lms fundamentals of durability rev5 - home - … curve, cycle counting loads and damage load...
TRANSCRIPT
![Page 1: LMS Fundamentals of Durability Rev5 - Home - … Curve, Cycle Counting Loads and Damage Load Characterization Establishing Durability Targets: Superposition, Extrapolation Durability](https://reader031.vdocument.in/reader031/viewer/2022013120/5a9ecf427f8b9a8e178be4bf/html5/thumbnails/1.jpg)
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Fundamentals of Durability
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Your single provider of solutions
3D simulation solutions
System simulation solutions
Test-based engineering solutions
� Troubleshooting interventions
� Development support from concept to final validation
� Sharing know-how and best practices
� Extensive trainings
Engineering services - Deployment services
From troubleshooting to “Design-Right-First-Time”
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Durability Agenda
S-N Curve, Cycle Counting
Loads and Damage
Load Characterization
Establishing Durability Targets: Superposition, Extrapolation
Durability Basics
Fatigue, Stress, Strain
Fatigue Life Predictions
Infinite Life, Stress Life, Strain Life
Load Determination
Measurements, Multi-Body Simulation
Accelerated Testing & Analysis
RP-Filter, Mission Synthesis
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Durability Engineering in Product DevelopmentC
ost
of
Ch
an
ge
Concept DetailDrawing
Prototype Production FieldFailure
Engineer
Troubleshoot
Validate
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Durability – Why is it important?
Warranty Costs• High rate of return is large liability• Example: Heavy truck
Competitive Advantage• Reputation for reliability• Example: Longest lasting appliance, safest aircraft
Performance• Over-engineering reduces performance• Example: Fuel economy on heavy car
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The Durability Process
Acquisition Analysis Shaker testingSimulation Sign-off
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EnergyWind turbine – blade failure / structural failure
“There is a general trend upward in accident numbers
over the past 10 years.”
Blade failure – 24 accidents in 2009
Structural failure – 15 accidents in 2009
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Civil construction2007 Minneapolis' I-35 Bridge Collapse (2007)
Kenneth Russell, professor MIT, suspects metal
fatigue could be a contributing factor “The bridge
was very near to the fatigue limit and had gone
through many cycles," he says.
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Turbine Blade Failure
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Wall
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Helicopter
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Tacoma Narrow Bridge
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What is fatigue ?Versailles rail crash (1842)
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What is fatigue ? Woehler (1870) railroad axles
Cyclic stress range Can be more important than peak stress
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Sir Robert Hooke
British
(1635-1703)
Tatsuo Endo
Japan
(1925 - 1989)
Famous People In Fatigue
Hooke’s Law of
Elasticity in 1660
Wohler
curves in
1867
August Wohler
German
(1819-1914)
Rainflow Counting in 1968
MA Miner
English
(1915 - 1978)
Miner’s Rule in 1945Goodman
English
(1869 - 1942)
Goodman’s Rule in 1899
Richard Von Mise
Austrian
(1883 - 1953)
Theory of Plasticity
1913
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Durability Agenda
S-N Curve, Cycle Counting
Loads and Damage
Load Characterization
Establishing Durability Targets: Superposition, Extrapolation
Durability Basics
Fatigue, Stress, Strain
Fatigue Life Predictions
Infinite Life, Stress Life, Strain Life
Load Determination
Measurements, Multi-Body Simulation
Accelerated Testing & Analysis
RP-Filter, Mission Synthesis
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Dynamic versus Static Failures
Cyclic Fatigue refers to gradual
degradation and eventual failure that
occurs under loads which vary with time,
and which are lower than the static
strength of the metallic specimen,
component or structure concerned.
The Static Strength is the load which
causes failure in one application.
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Static Strength
Aircraft Wing Bending Test
Bend till Break
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Dynamic (Cyclic) Loading
Dynamic Loads below Static
Strength vary with time
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Definitions
Durability is the ability of something to perform its function long-
lasting and repeatedly.
Failure is Industry specific. For example: Crack growth versus
crack initiation
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Fatigue Failures in Real Life
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22 copyright LMS International - 2010
Aloha airlines flight #243April 28th, 1988Maui, HI
Fatigue failure occurred due to repeated pressurization of the cabin causing a small crack to rupture in the fuselage, killing a stewardess.
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Crack Growth
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Definitions
Durability is the ability of something to perform its function long-
lasting and repeatedly.
Failure is Industry specific. For example: Crack growth versus
crack initiation
Fatigue is the progressive and localized structural damage that
occurs when a material is subjected to cyclic loading. Stress and
strain are used to calculate fatigue damage.
Damage – Measure of fatigue. When = 1 by Miner’s Rule, failure
occurs.
Fatigue Life – Inverse of damage (Example: 0.5 damage, is
fatigue life of 2)
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Stress
A
* Normal Stress
How to reduce Stress?
Either:• Increase Area• Reduce Force
Fn
σ = σ = σ = σ = Fn/A
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Stress
A
Fn
* Normal Stress
How to reduce Stress?
