of the problem of being deliberately damaged or not accepted by the purchaser. This paper proposes an efficient, accurate, non-contact vehicle overload identification method which can keep the road unimpeded. The method can detect the vehicle overload by the relative distance (as the characteristic distance) between the dynamic vehicle's marking line and the road surface. First, the dynamics model of the vehicle suspension is set up. Then, the dynamic characteristic distance of the traffic vehicle is detected from the image acquired by the calibrated camera based on computer vision and image recognition technology. The data error caused by the vehicle vibration can be reduced by the filter set up in this paper. Finally, the actual axle load of the vehicle can be obtained combined with the established model, which can be compared with the recorded standard data to detect overload vehicles. In this paper, the real vehicle test was carried out with Dong Feng Aeolus S30. The results show that the characteristic distance identification absolute error and relative error can respectively be controlled within 42.2mm and 3.18%, and the vehicle load identification precision can be 96.0%. The method above can effectively improve the efficiency of the overload identification and has certain guiding significance for maintaining the safety of intelligent transportation.
Zhou, DaolinTan, GangfengDing, YiranYu, ShiminMa, XiaofeiWang, ShuaiWang, Zhenyu
ABSTRACT This paper describes the flight test of a mounted touchscreen device in a UH-60 helicopter. The device assists crew chiefs in their fuel management tasks and provides situational awareness information regarding the route/flight plan, map data, external camera displays, publications and aircraft system information. The touchscreen tested was a 10.5" display and used Projected Capacitive for touch input. It was surrounded by 28 bezel switches. Eight current crew chiefs performed tasks using the device in flight. The participants wore gloves. Flight test evaluation results show that the subjects used and preferred the bezel switches over soft buttons on the touchscreens. Results also show that 16% percent of touchscreen presses required multiple presses to register the touch. Vibration did not appear to cause a problem with using the touchscreen. Gloves did present a problem in using the Projected Capacitive touchscreen.
Schutte, Paul
Effect of E-Modulus Variation on Springbackand a Practical Solution2018-01-06304/3/2018
Springback affects the dimensional accuracy and final shape of stamped parts. Accurate prediction of springback is necessary to design dies that produce the desired part geometry and tolerances. Springback occurs after stamping and ejection of the part because the state of the stresses and strains in the deformed material has changed. To accurately predict springback through finite element analysis, the material model should be well defined for accurate simulation and prediction of stresses and strains after unloading. Despite the development of several advanced material models that comprehensively describe the Bauschinger effect, transient behavior, permanent softening of the blank material, and unloading elastic modulus degradation, the prediction of springback is still not satisfactory for production parts. Dies are often recut several times, after the first tryouts, to compensate for springback and achieve the required part geometry. In this study, the effect of Young’s modulus (E-modulus) on springback is investigated. Current challenges in determination of E-modulus through tensile test are discussed and a practical method is proposed which has the potential to improve springback prediction after the first die tryout. In this method, the unloading elastic modulus is adjusted by measuring the springback of the part produced during the first tryout and comparing it with finite element (FE) simulation results. The unloading elastic modulus obtained from this method is called the “apparent E-modulus”. This method is applied to three bending cases: a wipe bending, a U-drawing, and a 3-D crash forming of an actual production part. Results show that the springback can be predicted fairly accurate using the apparent E-modulus and a simple isotropic hardening model.
