Springback experimental evaluation and validation of aircraft industry sheet metal

M. Pandian, M. Gupta
{"title":"Springback experimental evaluation and validation of aircraft industry sheet metal","authors":"M. Pandian, M. Gupta","doi":"10.5958/2454-762X.2018.00022.7","DOIUrl":null,"url":null,"abstract":"The tendency of the metal to regain its original shape will result in the spring back when it is being formed to make aircraft components like outer body panels and brackets. When spring back occurs, the components will not meet the requirements of the design and there will be a need for shims to fit the component into place. This will lead to increase in weight, fabrication cost and also the assembly line time. So the Finite-Element Analysis (FEA) is used to accurately predict this deflection so that manufacturing processes can be optimized to produce a perfect output with least deviations from the design. This thesis bridges a relation between the experimentally evaluated spring back and FEA calculated spring back. Also in order to validate the FEA Analysis regression analysis has been performed. Variations have been tabulated and graphed as it bridges the gap between experimentally evaluated spring back and analysis of the design. INTRODUCTION Aircraft construction involves a wide range of materials. Out of these sheet metal plays a major role. Sheet metal aircraft construction is the most prevalent aircraft construction material by all measures, used extensively from jetliners to light, single engine airplanes and kits over the past five decades. Furthermore, virtually all other aircraft types use sheet-metal construction to some degree whether an instrument panel on a composite aircraft, or a firewall on a wood or steel tube and fabric design. New and modern metal alloys and materials have allowed aviation technology to advance, and is the reason it continues to dominate over other aircraft building methods. Steel’s and Aluminum’s unique combination of properties makes it one of the most versatile engineering and building materials in existence:  Low weight / high strength relationship.  Corrosion resistance, especially with newer alloys and modern primers.  Low cost and widespread availability. The Bending process is the forming of sheet metal where angled or other shaped parts are produced. The process involves the uniform straining flat metal sheets around a linear axis, but it also may be used to bend tubes, drawn profiles bars, and wire. In bending, the plastic state is brought by a bending load. In fact, one of the most common processes for sheet metal forming are bending, which is used not only to form pieces such as L, U or V-profiles. Bending has the greatest number of applications in the automotive, aircraft and defense industries and for production of other sheet metal products. Typical examples of sheet-metal bends are illustrated in Fig 1. The basic characteristic of bending is tensile elongation on the outer surface and compression on the inner surface as shown Fig 1. Fig 1: Typical examples of sheet metal bend parts. The entire stress-strain curve is transverse, elastic stresses result in spring back and the residual stress pattern. Here, the bend radius Ri is measured on the inner surface of the bent piece. The bend angle φ is the angle of the bent piece and T is the material thickness. In bending process, since the outer fibers of the material are in tension and the inner fibers are in compression, theoretically the strain values on the outer and inner fibers are equal in magnitude and are given by the following equation: [Gupta*, 2.(9): September, 2015] ISSN 2349-6193 Impact Factor (PIF): 2.243 IJESMR International Journal OF Engineering Sciences & Management Research http: // www.ijesmr.com © International Journal of Engineering Sciences & Management Research [43] e0= e1 = 1 ( 2R T )+1 Experimental research indicate that this formula is more precise for calculating the deformation of the inner fibers of the material, e1, than for the deformation of the outer fibers, e0. The deformation in the outer fibers is notably greater, that is why neutral fibers move towards the inner side of the bent piece. As Ri/T ratio decreases, the bend radius becomes smaller; the tensile strain at the outer fibers increases and the Material eventually cracks. LITERATURE SURVEY Since sheet metal forming industry has become one of the major manufacturing centers for automobile