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DOI: 10.32604/cmes.2022.019835

ARTICLE

Time-Variant Reliability-Based Multi-Objective Fuzzy Design Optimization for Anti-Roll Torsion Bar of EMU

Pengpeng Zhi1,2,3, Zhonglai Wang1,2,*, Bingzhi Chen3 and Ziqiang Sheng4

1Yangtze Delta Region Institute (Huzhou), University of Electronic Science and Technology of China, Huzhou, 313001, China
2School of Mechanical and Electrical Engineering, University of Electronic Science and Technology of China, Chengdu, 611731, China
3School of Mechanical Engineering, Dalian Jiaotong University, Dalian, 116028, China
4Hefei CRRC Rolling Stock Co., Ltd., Hefei, 230012, China
*Corresponding Author: Zhonglai Wang. Email: wzhonglai@uestc.edu.cn
Received: 19 October 2021; Accepted: 05 November 2021

Abstract: Although various types of anti-roll torsion bars have been developed to inhibit excessive roll angle of the electric multiple unit (EMU) car body, it is critical to ensure the reliability of structural design due to the complexity of the problems involving time and uncertainties. To address this issue, a multi-objective fuzzy design optimization model is constructed considering time-variant stiffness and strength reliability constraints for the anti-roll torsion bar. A hybrid optimization strategy combining the design of experiment (DoE) sampling and non-linear programming by quadratic lagrangian (NLPQL) is presented to deal with the design optimization model. To characterize the effect of time on the structural performance of the torsion bar, the continuous-time model combined with Ito lemma is proposed to establish the time-variant stiffness and strength reliability constraints. Fuzzy mathematics is employed to conduct uncertainty quantification for the design parameters of the torsion bar. A physical programming approach is used to improve the designer's preference and to make the optimization results more consistent with engineering practices. Moreover, the effectiveness of the proposed method has been validated by comparing with current methods in a practical engineering case.

Keywords: Anti-roll torsion bar; time-variant reliability; fuzzy design optimization; multi-objective

1  Introduction

Reliability-based design optimization (RBDO) is an important way to improve the reliability of products under uncertainty in the design stage. Due to the time-variant property of design parameters, working conditions and uncertainties affecting the products’ performance, time-variant reliability-based design optimization (TRBDO) has become urgent to ensure the operating reliability and safety during the products’ lifecycle. Currently, TRBDO has attracted more attentions and is being applied in engineering practices [14].

For a complicated engineering problem, one main challenging task is to build the TRBDO model sufficiently considering the complexity of the working conditions and uncertainty quantification as well as the nested relationship between objectives and constraints. In addition, several objectives should be balanced and therefore the multi-objective optimization should be performed during the procedure of the TRBDO. So far, there are several preliminary developments by integrating the TRBDO and the multi-objective optimization, which will be one of the important trend of the design technique under uncertainty. Multidisciplinary design optimization (MDO) mainly focus on the coupled relationship between different disciplines or subsystems [511], while multi-objective optimization makes a decision by balancing the objectives under the satisfaction of constraints [1214]. In some special cases, the MDO problem can be transformed to the multi-objective optimization problem. Therefore, time-variant reliability-based multi-objective design optimization (TRBMDO) is a necessary approach to guaranteeing the lifecycle reliability and safety of products while the balance of several objectives and other constraints are satisfied. Currently, several methods have been developed for the TRBMDO. Yu et al. [15] proposed a multi-objective design optimization framework combining both the time-variant reliability and robustness. Zhang et al. [16] implemented the multi-objective optimization model for the lifting gear transmission system, where the distance between natural frequency and meshing frequency is maximized and the volume of gears is minimized under the time-variant reliability constraints. Dong et al. [17] studied the multi-objective optimization by considering the deterioration of the bridge with the time progressing under uncertainty. Okasha et al. [18] discussed the time-variant redundancy of structural systems and provided the multi-objective optimization framework for the risk-based management. Wang et al. [19] employed a nested extreme response surface to conduct the multi-objective optimization in an iterative RBRDO process with the lifecycle cost and the quality of aircraft tubing as the design objectives. Angelis et al. [20] gave the general and effective numerical method for a fatigue-prone weld to achieve the robust and time-variant maintenance plan.