Fallahiarezoodar, AliGoertemiller, CliffKatre, AananditaAltan, Taylan
Replacing Press Hardenable Steel with 980 MPa Generation 3 Steel for Automotive Pillars2018-01-01174/3/2018
Press hardenable ultra high strength steel (UHSS) is commonly used for automotive components to meet crash requirements with minimal mass addition to the vehicle. Press hardenable steel (PHS) is capable of forming complex geometries with deep sections since the forming takes place at elevated temperatures up to 900 degrees Celsius (in the Austenitic phase). This forming process is known as hot-stamping. The most commonly used PHS grade is often referred to as PHS1500. After hot-stamping, it is typically required to have a yield strength greater than 950 MPa and a tensile strength greater than 1300 MPa. Most automotive design and material engineers are familiar with PHS, the hot-stamping process, and their capabilities. What is less known is the capability of 3rd Generation advanced high strength steels (AHSS) which are cold stamped, also capable of forming complex geometry, and are now in the process of, or have recently completed, qualification at most automotive manufacturers. This paper will show that U. S. Steel’s Generation 3 steel with 980 MPa minimum tensile strength (980GEN3) has comparable crash performance to PHS1500 when used for automotive body-in-white (BIW) Pillars in a sedan. This paper will also show that these 980GEN3 BIW Pillars can achieve the same complex geometry as PHS1500, that the springback can be predicted and controlled, and that prototype parts can be assembled into a vehicle build and physically crashed without issues. Furthermore, correlation between cold stamped 980GEN3 BIW Pillars and forming simulation results will also be discussed.
McKune, PaulKhutorsky, AlexButala, Kapil
Effects of AHSS Sheared Edge Conditions on Crash Energy Absorption in Component Bend Test2018-01-01134/3/2018
Edge fracture of advanced high strength steels (AHSS) can occur in both the stamping process and the crash event. Fracture due to poor sheared edge conditions in the stamping process was reduced with a recently developed optimal shearing process for AHSS. Currently, the improvement in the energy absorption due to the improved edge condition during crashes performed under different loading conditions had not been closely verified. The purpose of this study is to design and build a miniature component of AHSS and a three-point bending test for investigating the influence of various conditions of the sheared edge on the energy absorption in crashes. AHSS including DP600, TRIP780, DP980 and DP1180 were selected in the study. A small channel component was developed and fabricated using DP980 to simulate key features of the B-pillar. The exposed non-constrained, as-sheared edge was subject to stretch bending forces in three-dimensional space during the three-point bending test. Two bottom rollers equipped in the three-point bending test allowed the test specimen to bend freely without generating extra friction force between the test material and tooling. Previously developed shearing parameters were fine-tuned for generating the test specimen on the flexible shearing machine and then compared to the specimens made by water jet cutting and laser cutting. A life cycle analysis was also conducted by FEA to evaluate the new design of the shear blade. The experiment results indicate the improvement of the sheared edge conditions can also increase the material energy absorption in crashes. The laser cut sample has the best energy absorption capability, while the conventional cutting edge shows the worst. In addition to the three-point bending test, a wedge bend test was conducted on the flat sample and reached a similar energy absorption trend as in the component bend test. The wedge bend test on flat sample is recommended for baseline comparison in material bendability and crash energy absorption capability among different advanced high strength steels.
Shih, Hua-ChuChen, Guofei
Spring Assistance (Energy-Swing) in an Electro Mechanical Brake2017-01-25179/17/2017
On Electro-Mechanical Brakes (EMB) spring-support can be necessary for releasing the brake without electrical energy. Advantageous brake-configurations can make use of the spring over the whole actuation range during engage and release. Such optimized spring support is known as “energy-swing. Under loss-less conditions the spring force could be in permanent equilibrium with the force required to press the pad, i.e. the brake could be controlled without actuation energy. In reality this will not be fully achievable as actuation losses and different operational conditions need to be covered. Still, significant advantages can be gained. The EMB of Vienna Engineering (VE) fulfills a key condition for energy-swing as it facilitates using the spring for engage- and release-support. Car brakes must release automatically when power is off. Consequently, spring-induced engage-support must always be smaller than release-forces and release-support must ensure overcoming mechanical resistance. The VE-EMB can fulfill the requirements while maximizing the benefits by introducing a cam /rocker mechanism. With realistic assumptions of losses, tolerances and operational influences the potential of the mechanism in terms of saving actuation energy, reducing actuator motor power and actuation timing improvement must be questioned. Besides, the related increase of complexity needs to be addressed. This paper discusses the issues by comparing a VE-EMB without spring, the cam-rocker design and the simpler but less configurable lever-pushing method.