and aerospace and defense industries, the popularity of sheet metal products is attributable to their light weight, great interchangeability, good surface finish, and low cost. There has been a growing interest during the past decade in using finite element method for Springback prediction following forming of arbitrary shapes. While it is apparently simple in concept, the prediction of Springback has proven challenging for a variety of reasons, including numerical sensitivity, physical sensitivity, and poorly characterized material behavior under reverse loading and unloading conditions. Springback of sheet metal parts after forming causes deviation from the designed target shape and produce downstream quality problems as well as assembly difficulties. Its economic impact in terms of delayed production, tooling revision costs, and rejection of unqualified parts is estimated to exceed $50million per year in the U.S. automotive industry alone. It is obvious that controlling Springback is a vital concern in manufacturing.Several studies has been done for past decades in order to develop Springback reduction and compensation methods. S. Nishino et al.[4] examined a new method of predicting a shape fixation property by combining free bending test data with the results of the computer simulations conducted using the finite element method (FEM). With the increased use Finite Element Simulation in tooling departments, the forming analyses of sheet metal components are used more frequently in the design feasibility studies of production tooling. These computer based tools allow the design engineer to investigate the process and material parameters controlling the material floe over the die surfaces. Several studies were done in past decade. M. Firat [17] studied U-Channel forming analysis to predict Springback. He established a kinematic hardening model based on additive back stress form in order to improve the predicted sheet metal deformation response .S.K.Panthi et al. [18] were also studied on a large deformation algorithm based on Total-Elastic-Incremental-Plastic Strain (TEIP) which was used for modeling atypical sheet metal bending process. The process involves large strain, rotation as well as Springback. N.Narasimham et al. [19] aimed to introduce a coupled explicit to-implicit finite element approach for predicting Springback deformations in sheet metal stamping that can be utilized for minimizing die prototype design time. In this study, they have utilized the explicit method initially to analyze the contact based forming operation of stamping process. Then an implicit solution has been performed to simulate the Springback developing in a blank after the forming pressure removed. They have coupled ANSYS/LS-DYNA explicit and ANSYS implicit codes to solve sheet metal forming processes that involves a high degree of Springback. One of the important studies of finite element analysis of Springback in bending was done by V. Esat [20]. In the mentioned work, V. Esat et al. developed a finite element simulation in order to simulate Springback by means of a Springback factor using commercially available finite element program. They reached a good agreement between the finite element simulation and empirical data. Their finite element model is based on 2-D shell elements and Chung-Hulbert dynamic implicit as time integration scheme. They used penalty method on analytically defined rigid bodies to handle contact algorithm. D.W.Park et al. [22] proposed a new shell element to improve accuracy and efficiency of Springback simulation by describing complicated bending deformation accurately. They applied the new element both implicit Finite Element Method and explicit Finite Element Method to conduct Springback simulation. Many studies had been carried out on different perspectives of Springback. Micari et al. [33] presented a Springback prediction technique in three dimensional stamping processes which is based on a combined approach in which an explicit finite element code has been employed to simulate the forming phase while a traditional implicit procedure has been used to analyze the Springback phase. Gauand Kinzel [34] performed an experimental study for determining the Bauschinger Effect on Springback predictions which seems very significant in wipe bending operations. Since Springback is a vital concern in manufacturing industry, beyond evaluating and simulating attempts of Springback, some researchers studied the parameters that effect Springback in sheet metal forming operations in order to control these disturbing parameters. [Gupta*, 2.