bracket model with direct transent results

CAD model verification of a simple bracket

sheet metal model

•Objective•Cad model•Manufacturing sheet.•Fea model•Basic analysis methods implemented.•Loading condition with respect to the analysis methods.•Material and property•The results•conclusion

objectiveTo do some thing “”FTP””

To verify the analytical skills with the help of CAD/CAE tool and also with the microsoft tool.

To verify the tool knowledge to achieve the goal.

The CAD model

Manufacturing model• 2.5mm sheet with aluminum alloy • 2.5mm sheet with aluminum alloy

Outer face with offseted FEA model

Direct Transient analysis (0-1.6 with

cosine function)1. Direct transient analysis:-

I. Magnitude and the location are same as static analysis with a function of cosine with phase 250 and time range is 0.0 to 1.6.

II. Boundary condition is same as static analysis.

Load and boundary condition in direct transient response analysis

Load and boundary condition for static x-directional loading

Load and boundary condition for static y-directional loading

Load and boundary condition for static Z-directional loading

Load and boundary condition for direct transient x,y,z-directional

loading Full constrained area

Load as per static with time function

Material selected for the component and its

Engineering property for analysis

Material and property• Aluminum alloy with SI unit

YOUNGS MODULUS

SHEAR MODULUS POISIONS RATIO DENSITY YIELD_STRESS_VALUE

7.00E+04 2.632E+04 0.33 2.80E-09 3.50E+04

Analysis results• Transient (direct ) analysis result

• X-directional load case• Spc-force & External force• Max- displacement and vonmises stress value and

region plot• y-directional load case

• Spc-force & External force• Max- displacement and vonmises stress value and

region plot• z-directional load case

• Spc-force & External force• Max- displacement and vonmises stress value and

region plot

X-directional load caseDirect transient response

analysis results

Reaction force and external force result in direct transient response analysis for x-directional

loading

Spc- force External force

x-directional load-caseMax displacement result Max vonmises stress result

Maximum value of Results corresponding to time in x-direction

X-DIRECTIONAL DYNAMIC_LOAD(0-1.6)

DISPLACEMENT(MAX)(Node-8266,7096)

time 0.266667 1.333333 1.599999

VALUE 1.62E+00 1.62E+00 1.82E+00

vonmises stress(max) Nodal_results

elements 10819/10845/10818/10847

NODE 5836

TIME 0.266667 1.333333 1.599999

VALUE 3.17E+02 3.17E+02 3.37E+02

elements 8995/9024/8996/9022

NODE 5786

TIME 0.266667 1.333333 1.599999

VALUE 3.17E+02 3.17E+02 3.37E+02

Y-directional load caseDirect transient response

analysis results

Reaction force and external force result in direct transient response analysis for y-directional

loading

Spc- force External force

y-directional load-caseMax displacement result Max vonmises stress result

Maximum value of Results corresponding to time in y-direction

Y-DIRECTIONAL DYNAMIC_LOAD(0-1.6)

DISPLACEMENT(MAX)(NODE-184,7212)time 0.266667 1.333333 1.599999

VALUE 1.27E+00 1.27E+00 1.42E+00

vonmises stress(max) Nodal_resultselements 8994/8995/9026/9024

NODE 5787

TIME 0.266667 1.333333 1.599999

VALUE 2.62E+02 2.62E+02 2.93E+02

 elements 10818/10847/10817/10849

NODE 7837

TIME 0.266667 1.333333 1.599999

VALUE 2.62E+02 2.62E+02 2.93E+02

Z-directional load caseDirect transient response

analysis results

Reaction force and external force result in direct transient response for z-directional loading

Spc- force External force

z-directional load-caseMax displacement result Max vonmises stress result

Maximum value of Results corresponding to time in z-direction

z-DIRECTIONAL DYNAMIC_LOAD(0-1.6)

DISPLACEMENT(MAX)(NODE-7507/5359)

time 0.266667 1.333333 1.599999

VALUE 2.33E+00 2.33E+00 2.62E+00

vonmises stress(max) Nodal_results

elements 10226/10227/10223/10224

NODE 7076

TIME 0.266667 1.333333 1.599999

VALUE 2.93E+02 2.93E+02 3.28E+02

elements 11285/11286/11288/11289

NODE 8250

TIME 0.266667 1.333333 1.599999

VALUE 2.93E+02 2.93E+02 3.28E+02

IT HAS TO BE FILLED

TO BE FILED

TO BE FILED

CONCLUSIONTHIS IS JOST THE BEGINNING

PICTURE ABHI BAKIHE

With thanks,Manas Ranjan Ray