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Fracture of materials
破壊事故破面解析事例Ⅳ
④ (破壊の実例)
◎ ジェット戦闘機 「F‐111」の破壊事故 (1969年)
◎ 日航ジャンボ機墜落事故 (1985年)
◎ 高速増殖炉「もんじゅ」のナトリウム漏洩事故 (1995年)
◎ 京福電鉄事故、ブレーキ制御棒の破断 (2000年)
◎ 中華航空機墜落事故 (2002年)
⇒ 金属疲労による機体の空中分解による墜落。
⇒ 主翼の金具に疲労き裂が発生し、
このき裂のわずかな進展により早期運転中に破壊
⇒ 機体後部圧力隔壁が金属疲労により破壊し、機体もろとも御巣鷹山に墜落
⇒ 温度計さやの金属疲労が原因で、大量のナトリウムが漏洩
⇒ ブレーキ制御棒の金属疲労が進み破断に至った
Actual fracture accidents
Classification of fracture
Static fracture
13%
Corrosion
3%
Delay fracture、
Stress corrosion cracking 5%
Themal fatigue
Corrosion fatigue
Fretting fatigue
11% Fatigue
60%
Low cycle fatigue
8%
Ductile fracture
Classification of fractureⅠ
① Amount of plastic deformation
Vertical fracture Cup and cone
Type fracture
Chisel point
fracture
Shear fracture
(Separation of slip plane)
Fracture surface geometry Small plastic deformation
Brittle fracture Ductile fracture
Large plastic deformation
Classification of fractureⅡ
② Transgranular and intergranular fracture
Fracture occurs along grain boundary
Intergranular
fracture
Brittle fracture
Transgranular
fracture Ductile fracture
Fracture occurs in the grain
Intergranular and transgranular
fracture
Microstructure types
Brittle fracture
σ
σ
Classification of fracture III
Cleavage plane
(a) Cleavage fracture
(b) Shear fracture
③ Atomic level
τ
τ
Slip plane
Slip plane {111}
{0001}
{123}
{112} {110}
{1011}
{1010}
Cleavage
plane {0001} {100} Non
Materials
Al、Cu、Ni
Ag、Au
γsteel
Cr、Mo、V
W、β-Ti
Mild steel
Zn、Mg
Be、Sn
α-Ti
fcc bcc hcp
Relation between slip and cleavage plane
Fractography
Initiation of
crack
Crack growth Final fracture Fracture
surface
Fractography?
Method of observation and analysis of fracture surface
which records progress of fracture.
例.
River pattern
Process of fracture
Fracture shows peculiar appearance
Macro-fractography
Naked
Loupe
Angle/color
Appearance
Micro-fractography
Optical
Electon Microscopic
appearance
Characteristics of ductile fracture surfaceⅠ
Tensile fracture
Plain strain
Perpendicular fracture surface
Cup and cone type
Example
Geometry of fracture surface depends on
stress state.
Shear fracture Plain stress
Slant type (shear) fracture surface
Color of fracture surface : Gray
Macroscopic ~ Difference between
tensile and shear
Microscopic ~ Dimple formation
Characteristics: mentioned later Shear fracture
Chisel point
fracture
Characteristics of brittle fracture surfaceⅡ
Cleavage Geometry
Fracture pattern
Perpendicular fracture surface
Color : Metal gray
Roughness
Chevron pattern
Starter notch
Brittle fracture surface
Chevron pattern Fatigue crack Shear lip
Characteristics of fatigue fracture surfaceⅢ
・Low cyclic stress and thick plate
Slant fracture surface
Perpendicular; fracture surface
・High cyclic stress and thin plate
Ductile materials
Brittle materials
Perpendicular fracture surface
Color : Gray
(Brittle fatigue fracture ⇒ Metal luster
◎
For random cyclic stress
Beach mark
Fati
gu
e F
ina
l
fract
ure
(D
uct
ile)
Initiation point
Beach mark
Microscopic characteristicsⅠ(Ductile①)
25μm 25μm 25μm 25μm
(a) (b) (c) (d)
Tensile ductile fracture in stainless steel(28% Cr-9% Ni steel )
(Ductility); (a) < (b) < (c) < (d))
Microscopic characteristics of ductile fracture
Dimple … Many dips are formed
Ripple
Wavy pattern
σ1
σ1
σ1 σ2
σ1
τ
τ
σ2
M
M
σ1
σ1 τ
τ M
M
(a) Equaxed dimple (b) Elongated dimple (c) Elongated dimple
(Shear load) (Tear load)
Characteristics of ductile fracture surfaceⅡ
When crack propagates on
cleavage plane in which
dislocation exists,
River pattern is formed.