Putz, Michael HerbertZipper, Thomas
Modeling and Simulation of Compression Molding Process for Sheet Molding Compound (SMC) of Chopped Carbon Fiber Composites2017-01-02283/28/2017
Compression molded SMC composed of chopped carbon fiber and resin polymer which balances the mechanical performance and manufacturing cost presents a promising solution for vehicle lightweight strategy. However, the performance of the SMC molded parts highly depends on the compression molding process and local microstructure, which greatly increases the cost for the part level performance testing and elongates the design cycle. ICME (Integrated Computational Material Engineering) approaches are thus necessary tools to reduce the number of experiments required during part design and speed up the deployment of the SMC materials. As the fundamental stage of the ICME workflow, commercial software packages for SMC compression molding exist yet remain not fully validated especially for chopped fiber systems. In the present study, SMC plaques are prepared through compression molding process. The corresponding simulation models are built in Autodesk Moldflow with the same part geometry and processing conditions as in the molding tests. The output variables of the compression molding simulations, including press force history and fiber orientation of the part, are compared with experimental data. Influence of the processing conditions to the fiber orientation of the SMC plaque is also discussed. It is found that generally Autodesk Moldflow can achieve a good simulation of the compression molding process for chopped carbon fiber SMC, yet quantitative discrepancies still remain between predicted variables and experimental results.
Li, YangXu, HongyiDahl, JeffreyZeng, DanielleSu, XumingMirdamadi, MansourChen, Zhangxing
An Investigation of Deformation Effects on Phase Transformation in Hot Stamping Processes2016-01-03614/5/2016
To reduce the fuel consumption as well as to improve the crash safety of vehicles, the usage of hot stamping parts is increasing dramatically in recent years. Aisin Takaoka has produced hot stamping parts since 2001 and has developed various technologies related to Hot Stamping. In an actual hot stamping process, parts with insufficient strength could be produced sometimes at a prototyping phase, even under the proper forming conditions. In order to understand these phenomena, in this paper, phase transformation in a boron steel 22MnB5 under various cooling rates were investigated and the effects of pre-strain conditions on the phase transformations were characterised. Uniaxial tensile specimens were stretched under isothermal conditions to different strain levels of 0-0.3, at strain rates of 0.1-5.0/s and deformation temperatures of 650-800°C. A dilatometer was used to measure the dimensional changes of the specimen to rationalize the phase transformation of the boron steel during rapid cooling after deformation. The results showed that the deformation at austenite phase causes the reduction in martensitic phase transformation. For a certain strain level, deformation applied at a lower temperature and a higher strain rate would result in less amount of martensitic phase transformation. In addition, the relations between hot stamping conditions and Vickers hardness, which are normally used as a daily quality check in the industry, are also presented in the paper.
Matsumoto, TakekiLi, NanShi, XinLin, Jianguo
Innovative Door Design for Commercial Vehicles2014-01-24119/30/2014
Design of body structures for commercial vehicles differs significantly from automotive due to government, design and usage requirements. Specifically, heavy truck doors are not required to meet side impact requirements due to their height off the ground as compared to automobiles. However, heavy truck doors are subjected to higher loads, longer life, and cannot experience permanent deformation from overload events. Aluminum has been used intensively in commercial vehicle doors and cab structures for over 50 years by several different manufacturers in North America. It has been only in the last few years that aluminum has appeared in automotive door structures other than in high-end luxury vehicles. Commercial vehicle customers are expecting the same features found in premium automobiles resulting in opportunities to learn from each other's designs. In order to optimize the strength and weight of a commercial vehicle door, a new aluminum intensive structure was developed. The new structure featured a unique architecture that was the first in the industry to use a multi-cavity aluminum extrusion joined to stamped sheet reinforcements in order to provide a direct load path between the hinges and the latch. The shape of the extrusion also allows the use of a one piece glass and door mounted mirror. The “barn door” architecture of the inner structure of the door allowed for gauge optimization of the both the inner and outer stampings, the two largest and heaviest components of the assembly. Additionally, the use of an extrusion allowed for a single drop glass for improved visibility and the ability to use a door mounted mirror with only one extra reinforcement. Overall the design architecture used in the new doors provide best in class structural performance, sealing and features normally found in luxury automobiles for the first time in the heavy truck industry.
