ANALYSIS & OPTIMIZATION OF LIFTING LUG ACCORDING TO LOAD CONDITIONS

Introduction

The main focus of this project was to analyze the existing lifting lug under the set load conditions and observe its behavior. The different analysis like: Stress-strain analysis, deformation, safety factors were obtained using ANSYS workbench. The results were not satisfactory. We then optimized the model so that the model would sustain with respect to load conditions. During the process, various parameters were selected as input and output parameters for optimization.

Keywords:- ANSYS Workbench 2022, Lifting Lug, Stress-strain Analysis, Total Deformation, Safety Factor, Optimization.

As lifting lug is a thin plate with a hole in it which assists in raising/lifting objects in different cases, it must be hard and must withstand the load subjected to it without undergoing any deformation.

Structural steel is a category of steel used for making construction materials in a variety of shapes. Structural steel shapes, sizes, chemical composition, mechanical properties such as strengths, storage practices, etc., are regulated by standards in most industrialized countries. Most structural steel shapes, such as I-beams, have high second moments of area, which means they are very stiff in respect to their cross-sectional area and thus can support a high load without excessive sagging. Therefore, we have selected structural steel for the model.

The model is designed to withstand the bearing load as follow:

Bearing Load

Design Optimization

First of all, the parameters were selected on whose basis the design was to be optimized. Outline of Schematic Parameters:

S.N.

INPUT

PARAMETER

OUTPUT

PARAMETER

1

Base Thickness

Safety Factor

2

Vertical Thickness

Geometry Mass

3

Fillet Radius

Following constraints were setup:

Domain of Input Parameters:

Input Parameters

Name

Lower Bound

Upper Bound

P10 - FilletRadius (mm)

9

11

P11 - VerticalThickness (mm)

10

10.6

P12 - BaseThickness (mm)

10.5

11.5

Parameter Relationships

Name

Left Expression

Operator

Right Expression

New Parameter

Relationship

The model was analyzed under 15 different sets of design points to check how the system responded under above conditions. The results obtained were as follows:

Name

P10 -

FilletRadius (mm)

P11 -

VerticalThickness (mm)

P12 -

BaseThickness (mm)

P5 - Geometry Mass (kg)

P9 - Safety Factor Minimum

1

9.066666667

10.02

10.53333333

1.431913622

0.689172201

2

9.2

10.32

10.86666667

1.476142521

0.707393408

3

9.333333333

10.17

11.2

1.493287875

0.759651334

4

9.466666667

10.47

10.64444444

1.469955089

0.680159003

5

9.6

10.095

10.97777778

1.47357664

0.700520798

6

9.733333333

10.395

11.31111111

1.517853457

0.775980239

7

9.866666667

10.245

10.75555556

1.467461085

0.699319639

8

10

10.545

11.08888889

1.511761861

0.737493888

9

10.13333333

10.0575

11.42222222

1.508657449

0.77698146

10

10.26666667

10.3575

10.57037037

1.462867992

0.689365856

11

10.4

10.2075

10.9037037

1.480109182

0.70869156

12

10.53333333

10.5075

11.23703704

1.524457876

0.786750182

13

10.66666667

10.1325

10.68148148

1.460589619

0.699476961

14

10.8

10.4325

11.01481481

1.504962273

0.722480504

15

10.93333333

10.2825

11.34814815

1.522251381

0.783492985

It is clear from the above data that the domain set for the design point failed to give the required factor of safety. Hence, second iteration was done by studying the above table and setting new domain for the input parameters.

This time only two parameters were selected as input parameters under the following domains and different design points were evaluated.

Input Parameters

Name

Lower Bound

Upper Bound

P11 - VerticalThickness (mm)

13

28

P12 - BaseThickness (mm)

13

20

Parameter Relationships

Name

Left Expression

Operator

Right Expression

New Parameter Relationship

The model was again analyzed under 20 different sets of design points and 5 best design points were obtained.

Name

P11 - VerticalThickness (mm)

P12 - BaseThickness (mm)

P5 - Geometry Mass (kg)

P9 - Safety Factor Minimum

1

13.375

13.175

1.840777664

0.888823914

2

14.125

16.675

3

14.875

14.925

2.064155316

1.045175934

4

15.625

18.425

5

16.375

14.05

2.087944113

0.971759668

6

17.125

17.55

7

17.875

15.8

8

18.625

19.3

9

19.375

13.6125

2.253812262

0.958886415

10

20.125

17.1125

11

20.875

15.3625

12

21.625

18.8625

13

22.375

14.4875

2.530572514

0.972085782

14

23.125

17.9875

15

23.875

16.2375

16

24.625

19.7375

17

25.375

13.39375

2.657361985

0.729956675

18

26.125

16.89375

19

26.875

15.14375

20

27.625

18.64375

The candidate point 5 was chosen as the best design point for our model on the basis of best combination of factor of safety and mass.