(9): September, 2015] ISSN 2349-6193 Impact Factor (PIF): 2.243 IJESMR International Journal OF Engineering Sciences & Management Research http: // www.ijesmr.com © International Journal of Engineering Sciences & Management Research [44] FACTORS AFFECTING BENDING Bend radius Ri, is one of the most important parameter which affects bending operations of sheet metals. The bend radius in bending operations always pertains to the inside radius of bend. Minimum bend radius is dependent on the material thickness and the mechanical properties of the material. Minimum bend radii vary for various metals; generally, most annealed metals can be bent to a radius equal to the thickness, T and sometimes to T/2, for a given bend angle and bend length. Bend angle is another crucial factor in bending operations. As the bend angle becomes larger, especially with bend angles over 90°, many difficulties arise. In this case, the amount of bend radius become more critical and the material hardness becomes more detrimental to the success of the bending process. In bending process, some deformations occur in the bent-up region of the work piece depending on the dimensions of the work piece, bend angle, and bend radius. As th","PeriodicalId":14491,"journal":{"name":"Invertis Journal of Science & Technology","volume":"93 1","pages":"165"},"PeriodicalIF":0.0000,"publicationDate":"2018-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Invertis Journal of Science & Technology","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.5958/2454-762X.2018.00022.7","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
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Abstract

The tendency of the metal to regain its original shape will result in the spring back when it is being formed to make aircraft components like outer body panels and brackets. When spring back occurs, the components will not meet the requirements of the design and there will be a need for shims to fit the component into place. This will lead to increase in weight, fabrication cost and also the assembly line time. So the Finite-Element Analysis (FEA) is used to accurately predict this deflection so that manufacturing processes can be optimized to produce a perfect output with least deviations from the design. This thesis bridges a relation between the experimentally evaluated spring back and FEA calculated spring back. Also in order to validate the FEA Analysis regression analysis has been performed. Variations have been tabulated and graphed as it bridges the gap between experimentally evaluated spring back and analysis of the design. INTRODUCTION Aircraft construction involves a wide range of materials. Out of these sheet metal plays a major role. Sheet metal aircraft construction is the most prevalent aircraft construction material by all measures, used extensively from jetliners to light, single engine airplanes and kits over the past five decades. Furthermore, virtually all other aircraft types use sheet-metal construction to some degree whether an instrument panel on a composite aircraft, or a firewall on a wood or steel tube and fabric design. New and modern metal alloys and materials have allowed aviation technology to advance, and is the reason it continues to dominate over other aircraft building methods. Steel’s and Aluminum’s unique combination of properties makes it one of the most versatile engineering and building materials in existence:  Low weight / high strength relationship.  Corrosion resistance, especially with newer alloys and modern primers.  Low cost and widespread availability. The Bending process is the forming of sheet metal where angled or other shaped parts are produced. The process involves the uniform straining flat metal sheets around a linear axis, but it also may be used to bend tubes, drawn profiles bars, and wire. In bending, the plastic state is brought by a bending load. In fact, one of the most common processes for sheet metal forming are bending, which is used not only to form pieces such as L, U or V-profiles. Bending has the greatest number of applications in the automotive, aircraft and defense industries and for production of other sheet metal products. Typical examples of sheet-metal bends are illustrated in Fig 1. The basic