Auger, MarcPlourde, LarryTrumbore, MelissaManuel, Terry
Thermoplastic composites offer many attractive characteristics such as no shelf life, high fracture toughness, high temperature resistance, recyclability etc. The short coming of thermoplastic composites is their high viscosity, even at processing temperature. Due to the high viscosity, techniques for the manufacturing of thermoplastic composite have been limited to molding processes such as compression molding, high temperature stamping, where high temperature, high pressure and long duration are used. The advent of automated fiber placement machine brings forward possibilities to manufacture of large thermoplastic composite components. This is due to the fact that heating and compaction is done on the go directly on the surface of the substrate, and the flexibility of the feeding head to conform to the shape of the mold. It is in the spirit of exploration for new manufacturing possibilities that Bell Helicopter has supported an inter industry- university project for the development of thermoplastic composite cones aimed at helicopter tail boom applications. The cone represents a segment of the helicopter tail boom. It is made using carbon/PEEK material and automated fiber placement. The work consists of the Determination of the lay-up sequence to address the loads, the Development of the manufacturing processes, the Measurement of temperature variation during the making of a ring, the Checking of the quality of the cone, Development of tube bending test set up, Development of theoretical calculations to determine the buckling load of the cone subjected to bending, Testing the cone under bending load, and Comparing the experimental buckling with calculated buckling load.
Hoa, SuongShadmehri, FarjadCai, XiaoSimpson, JeffHojjati, MehdiHubert, PascalQuinlan, ErinBeaulieu, PierreDion, Michel
Integrated CAE Methods for Perceived Quality Assurance of Vehicle Outer Panels2014-01-03664/1/2014
Oil canning and initial stiffness of the automotive roofs and panels are considered to be sensitive customer ‘perceived quality’ issues. In an effort to develop more accurate objective requirements, respective simulation methods are continuously being developed throughout automotive industries. This paper discusses a latest development on oil canning predictions using LS-DYNA® Implicit, including BNDOUT request, MORTAR contact option and with the stamping process involved, which resulted in excellent correlations especially when it comes to measurements at immediate locations to the feature lines of the vehicle outer panels. Furthermore, in pursuit of light-weighting vehicles with thinner roofs, a new CAE method was recently developed to simulate severe noise conditions exhibited on some of developmental properties while going through a car wash. This paper introduces such a method to discuss Fluid Structure Interaction (FSI) approach using an Arbitrary Lagrangian Eulerian (ALE) formulation in LS-DYNA® for vehicle roof car wash boom noise prediction. This CAE method was developed to simulate force behavior from airflow as the car wash air blowers are expelling high speed air at the vehicle roofs during car wash. LS-DYNA® was proven an appropriate tool to precisely simulate popping noises by creating instantaneous local instabilities - recoverable/non-recoverable - and continuous fluttering of the roof. This paper additionally briefs the history of oil canning CAE method developments from inaccurate hand push evaluation to approaches using MSC Nastran® to Abaqus/Standard®, and then the final evolution to LS-DYNA® Implicit to provide optimized vehicle solutions.