For the structure of EMU, the secondary suspension system usually uses the air spring to obtain better vertical performance and improve the riding comfort. However, the low stiffness of the air spring will lead to the reduction of the roll stiffness of the vehicle and then the roll angle increases. Especially when the vehicle is operating on the curve track with superelevation, or when the vehicle encounters a large lateral wind, the smaller roll stiffness will raise the operating risk greatly. In order to address the issue well, the anti-rolling device is used to increase the counter-torque against the lateral rolling of the vehicle body. The overturning safety is then improved by reducing the inclination angle of the vehicle without increasing the vertical stiffness of the spring. As the most part of the anti-rolling device, the time-variant reliability of the anti-roll torsion bar will directly affect the operating safety of the vehicle.

However, many studies are about the stiffness and strength analysis under the time-invariant conditions as well as the fatigue experiments for the anti-roll torsion bar. Duan et al. [21] presented a calculation model for the deformation and stress considering the different loading state of the anti-roll torsion bar system. Lu et al. [22] described the stress and load-bearing state of the anti-roll torsion bar for the operating vehicle and then carried out the fatigue life analysis and experimental verification. Wang et al. [23] discussed the influence of velocity, the curve radius, and the superelevation on the anti-roll torsion bar according to the loading history. Dong et al. [24] provided a multi-response robust optimization method for the anti-roll torsion bar based on a stochastic model. However, the time-variant reliability of the anti-roll torsion bar has been rarely investigated.

In this paper, a time-variant reliability-based multi-objective fuzzy design optimization (TRBMFDO) method for the anti-roll torsion bar of the EMU is proposed. The TRBDO constraints related to the stiffness and strength are first established by accounting for the time-variant stochastic working conditions and the working principle of the anti-rolling torsion bar. The optimal rage of design variables is then determined by employing the membership function combined with the fuzzy allowable interval. The physical programming method is then presented to transform the multi-objective fuzzy design optimization problem to a single-objective design optimization problem under the satisfaction of the reliability constraints. The results of the TRBMFDO are finally achieved by using the combinatorial optimization strategy.

The remainder of the paper is organized as follows. Mechanical performance analysis of the torsion bar are presented in Section 2. Time-variant reliability model under the stochastic process is described in detail in Section 3. Section 4 proposes the fuzzy optimization model of the anti-roll torsion bar. Section 5 uses an engineering example to illustrate the effectiveness of the proposed method. Finally, Section 6 summarizes and concludes.

2  Mechanical Performance Analysis of the Torsion Bar

The mechanical performance analysis of the torsion bar is the foundation of the design optimization. Basically, the anti-roll torsion bar can be divided into the built-in bar and external bar according to the different position of the support seat. The support seat of the built-in anti-roll torsion bar is generally composed of the upper part and lower part, where the rubber joint is used. The support seat of the external anti-roll torsion bar is an entire structure, where the metal joint or integral polymer wear-resistant bushing is used. In the paper, we will study the external anti-roll torsion bar, whose installation position in the bogie frame is shown in Fig. 1.

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Figure 1: Anti-roll torsion bar device of EMU

2.1 Stiffness Analysis of the Torsion Bar

As the most important performance index of the anti-roll torsion bar device, anti-roll stiffness can ensure the roll angle of the vehicle body and the flexibility coefficient of the vehicle. Proper anti-roll stiffness can effectively improve the safety, stability, and comfort of operation. The anti-roll stiffness can be derived from the force analysis shown in Fig. 2 by considering the installation position and working principle of the anti-roll torsion bar in Fig. 2.

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Figure 2: Force diagram of the anti-roll torsion bar device

For the given parameters in Fig. 2, F is the axial force of the connecting rod, θ is the roll angle of the vehicle body, Kt is the anti-roll stiffness of the torsion bar, kr is the torsional stiffness of the torsion bar, br is the effective length of the torsion bar, l is the length of the torsion arm, and ζ is the vertical displacement of the connecting rod. M denotes the restoring moment of the torsion bar and

M=Ktθ(1)

Considering the working principle of the anti-roll torsion bar, the restoring moment can be expressed as

M=Fbr(2)

Fl=2ζkrl(3)

where

ζ=θbr2(4)

Therefore, the anti-roll stiffness of the torsion bar can be derived by

K=br2krl2(5)

The torsion bar includes three areas, namely the working area, transition area, and connection area. Therefore, the stiffness of the bar is integrated by the stiffness of the working area, transition area, and connection area. Provided that the cross-section of the torsion bar is circular and its diameter is d, the torsion stiffness can be expressed by

kri=πdi4G32bi(6)

where i is the number of the areas; bi is the length of the torsion bar.

