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Grinding Ball Impact Analysis of a
Semi-Autogenous (SAG) Mill Shell
Liner Using Rocky DEM and ANSYS
Mechanical
Alexander Herr & Amit Saxena
September 17, 2019
The Elecmetal
Group
2
The Elecmetal Group
Winery
Metallurgy
Glass Bottle
Business
3
Communications Renewable
Energy
ME Elecmetal at a Glance
• ME Elecmetal is part of The ELECMETAL Group with over US$1 billion p.a. in revenues
• ME Elecmetal is a leading wear consumable supplier for mining, construction, and energy,
with net revenue over USD 600 million p.a.
• Range of products: Mill liners, crusher liners, grinding media and GET
• Range of services: Service Centers, Engineering and Design, Early Alert, ME FIT(1) System,
ME UpTime+
• 1,000 employees
• Customers in +35 countries around the world
• Manufacturing capacity of +134.500 tons in 5 foundries facilities
• Manufacturing capacity of +400.000 tons in grinding media
4
We are Global
5
Analysis of
SAG Mill Liner
Impacts
6
Study Objective
•
Develop an impact model with FEA analysis
•
Develop a 3D DEM model
•
Show set-up and results from a coupled DEM/FEA
simulation and analysis.
•
Study the influence of operational parameters like
speed on impact forces and resulting stresses
•
Study the influence of liner design on impact forces
7
SAG Mill Operation
•
Semi-Autogenous Grinding (SAG) Mill
•
‘Semi-autogenous’ mills include ore pieces, steel balls
(grinding medial), and water.
•
The mill shell is lined with ‘shell liners’ designed to improve
ore comminution and survive long enough to minimize
downtime.
•
Ore particle comminution takes place in a SAG mill by: oreore, ore-ball, and ore-liner impacts.
•
Steel balls are introduced into mill at a size and rate
determined by mill operator.
•
Balls available in sizes up to 6¼” (160 mm) diameter and
weighing 35 lbs.
•
Water flows through the mill, aiding in the discharge of small
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particles.
SAG Mill With Grinding Media
Basic Parts of a SAG Mill
•
A: Mill Shell – externally visible structure of the mill
•
B: Shell Liners – protect mill shell during comminution
• Consists of high (rose) and low (maroon) lifts in this design
•
C: Grates – allow for the discharge of small/fine ore particles from
grinding chamber
•
D: Pulp Lifters – (not visible here) behind grates, allow for
discharge of ore as the mill spins
C
B
A
Internal View of SAG Mill
Assembly
Operational SAG Mill
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Study Objective
•
After a certain period of operation, liners get worn down or
broken
•
Relining — replace the spent liners with new liners
•
How can we design new liners that are better than the current
design? More failure resistant & longer lasting?
How to reduce liner failure risk?
•
Develop better alloys with higher hardness and toughness
•
Reduce impact force on the liners while
This study focuses on measuring impact
forces and resulting stresses
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Toe Nailing at the Grate Ribs
Examples of Heavy Peening
Peening on the Shell Liner Lifter
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Metal Flow inside the Grate Slots
Methods for
Analyzing Impacts
Inside a SAG Mill:
1)
2)
Analytical Method
DEM-Based Methods
a) De-coupled DEM/ANSYS
b) Coupled Rocky/ANSYS
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Analytical Model
An analytical model for a grinding ball flight inside a SAG mill
Absolute Velocity
Relative (Impact) Velocity
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Ball Speed vs Critical Speed
•
The absolute speed of the grinding ball reaches maximum at 80% CS
•
The relative speed between the ball and the liner reaches the peak value at 65 to 70% CS
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Eq. Free Fall Height vs Critical Speed
• The impact force shows similar variation pattern with mill speed for all size mill
• Maximum impact force occurs at 65% to 70% CS
• The larger the mill diameter, the stronger impact force it generates
Equivalent free fall height for the ball-liner impact in SAG mills of diameter from 26 to 40 feet, rotation
speed from 50% to 85% critical speed
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Summary of DEM
Simulations
Discrete Element Method
•
Discrete Element Method (DEM) – A stochastic numerical method
for computing the motion and effects of a large number of particles.
•
The inside of a mill is a very difficult environment to know what is
happening: dark, wet, hot, full of water and dust particles.
•
Given reasonable assumptions about materials and particles, DEM
provides reasonable simulations of the events inside a mill.
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Features of Rocky DEM
•
Capable of simulating particles of various
shape and stiffness
•
Increased solving speed with multi-CPU,
GPU, and multi-GPU solvers
•
Full integration into ANSYS Workbench
including sharing parameters
•
Particle breakage models
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DEM Analysis SAG Mill
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SAG mill size: 22’ x 9’
•
Variable speed mill
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Analyze particle (balls & ore)
trajectory
•
Power draw
•
Maximum impact force magnitude
•
Large collision frequency
Full view of high lift (upper/left) and
low lift (right/lower) shell liner
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DEM Setup Steps
•
Select simulation type:
•
Mill data including:
•
Simplify geometry
•
Input data above
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Symmetry constraints (if applicable)
• Mill shell section
• Discharge end
• Wear (if applicable)
•
•
•
•
•
Rotational velocity
Ore density
Particle fill level
Particle size distribution
Mill power draw
Model Setup Within RockyDEM
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Parameterization in Rocky
•
Advantages of solving DEM simulations
in ANSYS:
•
Ability to link to other physics:
•
Any quantity can be parameterized:
• Transient stress responses
• Include water/slurry with Fluent
Setting up an Expression within Rocky DEM
• Geometry
• Rotational velocity (shown at
right and below)
• Fill rate, material distribution
• Material properties
• Etc
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Coupled Simulation in ANSYS
•
Rocky transfers impact-induced pressures to
ANSYS as surface pressure loads.
