bracket model with direct transent results
DESCRIPTION
same bk_with direct time dependent loading condition with results but the approach is deferent from the industry.TRANSCRIPT
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