When the transition area is an arc, the length of the transition section can be provided by [25]:

L=Dd24rDd1(7)

where D and d represent the large diameter and small diameter at the transition of the arc, respectively; r represents the radius of the transition arc.

Considering the relationship of the stiffness between the torsion bar and the three areas, the torsional stiffness of the torsion bar is

1kr=2kr1+2kr2+1kr3(8)

2.2 Strength Analysis of the Torsion Bar

When the anti-roll torsion bar is operating, it will suffer from the bending stress and torsion shear stress. Generally, the torsion shear stress is greater than the bending stress. The strength of the bar can be derived with the help of the third strength theory by combining the bending stress and torsion shear stress, where the bending moment and torque are shown in Fig. 3.

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Figure 3: Bending moment and torque diagram of the torsion bar

From Fig. 3, we can see that the torsion bar is only subject to torque in the working area but subject to the bending moment and torque at the same time in the transition and connection areas. For the torsion bar without defect, the maximum stress appears at the crossing of the minimum section transitions.

With the combination of the bending and shear conditions, the stress of the torsion bar is therefore expressed by

σca=MeW=32M2+(αT2)πd33(9)

3  Time-Variant Reliability Model under the Stochastic Process

The stiffness, strength, and allowable stress of the anti-roll torsion bar are usually time-variant due to several uncertain factors from the working conditions, loadings and also the degradation of the material. The time-variant factors will result in the time-variant change of the reliability of the bar. If the time-variant property is ignored, the reliability only ensure the safety of the bar at the initial time, namely t = 0 not the whole lifecycle. Therefore, it is necessary to properly account for the time-variant property and further conduct TRBDO to guarantee the lifecycle reliability and safety.

3.1 Statistical Analysis for the Stiffness of the Torsion Bar

Since the diameter d changes with time due to the wear, the normal distribution geometric Brownian motion will be employed to describe d(t) under uncertainty. Here, Ito differential equation will be used for featuring the uncertainty propagation based on Eq. (6)

dd(t)=λdd(t)dt+δdd(t)dω2t(10)

lnkrid=4d;2lnkrid2=4d2(11)

dlnkri(t)=[lnkridλdd(t)+12(2lnkrid2δd2d2(t))]dt+lnkridδdd(t)dω2t(12)

Mean and variance of lnkri(t) are provided by

{μ^lnkri(t)=lnkri(0)+0t(4λd2δd2)ds=lnkri(0)+(4λd2δd2)tσ^lnkri2(t)=[0t(4δd)dω2s]2=(16δd2)t(13)

Based on Eqs. (8) and (13), the means of lnkri(t) can be obtained by

μ^lnkr(t)=12μ^lnkr1(t)+2μ^lnk2(t)+1μ^lnkr3(t)(14)

Based on Eqs. (5) and (14), the mean of lnKt can be expressed by

μ^lnK(t)=br2μ^lnkr(t)l2(15)

3.2 Statistical Analysis for the Strength of the Torsion Bar

Provided E is time-variant under uncertainty and also follows the normal distribution geometric Brownian motion, we have

{dE(t)=λEE(t)dt+δEE(t)dω1tdd(t)=λdd(t)dt+δdd(t)dω2t(16)

Take the logarithm of the function according to Eq. (9):

S=lnσca=ln32π+12lnE3lnd(17)

dS=(12λE3λd14δE2+32δd2)dt+12δEdω1t3δddω2t(18)

Mean and variance of S(t) are provided by

{μ^S(t)=lnσca(0)+0t(12λE3λd14δE2+32δd2)dS=lnσca(0)+(12λE3λd14δE2+32δd2)tσ^S2(t)=(120tδEdω1t)2+(0t(3δd)dω2t)=(14δE2+9δd2)t(19)

3.3 Statistical Analysis for the Material Strength

The material strength of the anti-roll torsion bar is random and time-variant, and therefore non-stationary random process can be employed to describe the material strength. The material strength of the torsion bar can be quantified as the product of the initial material strength and attenuation function.