•
Rocky output allows loads to be exported for
selected geometries.
•
Pressure loads are mapped onto applicable
surfaces
• Mapping is maintained throughout
the motion of the part(s).
Light-colored high and low lift have a
fine mesh in Rocky and loads exported
to ANSYS.
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Simulation Steps
2) Begin rotation (3 – 9 seconds)
12 rpm in this instance
Chaotic initial rotation
Particles are colored based on translational velocity
1) Fill mill slice section (0 – 2.5 sec)
18% in this instance
Note: Symmetry is turned on. Particles that leave one
side return on the other.
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Simulation Steps
3) Steady state rotation (16 – 20 seconds)
12 rpm
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Comparison of Charge Motion
Particle motion at 3 rotational velocities, t = 20 seconds.
Particle motion at rotational
velocity of 10 RPM.
Particle motion at rotational
velocity of 12 RPM.
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Particle motion at rotational
velocity of 14 RPM.
Power Draw Level
Average Power Draw at 3 Rotational Velocities
1200
1000
kW
800
600
400
200
0
10 RPM
12 RPM
14 RPM
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Parameters from Rocky/ANSYS
Design Points in ANSYS Workbench
•
Design points, shown above, include inputs from SpaceClaim/geometry and Rocky
simulation module.
•
Output stresses come from ANSYS Transient solution.
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Comparison of Charge Motion
Particle motion of 3 geometric modifications.
Rotational velocity = 12 RPM, t = 20 seconds.
‘Low’ lifts height increased 30
mm.
‘Low’ lifts raised 30 mm.
‘High’ lifts raised 12.7 mm.
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‘Low’ lifts raised 60 mm (equal
height to high lift).
ANSYS Setup
Mesh size is similar (20 mm) to the
discretization in Rocky for pressure
transfer.
Mapped pressure applied to the
highlighted surfaces.
Lower mill liner surfaces are fixed.
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ANSYS Transient Stress Results
Screen capture of the maximum
equivalent stress over the 10 seconds
of simulation time (18 sec of Rocky).
Video of stresses induced by particle loads - transferred from
Rocky within ANSYS Workbench, 12 RPM design point.
Note: lower blue stress bands have been modified to show
low stress variation over time.
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Rocky/ANSYS Synced Videos
Synchronized video of shell liners of interest in Rocky and
ANSYS over 10 seconds of simulation time (@ 12 RPM).
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Parameters from Rocky/ANSYS
•
Shown at right, generally
stress in the shell liners
increases as the rotational
velocity increases.
Due to randomness, even as
particles gain energy – at
higher rotation speeds –
they may not contact liners
directly.
Rotational Velocity vs. Max Equivalent Stress (psi)
Maximum Equivalent Stress (psi)
•
Varying Rotational Velocity in ANSYS
Workbench
7000
6000
DEM Run 1
5000
DEM Run 2
4000
3000
2000
1000
0
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10
11
12
Rotational Velocity (RPM)
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13
14
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Comments on Fatigue
•
Although the stresses in this example are relatively low, for larger mills, shell liner
impact energies increase exponentially with increases in diameter.
•
Liner life typically ranges from 3 – 9 months. At 12 RPM an impact every revolution
leads to ~500,000 cycles/month.
•
ANSYS fatigue functions, including the SMART Crack feature, allow modeling of
semi-elliptical or arbitrary crack front and visualization of crack propagation.
Minor Axis
Previous work with semi-elliptical
crack analysis has been done to
look at the potential for fatigue
failure.
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Major Axis
Uncoupled
Explicit
Dynamic Impact
Simulation
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Evaluate Impact Stresses
Example Mill 40’ (12.2 m):
Ball Size:
6 1/4 “
Falling Velocity:
52.5 ft/s (16 m/s)
Mill Rotational Velocity:
22 ft/s (6.7 m/s)
Ball Energy
0.5 kCal (2.1 kJ)
To find the worst case impact, particle size, velocity,
trajectory, and mass are extracted from the DEM and
applied to a grinding ball for an explicit impact
analysis.
Impact location(s) are chosen at suspected weak
points or at locations where breakage is observed.
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Equivalent Stresses -Surface
Impact on Liner Leading Face Radius
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Equivalent Stress– Cross Section
• Compressive Yield Strength = 871.9
Mpa
• Tensile Yield Strength = 799 Mpa
• Ultimate Tensile Strength = 1235 MPa
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Reaction Force – Ball/Shell Liner
38
•
Max Impact Force = 1.7
MN
•
Max Impact Force from
DEM Calculation = 45kN
Kinetic Energy of Impact
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Facts About DEM
•
DEM provides a more realistic numerical analysis for liner-particle
interactions inside the mill
•
DEM can capture the effect of mill liner structural factors like lifter height
•
DEM can also capture the effect of operational parameters like mill speed
•
DEM provides a direct measure of impact forces on the liner, which is one of
great contributors to liner failure in service
•
DEM has gained common acceptance for understanding the behavior of
particles inside the mill
•
DEM requires validation with experimental calibration
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Rocky DEM in ANSYS Workbench
•
•
Provides a streamlined method for running mill optimization studies.
Frequently these studies vary one or more of these parameters to optimize grinding
efficiency:
•
•
•
•
•
Shell liner design (angle and/or height)
Total charge level
Ball size
Ball:Ore ratio
Rotational velocity
•
DEM coupled with impact force results and frequency of collisions helps with better liner
design selection through relative comparisons of these parameters
•
Provides predictive results for new designs to mitigate the risk of future part breakage
•
The FEA model can be further developed to conduct high-cycle fatigue and predict liner life
41
Acknowledgements:
Thank you to Rahul and the
Rocky Support Team for their
help:
Ahmad
Saurabh
Guilherme
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