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ISSN : 1598-6721(Print)
ISSN : 2288-0771(Online)
The Korean Society of Manufacturing Process Engineers Vol.17 No.6 pp.75-82
DOI : https://doi.org/10.14775/ksmpe.2018.17.6.075

Structural Optimization of an LMU Using Approximate Model

Dong-Seop Han*, Si-Hwan Jang**, Soon-Hyeong Park***, Kwon-Hee Lee**#
*R&D Center, Remitite Co.
**Department of Mechanical Engineering, Dong-A University
***Technical Center, Central Corporation
Corresponding Author : leekh@dau.ac.kr Tel: +82-51-200-7638, Fax: +82-51-200-7656
23/08/2018 27/08/2018 30/08/2018

Abstract


This study suggests an optimal design process of an LMU, which is installed on the top side of offshore structures. The LMU is consist of EB(elastomeric bearing) and steel plate, and supports the vertical loads of offshore structures and assists its stable installation. The structural design requirement of the LMU is related to its stiffness. This study utilizes the finite element analysis to predict the stiffness. The stiffness of the EB depends on the size of the bearing. Thus, the design variables in this study are defined as the thickness, the width and the number of plates. Since the LMU has different loads for different locations, its stiffness should be designed differently. The multiobjective function is introduced to attain the target stiffness. In this process, the metamodel using the kriging interpolation method is adopted to replace the true stiffness.



근사모델을 이용한 LMU의 구조최적설계

한 동섭*, 장 시환**, 박 순형***, 이 권희**#
*(주)레미타이트 기업부설연구소
**동아대학교 기계공학과
***㈜센트랄 중앙연구소

초록


    National Research Foundation of Korea
    2017R1D1A3B03029727

    © The Korean Society of Manufacturing Process Engineers. All rights reserved.

    This is an Open-Access article distributed under the terms of the Creative Commons Attribution Non-Commercial License (http://creativecommons.org/licenses/by-nc/3.0) which permits unrestricted non-commercial use, distribution, and reproduction in any medium, provided the original work is properly cited.

    1. Introduction

    A leg mating unit (LMU) is a structure used to absorb loads and install a structure stably, as it is placed at the supporting point of the topside in a marine structure[1]. Generally, an LMU is a cylindrical shape, in which an elastomeric bearing and reinforced steel plate are alternately laminated, and a rubber pad is mounted on the lower lateral side[1]. Since loads applied differ at every supporting point in marine structures, the LMU should have the same displacement in all installation locations. That is, the compressive stiffness at each point should be designed differently[1].

    The stiffness of an LMU is dependent on the size of the bearing as well as the number and size of the reinforced plates laminated on the inside. A previous study[1] predicted the stiffness of an LMU through finite element analysis (FEA) and investigated the relationship between reinforced plates and compressive stiffness. To do this, the stiffness was evaluated through FEA while changing the thickness, width, and number of reinforced steel plates. However, the study was limited to designing an LMU with trial and error method. Thus, the present study aims to propose and apply an optimal design technique for an LMU by extending the previous study.

    The thickness, width, and number of reinforced plates were set as the design variables for the optimal design of the elastomeric bearing in the LMU. The elastomeric bearing[2] plays a role as a shock absorber, and its stiffness design is important. Here, the number of reinforced steel plates is a discrete design variable. Every location where the LMU is placed has its own goal stiffness. Thus, a multi-objective function was employed to consider this. The stiffness at each location was predicted using a metamodel in this process. A Kriging interpolation method[3-6] was used to create the metamodel, which was implemented by Excel. The optimal solution in the multi-objective function was calculated by using the built-in generalized reduced gradient algorithm in Excel. This study used the commercial program ANSYS for FEA.

    2. Structure of LMU and evaluation of stiffness

    This study proposed a design of an LMU with optimal stiffness used to install a topside of a marine structure, as shown in Fig. 1. Most LMUs are cylindrical shaped, and the reinforced plate-inserted rubber elastomeric bearing and steel plate are laminated in layers.

    The LMU in this study had an axisymmetric shape, which is equivalent to a two-dimensional (2D) axisymmetric simple model for FEA, as shown in Fig. 2. The material of the elastomeric bearing in the LMU was viscoelastic, and a force-displacement curve had to be made to calculate the compressive stiffness. This was done by calculating the reaction force (RF) by inputting a displacement as a load. The coefficient of friction in the boundary between the lower and upper steel plates was set to 0.1, and the contact capability of ANSYS was applied[1].