Sm(t)=Sm0(t)×φ(t)(20)

where Sm(t) denotes the initial material strength at t = 0, which can be expressed by Sm(0); φ(t) is the attenuation function of the material strength, which is a deterministic function.

Then the material strength can be expressed with the given expression of the attenuation function

Sm(t)=Sm(0)×exp(kt2)(21)

where k is the attenuation coefficient of the material strength.

Mean and variance of Sm(t) are provided by

{μ^Sm(t)=μSm(0)×exp(kt2)δ^Sm2(t)=δSm2(0)(22)

3.4 Time-Variant Reliability of the Anti-Roll Torsion Bar

According to the time-variant stress-strength interference (SSI) model, the reliability of the anti-roll torsion bar can be expressed by [26,27]

R(t)=P{lnSm(t)lnσca(t)0}(23)

We define Z=lnSm(t)lnσca(t), then Eq. (23) can be rewritten as

R(t)=P{Z0}(24)

Since lnSm(t) and lnσca(t) follow the normal distribution and are independent, Z also follows a normal distribution. Then the time-variant reliability of the torsion bar can be defined as

R(t)=P{Z0}=0φ(Z)dz=1(2π)1/2ZSm(t)exp(v22)dv=1(2π)1/2ZSm(t)exp(v22)dv(25)

The time-variant reliability of the torsion bar is the provided by

R(t)=Φ(lnμSm(0)kt2μ^σca(t)lnδSm2(t)+σ^σca2(t))(26)

4  Fuzzy Optimization Model of the Anti-Roll Torsion Bar

4.1 Physical Programming Model

Physical programming is an effective approach to dealing with the multi-objective optimization problem, since the designer can express his preferences according to the experience. Actually, there are four kinds of preference function, namely Class 1S, Class 2S, Class 3S, and Class 4S, to quantify the designer's requirements [28]. For the anti-roll torsion bar, we mainly focus on the lightweight and high reliability. Therefore, the reference function that the smaller the mass and structural stress the better will be chosen, which belongs to Class 1S and shown in Fig. 4.

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Figure 4: Preference functions for Class 1S

In Fig. 4, i represents the number of design objectives, i=1,2,,n; fi represents the preference value of the design objective; fik represents the interval boundary value of the design target value in the k segment. The value of the preference function on the boundary of each interval can be obtained by

f¯1=f¯~1=0.1(27)

f¯˜k=βnf¯˜(k1)(2k5,β >1)(28)

f¯k=f¯(k1)+f¯k(2k5)(29)

λik=fikfi(k1)(30)

where f¯k is the preference function value of the interval boundary k; β is the convexity coefficient; f¯~k is the change of the preference function value through the k-th interval.

s~ik=f¯~k/f¯~kλikλik(k=2,3,4,5)(31)

si1=αs˜i2(0 <α <1)(32)

sik=(sik)min+αΔsik(k=2,3,4,5)(33)

(sik)min=4s~iksi(k1)3,Δsik=83(s~iksi(k1))(34)

where sik is the first derivative of the preference function at the interval boundary k; s~ik is the average slope of the preference function at the interval boundary k.

The quantitative preference function can be obtained with the piecewise function curve fitting method based on Eqs. (27)(34). The preference function of each design objective is further taken into the common logarithm of the average value and synthesized into the comprehensive preference function with f(x) as the objective function. The physical programming model of the anti-roll torsion bar can be provided by

find d=(d1,d2,d3)minf(d)=log10{1n[i=13f¯i(fi(d))]}s.t.{f1(d)f1(d)5;f2(d)f2(d)5;f3(d)f3(d)5dididi+(35)

where di and di+ represent the lower and upper bounds of the fuzzy interval for design variables, respectively.

4.2 Membership Function of the Fuzzy Constraint and Non-Fuzzy Processing

Due to the existence of incomplete information, fuzzy variable is used to describe the uncertainty of the design variables. It is important to select the proper membership function for the fuzzy variables, since the shape of the membership function will affect the design optimization results. According to the boundary constraint of the design variables, the linear membership function is usually used and provided by

μdj={0djd_jl(djd_jl)/(djd_jl)(d_jud_jl)(d_jud_jl)d_jldjd_ju1d_judjd¯jl(d¯judj)/(d¯judj)(d¯jud¯jl)(d¯jud¯jl)d¯jldjd¯ju0d¯judj(36)

where d_jl is the lower limit for the lower bound; d_ju is the upper limit for the lower bound; d¯jl is the lower limit for the upper bound; d¯ju is the upper limit for the upper bound.