Either:• Increase Area• Reduce Force
σ = σ = σ = σ = Fn/A
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Stress
A
Fn
* Normal Stress
Either:• Increase Area• Reduce Force
Reduced cross-sectional area causes stress concentration
Effective Cross-
sectional area
σ = σ = σ = σ = Fn/A
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What about Simulation?
Fn
* Normal Stress
Finite Element Models are used
• When Fn=1: referred to as a “Static Unit Load Case”
• Stress is calculated at each element – as opposed to a predetermined location
• because real geometry is more complex than this . . .
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Strain
lo = original length
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Strain
lo = original length
dl = change in
length
Strain:
εεεε = = = = dl / lo
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Stress and Strain: Hooke’s Law – Young’s Modulus
lo = original length
A
Fn
σ = σ = σ = σ = E εεεε
E = Young’s Modulus
Strain
Str
ess
E is slope
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Sir Robert Hooke
British
(1635-1703)
Tatsuo Endo
Japan
(1925 - 1989)
Wohler
curves in
1867
Famous People In Fatigue
Hooke’s Law of
Elasticity in 1660
August Wohler
French
(1819-1914)
Rainflow Counting in 1968
MA Miner
English
(1915 - 1978)
Miner’s Rule in 1945Goodman
English
(1869 - 1942)
Goodman’s Rule in 1899
Richard Von Mise
Austrian
(1883 - 1953)
Theory of Plasticity
1913
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Stress and Strain: Hooke’s Law – Young’s Modulus
σ = σ = σ = σ = E εεεε
E = Young’s Modulus
Strain
Str
ess
E is slope
Yield Strength
Ultimate
Strength
Rupture
Time Lapsed Video
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Static Stress and Strain Relationship
A - Red – Fixed Area(Engineering Stress)
B - Blue – Changing Area(True Stress)
1 – Ultimate Strength2 – Yield Strength3 – Fracture Strength
1. Necking occurs, applied load decreases
2. Plastic Deformation Begins3. Fracture Occurs4. Strain hardening region5. Necking
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Materials Terms
Creep: is a time-dependent deformation of a material while under an applied load
that is below its yield strength
•Hardness: is the resistance of a material to localized deformation
•Toughness: the ability of a metal to deform plastically and to absorb energy in
the process before fracture
•Yield strength or yield point: of a material is defined in engineering and
materials science as the stress at which a material begins to deform plastically.
•Ductility: is a solid material's ability to deform under tensile stress
• The following list ranks metals from the greatest ductility to least: gold, silver,
platinum, iron, nickel, copper, aluminum, zinc, tin, and lead
• The ductility of steel varies depending on the alloying constituents. Increasing
levels of carbon decreases ductility
•Brittle: A material when subjected to stress, it breaks without significant
deformation (strain)
•Ultimate tensile strength (UTS), often shortened to tensile strength (TS) or
ultimate strength, is the maximum stress that a material can withstand while
being stretched or pulled before necking. Point at which load on specimen
decreases
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Graphical Representation of Material Terms
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Some Material Properties and Failure Modes
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Definition of the Stress Ratio R
t
σσσσ
σσσσm= 0R = -1
stress ratio R= σσσσlower
σσσσupper
σσσσu= 0R = -∞
0
σσσσl= 0R = 0
σσσσu= 2 σσσσl
R = 0.5
σσσσl = 2 σσσσu
R = 2
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Stress Ratio R Plotted On the Haigh Diagram
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Dynamic Stress/Strain Test
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Dynamic Fatigue: Crack initiation and crack growth
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What influences fatigue?
LoadsMaterial
Fatigue
Fatigue Life
Geometry
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What influences fatigue?
Loads•Load level•Uni-axial/multi-axial•Constant/variable
amplitude
Material :•Surface Finish•Residual Stresses•Basic Properties
Fatigue
Fatigue Life
Geometry:•Load Configuration•Notch Severity•Local Stress State
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failure: loading > strength
Applied loading vs. structural strength
LOADS
Material + Geometry
(structural strength)probability
density
strength criterion
Optimal Design – Minimal Overlap – Affordable CostOptimal Design – Minimal Overlap – Affordable Cost
more scatterless
scatter
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typical load ratios of 10% / 90% probability
manufacturinggeometry 1.02
material- controlled 1.15- different welds 1.45
loads (car) 2.00
Today, customer usage is the most
important source of fatigue scattering.
10% 50% 90%failureprobability:
life
load
usagestrength
Sources of Fatigue Scattering
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When were your durability test schedules established ?Applied loading vs. structural strength
probabilitydensity
strength criterion
Wider - Over-Design - More expensiveWider - Over-Design - More expensive
more scatterless
scatter
LOADS
Material + Geometry
(structural strength)
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Page 47 Siemens PLM Software
When were your durability test schedules established ?Applied loading vs. structural strength
probabilitydensity
strength criterion
NOT SO GREAT DESIGNNOT SO GREAT DESIGN
more scatterless
scatter
LOADS
Material + Geometry
(structural strength)!