    3. Application of metamodel-based optimization

    3.1 Metamodel-based optimization

    The metamodel is generally used to calculate optimal solutions if shape variables are complex, the sensitivity analysis is difficult, a discrete design is included, or the FEA time is too long in the structural optimal design. The stiffness analysis of the LMU should consider the contact phenomenon, and discrete design variables are included in the design. Thus, this study adopted the metamodel-based optimization technique for the LMU design. The metamodel can be built using a Kriging model[3-6] and a response surface model[7], etc.

    This optimization process is shown in Fig. 3. First, design variables were defined, and experiments were set to build a metamodel using the experimental design. Here, a full factorial experiment was used. In addition, FEA was performed for each experiment. ANSYS was used to calculate the stiffness in this study. Next, based on the analysis results, a Kriging interpolation method was employed to build an approximate model. The multi-objective function was substituted with the approximate model, and finally, the optimal solution was calculated using the generalized reduced gradient (GRG) algorithm in the solution search function, a built-in function in Excel. In addition, verification analysis was performed to calculate the actual value in the optimal solution, since the predicted optimal solution was based on the approximate model.

    3.2 Formulation for optimal design

    The cross-section of the elastomeric bearing model in this study is shown in Fig. 4. The design variables considered in the optimization are related to the steel plate inside of the elastomeric bearing. As shown in the figure, the thickness (t), width (w) and number of steel plates (n) are defined as the design variables. For example, a model with two reinforced plates is shown. The design variables are selected based on the results in [1].

    The formulation for the optimal design can be described as follows:

    Minimize   R = i = 1 p w f ( y ^ i y t ) 2 ( i = 1 , 2 , ... , p ) Subject to        3 t ( m m ) 9 100 w ( m m ) 200 1 n ( e a ) 3
    (1)

    Here, p is 6, which is the maximum displacement load 60 mm divided by 10 mm. yt refers to the goal RF (stiffness) at the divided displacement load, and y ^ i refers to the RF (stiffness) predicted with the Kriging approximation model at the given displacement load. Design variables t and w are continuous design variables and design variable n is a discrete design variable. In Section 3, the Kriging approximation model is first calculated with regard to y ^ i for each displacement load. That is, a RF in response to each displacement is indicated as a design variable.

    3.3 Design of experiments

    This study employed a full factorial experiment method for each design variable as a design of experiment method. The level of each design variable was set to 3, as presented in Table 1, so that 33 = 27 experiments were defined.s

    3.4 Kriging model

    In the Kriging model, a global approximation model is predicted as follows[3-6].

    f ^ ( x ) = β ^ + r T ( x ) R 1 ( f- β ^ q )
    (2)

    Here, x refers to the design variable vector (x=[t, w, n] in this study), ^ refers to an estimate, f ^ is the predicted response( y ^ i in this study), R-1 refers to the inverse matrix of correlation matrix R, r refers to the correlation matrix, f refers to the response value vector, q refers to the unit vector, and ß refers to the constant. The correlation vector can be defined as follows:

    R ( x j , x j ) = E x p [ i = 1 n θ i | x i j x i k | 2 ] , ( j = 1 , ... , n s k = 1 , ... , n s )
    (3)

    Here, Ө refers to a parameter that can be calculated by following the optimization, and it equals the number of design variables.

    m a x i m i z e [ n s ln ( σ ^ 2 ) + ln | R | ] 2
    (4)

    A more detailed description of Kriging theory and induction can be found in [3-6].

    3.5 Generation of Kriging model

    Table 2 presents the parameter values in the Kriging approximate model created every 10 mm from 10 mm to 60 mm of displacement load. The Kriging predicted value in the RF can be calculated by substituting each parameter value in Table 2 into Eq. (2).

    To validate of the Kriging model, 27 arbitrary de sign points were created within the design variable r ange as presented in Table 3, and predicted and tru e analysis values were compared at those points. Th e displacement load values considered important in t his study were 30 mm and 60 mm. The errors betw een the structural analysis results and predicted valu es in the Kriging approximate model are shown in Figs. 5 and 6. As shown in the figures, the error w as smaller when the displacement load was 60 mm than when it was 30 mm.