The upper and lower limits of the upper and lower bounds in Eq. (36) are determined by the expansion coefficient method, which is widely used in engineering practices. The upper and lower limits of the transition interval are determined by introducing an amplification coefficient. Therefore, the range of the expansion coefficient can be determined as α¯[1.05,1.30], α_[0.7,0.95]. Level cut set is a commonly used method and the fuzzy comprehensive evaluation method can be used to the optimal level cut set λ [29].

The framework of the proposed TRBMFDO method of the anti-roll torsion bar is shown in Fig. 5.

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Figure 5: The framework of the proposed TRBMFDO method

5  Practical Engineering Examples

The detailed structure of the anti-roll torsion bar is shown in Fig. 6. The material of the anti-roll torsion bar is 52GrMoV4, whose tensile strength is 1450 MPa, yield limit is 1300 MPa, and allowable stress is 745 MPa.

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Figure 6: Structural diagram of the torsion bar

5.1 Time-Variant Stiffness of the Torsion Bar

The initial stiffness of the torsion bar in the working area, transition area, and connection area can be calculated, respectively

kr1=πd14G32b1=2.246×106Nm/rad

kr2=πd24G32b2=2.918×106Nm/rad

kr3=πd34G32b3=3.20×104Nm/rad

In order to obtain the distribution parameters of d(t), the experimental data about the torsional stiffness of the torsion bar are collected, shown in Fig. 7.

With the collected data in Fig. 7, the shift and volatility rate of the stiffness can be estimated as

λd=1.5×105;δd=1×103.

When the drift and volatility rate are substituted into Eqs. (13)(15), the time-variant stiffness of the torsion bar can be obtained at t = 9000.

μ^lnkr1(t)=lnkr1(0)+(4λd2δd2)t=14.07Nm/rad

μ^lnkr2(t)=lnkr2(0)+(4λd2δd2)t=14.328Nm/rad

μ^lnkr3(t)=lnkr3(0)+(4λd2δd2)t=10.32Nm/rad

Then the time-variant stiffness of the torsion bar is

K=br2krl2=2.7522×2.8×1040.172=7.34MNm/rad

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Figure 7: Historical observations of torsion bar stiffness

Considering the design requirements and stiffness change with time of the torsion bar, the constraint of stiffness is given as 6.606MNm/radK(t)8.074MNm/rad.

5.2 Time-Variant Strength of the Torsion Bar

According to the CRH3-350-PS-021 technical specification, the loadings of the torsion bar mainly include the static loading Fstatic caused by the vehicle's center of gravity deviation, the dynamic operating loading Fdynamic, and the loading Fmax under special working conditions. The detailed information of the loadings is provided in Table 1.

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The value of the loading is usually determined by the vehicle's center of gravity deviation and the outside lateral force. The expressions of the loading normal condition and special condition are provided by

Fnormal=Fstatic+Fdynamic=37kN

Fspecial=Fstatic+Fmax=62kN

When designing the torsion bar, three conditions should be satisfied: (1) the maximum stress should be less than the fatigue limit of the material; (2) the maximum stress is not greater than the yield strength of the material; (3) the maximum shear stress is less than the allowed shear stress of the material under the special load case. The stresses of the torsion bar under the normal and special conditions are calculated based on Eq. (9):

σca1=Me1W=378.26MPa < 745 MPa

σca2=Me2W=633.85MPa < 1300 MPa

where Me1 and Me2 are the moments of torsion bar under normal condition and special condition, respectively, W is the bending section coefficient.

The stresses of σca1 and σca2 observed from the product are shown in Fig. 8, where the observation interval Δ = 1d.

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Figure 8: Historical observations of torsion bar stress (a) Torsion bar stress σca1 (b) Torsion bar stress σca2

With the collected data in Fig. 8, the shift and volatility rate of the stress can be estimated as λE=9×105;δE=8×104.

When the drift and volatility rate are substituted into Eq. (19), the time-variant stress of the torsion bar can be obtained at t = 9000.