characteristic of bending is tensile elongation on the outer surface and compression on the inner surface as shown Fig 1. Fig 1: Typical examples of sheet metal bend parts. The entire stress-strain curve is transverse, elastic stresses result in spring back and the residual stress pattern. Here, the bend radius Ri is measured on the inner surface of the bent piece. The bend angle φ is the angle of the bent piece and T is the material thickness. In bending process, since the outer fibers of the material are in tension and the inner fibers are in compression, theoretically the strain values on the outer and inner fibers are equal in magnitude and are given by the following equation: [Gupta*, 2.(9): September, 2015] ISSN 2349-6193 Impact Factor (PIF): 2.243 IJESMR International Journal OF Engineering Sciences & Management Research http: // www.ijesmr.com © International Journal of Engineering Sciences & Management Research [43] e0= e1 = 1 ( 2R T )+1 Experimental research indicate that this formula is more precise for calculating the deformation of the inner fibers of the material, e1, than for the deformation of the outer fibers, e0. The deformation in the outer fibers is notably greater, that is why neutral fibers move towards the inner side of the bent piece. As Ri/T ratio decreases, the bend radius becomes smaller; the tensile strain at the outer fibers increases and the Material eventually cracks. LITERATURE SURVEY Since sheet metal forming industry has become one of the major manufacturing centers for automobile and aerospace and defense industries, the popularity of sheet metal products is attributable to their light weight, great interchangeability, good surface finish, and low cost. There has been a growing interest during the past decade in using finite element method for Springback prediction following forming of arbitrary shapes. While it is apparently simple in concept, the prediction of Springback has proven challenging for a variety of reasons, including numerical sensitivity, physical sensitivity, and poorly characterized material behavior under reverse loading and unloading conditions. Springback of sheet metal parts after forming causes deviation from the designed target shape and produce downstream quality problems as well as assembly difficulties. Its economic impact in terms of delayed production, tooling revision costs, and rejection of unqualified parts is estimated to exceed $50million per year in the U.S. automotive industry alone. It is obvious that controlling Springback is a vital concern in manufacturing.Several studies has been done for past decades in order to develop Springback reduction and compensation methods. S. Nishino et al.[4] examined a new method of predicting a shape fixation property by combining free bending test data with the results of the computer simulations conducted using the finite element method (FEM). With the increased use Finite Element Simulation in tooling departments, the forming analyses of sheet metal components are used more frequently in the design feasibility studies of production tooling. These computer based tools allow the design engineer to investigate the process and material parameters controlling the material floe over the die surfaces. Several studies were done in past decade. M. Firat [17] studied U-Channel forming analysis to predict Springback. He established a kinematic hardening model based on additive back stress form in order to improve the predicted sheet metal deformation response .S.K.Panthi et al. [18] were also studied on a large deformation algorithm based on Total-Elastic-Incremental-Plastic Strain (TEIP) which was used for modeling atypical sheet metal bending process. The process involves large strain, rotation as well as Springback. N.Narasimham et al. [19] aimed to introduce a coupled explicit to-implicit finite element approach for predicting Springback deformations in sheet metal stamping that can be utilized for minimizing die prototype design time. In this study, they have utilized the explicit method initially to analyze the contact based forming operation of stamping process. Then an implicit solution has been performed to simulate the Springback developing in a blank after the forming pressure removed. They have coupled ANSYS/LS-DYNA explicit and ANSYS implicit codes to solve sheet metal forming processes that involves a high degree of Springback. One of the important studies of finite