Jang, Jaehyuk
A Fastener Analysis Addressing Various Types of Misfit and Its Damage Life Calculations2013-01-23129/17/2013
In a fastening system when there is a small misalignment of the holes, the holes are enlarged to align the axes and a next size fastener is used to fit the joint. But when the misalignment is large then the enlargement need to be proportionally large. In this case a bushing is press fit onto the hole to handle the fastening. If we press fit a bushing, it generates residual stresses in the panel. These residual stresses reduce the damage life of the components on which the bushings were press fit. In the aircraft engine nacelle components the damage life is very critical in various failure conditions such as fan blade out condition, wind milling and bird strike. It increases the flight time in these events. Here four different case studies were considered to study the damage life of the aircraft components made of Aluminum or composite material. Case-study 1 (Aluminum panel and full ring bushing): A knock down factor to the damage life for the component material (Aluminum - in this case) is tabulated in this paper to account for the pre stresses added to the nacelle components due to the press fit of the bushing, which is added due to the misalignment of the holes. Case-study II (Aluminum panel and split ring bushing): An attempt is made to reduce the residual stresses on the Aluminum panel containing the fastening system for the non critical components. Here a split ring is used to press fit into the enlarged hole [1] in place of the bushing used in the Case-study I. The split ring reduces the tolerance requirements and decreases the manufacturing cost & time. This also reduces the stress on the panel and contains the fastening system. Case-study III (Composite panel and full ring): In this case- study the bushing is press fit into composite sandwich panel instead of the Aluminum panel that is used in previous Case-studies for a treatment on the misalignment. The residual stresses developed are used to recalculate the damage life of the composite panel. Also a knock down factor chart is developed for the fiber with +45. −45, 0 and 90 degree ply orientations. Case-study IV (Composite panel and split ring): In this case-study the split ring is used instead of full ring bushing on to the composite panel. These studies can be used to modify the damage number for the given material of any part subjected to a peak pre stresses between 4 to 12 Ksi. By computing the modified damage number, the RUL (Rest of Useful life) number can be computed. This helps in accessing the health of the part as well as can decide in reusing a part in non critical system as a carry over part. The split ring bushing is studied only to be used in the non-critical parts or in other systems such as automotive or consumer industrial components. For the critical aircraft components the added residual stresses will necessitate to compute the modified margin of safety as well as the modified damage life for the part.
Anandan, Vailore
Integrating Manufacturing Pre-Stress in FEA Based Road Load Fatigue Analysis2013-01-12044/8/2013
Most manufacturing and assembly processes like stamping, clamping, interference fits introduce a pre-stress condition in components or assemblies. Very often these stresses are high enough and alter the mean stress state resulting in significant effect on fatigue life performance and thus cannot be ignored. If the pre-stress is compressive, it will increase the allowable stress range and improve fatigue life performance; on the other hand if these stresses are tensile, they will decrease the allowable stress range resulting in a degradation of fatigue life. At times it becomes critical to effectively introduce the pre-stress condition in order to accurately represent the stress state in an FEA based durability simulation. Accounting for the pre-stress state in FEA based constant amplitude loading fatigue life simulation is relatively straight forward, but when it comes to random variable amplitude multi-channel loads simulation, the problem becomes more complicated. In this paper, a method to include the pre-stress effect on vehicle components or assemblies and perform FEA based fatigue analysis when subjected to random road loads is practiced. This paper outlines the procedure used to calculate the pre-stress followed by the modified material curves and eventually performs FE based fatigue analysis using vehicle road load data. A couple of case studies are also included that will demonstrate the correlation of this FE based method to the physical component test results.