{μ^σca1(t)=lnσca1(0)+(12λE3λd14δE2+32δd2)=666MPaσ^σca12(t)=(14δE2+9δd2)t=2.25×103MPa

{μ^σca2(t)=lnσca2(0)+(12λE3λd14δE2+32δd2)=1119MPaσ^σca22(t)=(14δE2+9δd2)t=2.25×103MPa

5.3 Degradation of the Material Strength and Time-Variant Stress Constraints

Due to the existence of the failure modes of fatigue, wear and corrosion, the strength of the bar will degrade with time. The collected historical data of the allowable stress is provided in Fig. 9.

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Figure 9: Historical observations of the material strength

When the data in Fig. 9 is considered as the inputs of Eqs. (20)(22), the mean and standard deviation of allowable shear stress can be obtained.

{μ^R1(t)=μR1(0)×exp(kt2)=691MPaδ^R1(t)=δR1(0)=1MPa

The mean and standard deviation of the yield limit can be expressed by

{μ^R2(t)=μR2(0)×exp(kt2)=1205.67MPaδ^R2(t)=δR2(0)=1MPa

The time-variant reliability constraints of the stresses are provided

{g4(t)=0.9Φ(ln745(9.3×1010)t2μ^σca1(t)lnδR12(t)+σ^σca12(t))0g5(t)=0.95Φ(ln1300(9.3×1010)t2μ^σca2(t)lnδR22(t)+σ^σca22(t))0

5.4 Fuzzy Allowable Interval of Design Variables

The diameters of the working area, transition area, and connection area for the anti-roll torsion bar of the EMU are usually uncertain, because the uncertainty is from the design, manufacturing and the working conditions. According to the design rule, the upper and lower bounds of expansion coefficients for diameter are α¯=1.05 and α_=0.9, respectively. Then the upper and lower bounds of the fuzzy allowable interval can be determined, shown in Table 2.

The optimal level cut set obtained by the fuzzy comprehensive evaluation is λ=0.6 [30]. The fuzzy allowable intervals of design variables are given by 62.4d175.4852.8d265.2849.92d362.22.

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5.5 Fuzzy Optimization Model of Time-Variant Reliability for the Anti-Roll Torsion Bar

In this example, the objective is to maximize the strength and stiffness, and meanwhile to minimize the mass of the anti-roll torsion bar under the satisfaction of the reliability and other performance constraints.

The mass can be calculated by

f1=m=ρ(πd122l1+πd222l2+πd324l3)(37)

where ρ is the density of material 52GrMoV4; l1, l2 and l3 are the length of the working area, transition area, and connection area, respectively.

The stresses are given by

f2=σca1=Me1W=32M12+(αT1)2πd33(38)

f3=σca2=Me2W=32M22+(αT2)2πd33(39)

The preference function interval of optimization objectives can be obtained based on relevant standards and engineering experience, provided in Table 3.

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By using Eqs. (27)(34), the preference function expression of each optimization objective can be obtained by piecewise function fitting.

The expression of preference function for the mass of the anti-roll torsion bar is

f¯1(m)=0.004862m40.8364m3+53.82m211534m+16350

The expression of preference function for the stress σca1 of the anti-roll torsion bar is

f¯2(σca1)=(7.184×107)σca140.001372σca13+0.9759σca12306.5σca1+35820

The expression of preference function for the stress σca2 of the anti-roll torsion bar is

f¯3(σca2)=(8.908×108)σca24(2.854×104)σca23+0.3406σca22179.5σca2+35180

The fitting curve of preference functions for the mass, stress σca1, and stress σca2 are shown in Fig. 10, respectively.

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Figure 10: Fitting curve of preference function. (a) Preference function curve of the mass (b) Preference function curve of the stress σca1 (c) Preference function curve of the stress σca2

With the obtained preference functions of the objective functions and the related constraints, the TRBMFDO model is

find d=(d1,d2,d3)minf(d)=log10{13[f¯1(f1(d))]+13[f¯2(f2(d))]+13[f¯3(f3(d))]}

s.t.

g1=f1(d)56.610g2=f2(d)6660g3=f3(d)1118.790

62.4d175.4852.8d265.2849.92d362.226.606K(t)8.074g4(t)=0.9Φ(ln745(9.3×1010)t2μ^σca1(t)lnδR12(t)+σ^σca12(t))0

5.6 Solving the TRBMFDO Problem

Since the complicated and coupled relationship exists in the TRBMFDO model, it is difficult to obtain the highly efficient and accurate results of the design by using general optimization strategies. In order to obtain the global optimal results effectively, a hybrid optimization strategy is implemented with integrating DOE sampling and numerical optimization. This hybrid optimization strategy can reduce the probability of trapping in the local optimal solution. The main task of the proposed strategy is that DOE method is employed to draw samples in the design region evenly and the parameter optimization module is to conduct design optimization for the optimal design results. The flowchart of the hybrid optimization strategy is provided in Fig. 11.