element analysis of Springback in bending was done by V. Esat [20]. In the mentioned work, V. Esat et al. developed a finite element simulation in order to simulate Springback by means of a Springback factor using commercially available finite element program. They reached a good agreement between the finite element simulation and empirical data. Their finite element model is based on 2-D shell elements and Chung-Hulbert dynamic implicit as time integration scheme. They used penalty method on analytically defined rigid bodies to handle contact algorithm. D.W.Park et al. [22] proposed a new shell element to improve accuracy and efficiency of Springback simulation by describing complicated bending deformation accurately. They applied the new element both implicit Finite Element Method and explicit Finite Element Method to conduct Springback simulation. Many studies had been carried out on different perspectives of Springback. Micari et al. [33] presented a Springback prediction technique in three dimensional stamping processes which is based on a combined approach in which an explicit finite element code has been employed to simulate the forming phase while a traditional implicit procedure has been used to analyze the Springback phase. Gauand Kinzel [34] performed an experimental study for determining the Bauschinger Effect on Springback predictions which seems very significant in wipe bending operations. Since Springback is a vital concern in manufacturing industry, beyond evaluating and simulating attempts of Springback, some researchers studied the parameters that effect Springback in sheet metal forming operations in order to control these disturbing parameters. [Gupta*, 2.(9): September, 2015] ISSN 2349-6193 Impact Factor (PIF): 2.243 IJESMR International Journal OF Engineering Sciences & Management Research http: // www.ijesmr.com © International Journal of Engineering Sciences & Management Research [44] FACTORS AFFECTING BENDING Bend radius Ri, is one of the most important parameter which affects bending operations of sheet metals. The bend radius in bending operations always pertains to the inside radius of bend. Minimum bend radius is dependent on the material thickness and the mechanical properties of the material. Minimum bend radii vary for various metals; generally, most annealed metals can be bent to a radius equal to the thickness, T and sometimes to T/2, for a given bend angle and bend length. Bend angle is another crucial factor in bending operations. As the bend angle becomes larger, especially with bend angles over 90°, many difficulties arise. In this case, the amount of bend radius become more critical and the material hardness becomes more detrimental to the success of the bending process. In bending process, some deformations occur in the bent-up region of the work piece depending on the dimensions of the work piece, bend angle, and bend radius. As th
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飞机工业钣金回弹试验评价与验证
据估计,仅在美国汽车行业,其在延迟生产、模具修订成本和拒绝不合格零件方面的经济影响每年就超过5000万美元。很明显,控制回弹在制造中是一个至关重要的问题。在过去的几十年里,为了开发回弹减少和补偿方法,已经进行了一些研究。S. Nishino等人[4]研究了一种通过将自由弯曲试验数据与使用有限元法(FEM)进行的计算机模拟结果相结合来预测形状固定性能的新方法。随着有限元仿真技术在模具部门应用的日益广泛,钣金件的成形分析在生产模具的设计可行性研究中得到越来越多的应用。这些基于计算机的工具使设计工程师能够研究控制模具表面材料流动的工艺和材料参数。在过去的十年中进行了几项研究。M. Firat[17]通过u形通道的成形分析来预测回弹。为了提高预测的板料变形响应,他建立了基于加性背应力形式的运动硬化模型。Panthi等人[18]也研究了基于总弹性-增量-塑性应变(TEIP)的大变形算法,该算法用于非典型钣金弯曲过程建模。这个过程包括大的应变、旋转和回弹。N.Narasimham等人[19]旨在引入一种耦合的显式-隐式有限元方法,用于预测钣金冲压中的回弹变形,可用于最小化模具原型设计时间。在本研究中,他们初步利用显式方法分析了冲压过程中基于接触的成形操作。在此基础上,采用隐式求解方法模拟了去除成形压力后坯料的回弹过程。他们耦合了ANSYS/LS-DYNA显式和ANSYS隐式代码来解决涉及高度回弹的板料成形过程。V. Esat[20]对弯曲回弹的有限元分析进行了重要研究。在上述工作中,V. Esat等人开发了一种有限元模拟方法,利用市售的有限元程序通过回弹因子来模拟回弹。他们在有限元模拟和经验数据之间达成了很好的一致性。他们的有限元模型是基于二维壳单元和钟-赫尔伯特动力隐式作为时间积分方案。他们对解析定义的刚体采用惩罚法处理接触算法。D.W.Park等[22]提出了一种新的壳单元,通过精确描述复杂的弯曲变形,提高回弹模拟的精度和效率。采用隐式有限元法和显式有限元法对新单元进行回弹模拟。从不同的角度对Springback进行了许多研究。Micari等人[33]提出了一种三维冲压过程中的回弹预测技术,该技术基于一种组合方法,其中使用显式有限元程序来模拟成形阶段,而使用传统的隐式程序来分析回弹阶段。Gauand Kinzel[34]进行了一项实验研究,以确定鲍辛格效应对回弹预测的影响,这在擦拭弯曲操作中似乎非常重要。由于回弹在制造业中是一个非常重要的问题,除了对回弹进行评估和模拟之外,一些研究人员还研究了板料成形过程中影响回弹的参数,以控制这些干扰参数。[古普塔*,2.(9):September, 2015]影响因子(PIF): 2.243 [j]国际工程科学与管理研究学报[j] . // www.ijesmr.com©国际工程科学与管理研究学报[44]弯曲半径Ri是影响板料弯曲操作的最重要参数之一。弯曲作业中的弯曲半径通常是指弯曲的内半径。最小弯曲半径取决于材料的厚度和材料的机械性能。不同金属的最小弯曲半径不同;一般来说,对于给定的弯曲角度和弯曲长度,大多数退火金属可以弯曲到等于厚度T的半径,有时可以弯曲到等于T/2。弯曲角度是弯曲作业的另一个关键因素。当弯曲角度变大,特别是弯曲角度超过90°时,就会出现许多困难。在这种情况下,弯曲半径的大小变得更加关键,材料的硬度变得更加不利于弯曲过程的成功。
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