    4. Results and discussion

    This study applied the metamodel-based optimization technique to optimize the elastomeric bearing in the LMU. In addition, an ideal function was selected to obtain desirable objective values, which were then analyzed and compared with the predicted values. The algorithm was implemented in Excel. The goal was to minimize the error between the objective function (yt) and approximate function ( y ^ i ) by performing the optimization.

    The most important design requirement of the elastomeric bearing is to have the force-displacement curve close to a linear shape. The load applied to the LMU was arbitrarily set to 10 MN, 20 MN, and 30 MN. These values were not only within the actual applied loads but also values in the boundary at the reinforced plate 1, 2, and 3[8, 9].

    When the size and number of reinforced plates are increased excessively, it makes the force-displacement curve become nonlinear. Considering this, the design goal was to find the design variables that made the force-displacement curve closer to linearity. Thus, optimization was performed to minimize the error between ideal function values and predicted function values, as presented in Eq. (1). In particular, this study emphasized the stiffness when displacement was 30 mm and 60 mm, which were regarded as important when performing the optimization. Figs. 7-9 show the comparison results between ideal function and predicted function values at the maximum loads of 10 MN, 20 MN, and 30 MN in the initial design. The results of optimization of the elastomeric bearing according to the maximum load value are presented in Table 4, and RFs with regard to the applied weighted values to obtain the ideal function values are marked in Table 5. As described above, the stiffness at 30 mm and 60 mm of displacement was mainly considered. In particular, a weighted value with regard to 60 mm was increased to the maximum to match the final stiffness. These weighted values were determined through several optimization tries. The errors of the predicted and analysis values with regard to the optimal values are presented in Table 6.

    Using the results, a flexible bearing design can be achieved with regard to loads applied in real sites. To show the errors of the predicted and analyzed results according to the maximum loads visually, Figs. 10, 11, and 12 are presented with graphs. The optimal solution provides a combination that makes the force-displacement curve as close to linearity as possible at the given condition.

    5. Conclusions

    This study optimized an elastomeric bearing in an LMU, which is required to install marine structures and absorb impact at the supporting point of marine structures, and obtained the following conclusions.

    • 1) The stiffness could be predicted with a function of design variables using the Kriging approximate model. To do this, the experimental design and Kriging approximate model were applied.

    • 2) The comparison results of the predicted and analysis values with regard to stiffness showed that a reliable approximate model was developed.

    • 3) The optimal solution was obtained that satisfied the design requirement of the ideal elastomeric bearing (i.e., to make the force-displacement curve as close to linearity as possible within the given design range).

    • 4) When the applied load was 10 MN, t=7.04 (mm), w=200 (mm), and n=1 (ea.); when it was 20 MN, t=9 (mm), w=189 (mm), and n=2 (ea.); and when it was 30 MN, t=3 (mm), w=185.53 (mm), and n=3 (ea.). The design procedure proposed in this study can achieve the flexible design of elastomeric bearings.

    Acknowledgment

    This research was supported by Basic Science Research Program through the National Research Foundation of Korea(NRF) funded by the Ministry of Education(No. 2017R1D1A3B03029727).

    Figure

    KSMPE-17-75_F1.gif
    Leg mating unit
    KSMPE-17-75_F2.gif
    Example of finite element model
    KSMPE-17-75_F3.gif
    Optimization process based on metamodel method
    KSMPE-17-75_F4.gif
    Section of EB and definition of design variable
    KSMPE-17-75_F5.gif
    Comparison of prediction and analysis at d=30mm
    KSMPE-17-75_F6.gif
    Comparison of prediction and analysis at d=60mm
    KSMPE-17-75_F7.gif
    Comparison of predicted function and ideal function at 10MN
    KSMPE-17-75_F8.gif
    Comparison of predicted function and ideal function at 10MN
    KSMPE-17-75_F9.gif
    Comparison of predicted function and ideal function at 10MN
    KSMPE-17-75_F10.gif
    Load-Displacement curve at 10MN
    KSMPE-17-75_F11.gif
    Load-Displacement curve at 20MN
    KSMPE-17-75_F12.gif
    Load-Displacement curve at 30MN

    Table

    Levels of design variables
    Parameters of θ and β
    Test points for model validation
    Optimum values according to the max. loads
    Reaction force according to the max. loads
    Comparison of optimum and analysis result

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