Qin, Wenxin
Analytical Method to Determine Press-fit Tolerance between Torque Carrying Members2012-01-19969/24/2012
This paper deals with an analytical method to calculate the press-fit tolerance and fits between gears and shaft for automotive applications. The relative interferences increase sharply in the small diameter range, therefore one must be especially careful when designing small diameter joints. The strength of press-fit depends on the amount of relative interference; extreme interference leads to excessive contact stresses between the gear and shaft eventually leading to failure. Too little interference leads to slippage of gear on the shaft. In the press fit connection a shaft's spline rolling operation and gear internal broaching is eliminated. It is more economical than a conventional spline connection. Press fit connections are used in various transmission between a shaft and a gear. They are used in 6 speed transmission to 9-speed transmission for (German based Vehicle Manufacturer) heavy and light commercial vehicle company. In India 5-speed transmission to 9-speed transmission for heavy and light commercial vehicle companies, also uses press fit connections. The strength of the press fit joint is directly proportional to the coefficient of the friction between the mating parts. The strength depends upon the pressure at the contacting surface, surface micro irregularities and material properties. Adequate surface finish of the mating component is an essential condition for the strength of the pressed connection. For connections undergoing heating during the operation, the influence of the temperature upon the fit must be considered. Therefore it is challenge to design an optimum press fit joint; a fine balance need to be determined while calculating interferences for the press-fit connection.
Bhat, Muralidhar SuryanarayanJadhav, Sagar
This test method is designed to determine the suitability of a painted or unpainted fiberboard for application involving creasing and bending. The specific purpose of the test is to determine whether a given material, properly creased, can be bent along the impressed crease without objectionable failure on the surface of the bend.
Textile and Flexible Plastics Committee
The Impact of Advanced Material Simulation Parameters in Press Shop Operations Using Mild Steel Grades2010-01-09924/12/2010
Forming simulation is a widely used tool to estimate production forming capabilities. During the last three to four years the prediction of process robustness by sensitivity analysis has been developed for industrial applications. The change of material parameters is one key figure and has a large impact on the final findings. Thus the user has to ensure that the variations done are in correlation with real material behaviour and the selected numerical model is reliable. Up to now the permitted changes in modelling are seldom secured by real measurements, especially when more advanced material models and hardening options are applied. Various materials chosen out of the production process for mild steel grades have been investigated for their mechanical properties using different tests. The limits of failure are defined by a reduced number of Nakajima tests to predict the forming limit curve (FLC). All data is prepared in the same manner to meet simulation program needs. The calibration of yield locus by solely tensile tests and in combination with hydraulic bulge tests gives a first estimation of possible compromises in data preparation. More advanced material calibration strategies allow a better fit of the models to the measured values (Hill ´90, Banabic 2005). Furthermore some principles can be noticed for yield locus calibration in biaxial stress space. The experimentally measured forming limits are compared to the TKS-in-house regression formula, Keeler´s approach and other models. Finally simplified state of the art simulations (input tensile test) are compared to simulation results gained with more accurate material data input parameters for yield locus and hardening for different complex parts. The resulting difference in the feasibility findings are then discussed with respect to a virtual process design chain.
Kessler, LutzGerlach, JoergBeier, ThorstenLinnepe, Michael
Robust Optimization of Drawbead Forces for a B-pillar Stamping2009-01-09804/20/2009
Many uncertainties exist in the sheet metal stamping such as the variation of incoming material properties, die and press setup conditions, long-term tool wear and degradations. They are interacting in a way to make the process less robust, thus contributing to increased scrap rates and more unscheduled downtime. This paper presents a new approach for the die design optimization where these uncertainties are taken into account. A Tailor-Welded B-pillar consisting of 1.65mm DP600 and 0.9mm DDQ is selected as the focal part to demonstrate the new design process. The study is divided into two phases. The focus of the first phase is to understand the complexity of the formability window and determine effective optimization techniques under deterministic conditions. It is found that the formability window is highly nonlinear, or even discontinuous if a global objective function such as the Maximum Failure Factor is used. It is therefore more advantageous to adopt a regional approach where the split-prone zones and wrinkle-prone zones are identified. Optimization can then take place for each region with a multi-objective approach using the Non-dominated Sorting Genetic Algorithm (NSGA-II). The second phase takes into account the stamping uncertainties, and both the formability values and their deviations are optimized simultaneously for robustness. It is demonstrated that the robust optimization under uncertainties is able to reduce output variability while maintaining the same level of “optimal” performance as compared with deterministic optimization.
Li, DayongChang, TonyWang, Yu-WeiXia, Z. Cedric
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