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Figure 11: The hybrid optimization strategy

Three combinations based on the DOE including DOE+NLPQL, DOE+MIGA and DOE+ASA are used for the problem. The related results are provided in Table 4. From Table 4, we can see that the DOE+NLPQL strategy is better than the DOE+MIGA and DOE+ASA methods in the computational efficiency under the satisfaction of the computational accuracy. The DOE+MIGA and DOE+ASA optimization strategies require a total of more than 1000 function calls respectively, but the DOE+NLPQL optimization strategy requires only 17 function calls. The optimization results from the non-fuzzy method (the cut level set method) is lightly more conservative, which will reduce the objective of the lightweight design of the torsion bar. The reliability of the torsion bar increases 14% and 4.7%, respectively under the fuzzy optimization and non-fuzzy optimization methods. The mass of the torsion bar obtained by the fuzzy optimization method is 56.265 kg, a decrease of 0.14%; while the mass of the torsion bar obtained by the fuzzy optimization method is 56.265 kg, a decrease of 0.6%. The iterative processes of the fuzzy and non-fuzzy optimization with three different optimization strategies are given in Fig. 12.

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Figure 12: Iterative processes of the fuzzy and non-fuzzy optimization. (a) Iterative process of fuzzy optimization (b) Iterative process of non-fuzzy optimization

It can be seen from Fig. 12 that the preference function value based on the fuzzy optimization method is lower than that based on the non-fuzzy optimization method. It means that the optimal solution of the multi-objective function obtained by the fuzzy optimization method is better than that by non-fuzzy optimization method. It also shows that the number of iterations of the DOE+NLPQL optimization strategy is smaller than that of the other two optimization strategies. The better computational efficiency of the proposed method is further validated.

To further verify the differences between the three optimization strategies in the optimization process, the design space and the optimal solution set are shown in Fig. 13. The solution set of the physical programming and the solution set of the DOE+ASA optimization strategy are more evenly distributed in the whole design space, but more function calls are needed. The solution set of the DOE+MIGA optimization strategy is still evenly distributed in the whole design space, however the number of iterations reduces because the solution set is around the concentration. Nevertheless, the DOE+NLPQL optimization strategy can quickly capture the optimal domain to obtain the global optimal solution with a minimum set of solutions.

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Figure 13: Optimal solutions of the physical programming with three optimization strategies. (a) The DOE+NLPQL optimization strategy (b) The DOE+MIGA optimization strategy (c) The DOE+ASA optimization strategy

6  Conclusions

In this paper, a TRBMFDO method for the anti-roll torsion bar of the EMU is proposed, which will be an effective tool to design the anti-roll torsion bar optimally under the satisfaction of the lifecycle reliability and safety. The time-variant reliability models of the torsion bar are first built related to the stiffness and strength considering the uncertainty and time-variant property. The physical programming method is then presented to handle the multi-objective design optimization to avoid the selection of the weight factors. The fuzzy allowable interval of design variables is then estimated based on the fuzzy theory. The comprehensive preference function is solved by the DOE+NLPQL hybrid optimization strategy. With the practical example, it is testified that the reliability of the anti-roll torsion bar increases by 14% during the lifecycle, and the weight of the torsion bar decrease by 0.6%. For the proposed DOE+NLPQL optimization strategy, only 17 function calls are needed for the global optimal solution, and therefore the computational efficiency increased by over 58.8 times compared with the DOE+ASA optimization strategy and the DOE+MIGA optimization strategy. In our future work, we will consider more time-variant failure modes including wear, corrosion and so on.

Funding Statement: This work was supported by Sichuan Science and Technology Program under the Contract No. 2020JDJQ0036.

Conflicts of Interest: The authors declare that they have no conflicts of interest to report regarding the present study.

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