Reference

Name

P11 -

VerticalThickness (mm)

P12 -

BaseThickness (mm)

P5 - Geometry Mass (kg)

P9 - Safety Factor Minimum

Parameter Value

Variation from Reference

Parameter Value

Variation from

Reference

Candidate Point 1

13.375

13.175

1.840777664

-18.33%

0.888823914

-7.31%

Candidate Point 2

14.875

14.925

2.064155316

-8.41%

1.045175934

9.00%

Candidate Point 3

19.375

13.6125

2.253812262

0.00%

0.958886415

0.00%

Candidate Point 4

22.375

14.4875

2.530572514

12.28%

0.972085782

1.38%

Candidate Point 5

25.375

13.39375

2.657361985

17.91%

0.729956675

-23.87%

New Custom Candidate Point

20.5

16.5

From the above table, it is clear that the candidate point 2 is the best design point from the above options, thus, its values were copied to the current design point and model was simulated to obtain the following results.

Solutions Information

Solution Information Results

Object Name

Total Deformation

Equivalent Stress

Results

Minimum

0. m

8070.5 Pa

Maximum

5.4486e-006 m

8.2474e+007 Pa

Average

1.6936e-006 m

2.5351e+006 Pa

Minimum Occurs On

Lifting Lug

Maximum Occurs On

Lifting Lug

Minimum Value Over Time

Minimum

0. m

0. Pa

Maximum

0. m

8070.5 Pa

Maximum Value Over Time

Minimum

0. m

0. Pa

Maximum

5.4486e-006 m

8.2474e+007 Pa

Total DeformationMechanical_Report_Files/Figure0003.png

Figure

Mechanical_Report_Files/Figure0005.png

Equivalent Stress

Mechanical_Report_Files/Figure0006.png

Figure

Mechanical_Report_Files/Figure0008.png

Fatigue Tools

Mechanical_Report_Files/Figure0011.png

Mechanical_Report_Files/Figure0012.png

Results

Object Name

Life

Safety Factor

Definition

Design Life

1.e+009 cycles

Results

Minimum

1.e+006 cycles

1.0452

Minimum Occurs On

Solid

Figure

Mechanical_Report_Files/Figure0010.png

Conclusion

S.N.

NAME

INITIAL VALUES

OPTIMIZED VALUE

OBJECTIVE

VARIATION FROM REFERENCE

1

Total Deformation

6.87E-06

5.45E-06

Minimize

-2.07E+01

3

Safety Factor

Minimum

0.66018

1.0452

Maximize

5.83E+01

Appendix Units

Geometry


TABLE 1

Unit System

Metric (m, kg, N, s, V, A) Degrees rad/s Celsius

Angle

Degrees

Rotational Velocity

rad/s

Temperature

Celsius

Structural Steel


TABLE 4

Model (A4) > Geometry

Properties

Volume

2.1621e-004 m³

Mass

1.6972 kg

Statistics

Nodes

9365

Elements

1635

Mesh Metric

None

TABLE 31

Structural Steel > Constants

Density

7850 kg m^-3

Coefficient of Thermal Expansion

1.2e-005 C^-1

Specific Heat

434 J kg^-1 C^-1

Thermal Conductivity

60.5 W m^-1 C^-1

Resistivity

1.7e-007 ohm m

TABLE 32

Structural Steel > Color

Red

Green

Blue

132

139

179

TABLE 33

Structural Steel > Compressive Ultimate Strength

Compressive Ultimate Strength Pa

0

TABLE 34

Structural Steel > Compressive Yield Strength

Compressive Yield Strength Pa

2.5e+008

TABLE 35

Structural Steel > Tensile Yield Strength

Tensile Yield Strength Pa

2.5e+008

TABLE 36

Structural Steel > Tensile Ultimate Strength

Tensile Ultimate Strength Pa

4.6e+008

TABLE 37

Structural Steel > Isotropic Secant Coefficient of Thermal Expansion

Zero-Thermal-Strain Reference Temperature C

22

TABLE 38

Structural Steel > S-N Curve

Alternating Stress Pa

Cycles

Mean Stress Pa

3.999e+009

10

0

2.827e+009

20

0

1.896e+009

50

0

1.413e+009

100

0

1.069e+009

200

0

4.41e+008

2000

0

2.62e+008

10000

0

2.14e+008

20000

0

1.38e+008

1.e+005

0

1.14e+008

2.e+005

0

8.62e+007

1.e+006

0

TABLE 39

Structural Steel > Strain-Life Parameters

Strength Coefficient Pa

Strength Exponent

Ductility Coefficient

Ductility Exponent

Cyclic Strength Coefficient Pa

Cyclic Strain Hardening Exponent

9.2e+008

-0.106

0.213

-0.47

1.e+009

0.2

TABLE 40

Structural Steel > Isotropic Elasticity

Young's Modulus Pa

Poisson's Ratio

Bulk Modulus Pa

Shear Modulus Pa

Temperature C

2.e+011

0.3

1.6667e+011

7.6923e+010