Characteristics of brittle fracture surfaceⅣ
20μm
River pattern for mild steel
at low temperature impact load
Characteristics of brittle fracture ①
River pattern
◎ Flow of river pattern
= Propagation direction of crack growth
◎ Crack initiation is in grain boundary
Fatigue cracks
Fatigue crack Fatigue crack Fatigue crack
Fatigue fracture Fatigue crack
Characteristics of fatigue fracture surface Ⅵ
2μm
Striation
(25% Cr-5% Ni steel)
Characteristics of fatigue fracture surface
Striation
Microscopic
Always don’t observe
Depending on loading、
point of fracture surface
Fracture mechanism changes
each stage of growth
Microscopic pattern depends on
each stage of crack growth
Ductile fractureⅠ
Ductile fracture
Macro ~ Cup and cone etc.
Micro ~ Dimple
a
b τ
τ
Theoretical shear strength
Perfect crystal without defect
O X
τ
Theoretical shear strength Next
Slip plane
X Elastic line in X=O
(τmax : Shear stress between atoms )
b
Xπ ττ
2sinmax
Ductile fractureⅡ
O X
τ Elastic line at X=O
a
XG G γ τ …( 4.2)
10
G
a
b
2
1max ≒
πτ G
…( 4.3)
( τ at X=0 )
b
X2
b
X2sin maxmax
πτ≒
π ττ
( For small θ ⇒ sin θ≒θ)
…( 4.1)
◎ Whiskerー
Material without dislocation
◎ Normal materilas
1/10 ~ 1/100
Ductile fractureⅢ Initiation and growth of void
(a) (b) (c) (d)
Cup and cone type tensile fracture process
Maximum
shear at
45 degree
Void : Initiates at inclusion and delaminate from matrix
Brittle fractureⅠ
Theoretical cleavage fracture strength
Brittle fracture surface
Macro ~ Chevron pattern
Micro ~ River pattern、Tonge
Brittle fracture
Absorbed energy : Small
Stored energy in material is
consumed to grow crack
Rapidly crack growth ⇒ Instant fracture
a0
λ/2
Balance position Displacement X
Str
ess
σ
Elastic line at X=0
σmax
Cleavage plane a0
X
σ
σ
Brittle fractureⅡ
(Stress-strain relation at X=0)
0a
X E E ε σ …( 4.5)
(Sine fuction)
λ
πσ≒
λ
π σσ
X2
X2sin maxmax
(For small θ ⇒ sin θ≒θ)
…( 4.4)
a0
λ/2
Balance position Displacement X
Str
ess
σ
Elastic line at X=0
σmax
a0 :Distance
between atoms
a
E
2 0
max
π
λσ
…( 4.6)
◎ Whisker
Without dislocation ⇒ Near value
◎ High strength steel etc.
Difference of one order more
Brittle fractureⅢ
a0
λ/2
Balance position Displacement X
Str
ess
σ
Elastic line at X=0
σmax
a
E
2 0
max
π
λσ
…(4.6)
Work used delamination of atoms
γπ
λσ
λ
πσλ
2 X2
sin max2
0max
dX
Two new free surfaces …(4.7)
Energy consumes formation of
new free surface
γ: Surface energy per unit area
10
E
a
E2
1
0
max ≒γ
σ
…(4.8、4.9)
Brittle fracture Ⅳ (Griffith’s theory①)
UE : Strain energy stored in plate
22
E2E
U cπσ
EU
22
E
σπc : Rigid solution
US : Energy to form crack plane
cc γγ 422Us
Next σ
σ
2c ρ
Free plane
Two planes
Fracture strength of perfect brittle material with crack
dc
dU
dc
dU SE
Criterion of fracture
…(4.12)
Brittle fractureⅤ ( Griffith’s theory ②)
E
c
dc
dUE
22 σπ
4dc
dUS
Crack length c
Rat
e of
ener
gy
Variation of energy rate
With increasing crack length
42 2
E
cσπ
2
1
2
c
E
πσ
Griffith’s equation
…(4.13)
(Plane stress state)
Fig. An oil barge that fractured in a brittle manner
by crack propagation around its girth
(The New York Times)
Classification of fractureⅣ
④ Loading and environment
Classification of fracture
Static fracture
13%
Corrosion
3%
Delay fracture、
Stress corrosion cracking 5%
Themal fatigue
Corrosion fatigue
Fretting fatigue
11% Fatigue
60%
Low cycle fatigue
8%
About 80% of fracture
was caused by fatigue
Impact failure
σ
t
Loading and fracture
Static, Environmental
Fatigue
Microscopic fracture surfaceⅢ(Ductile fracture③)
2μm
(a) Shallow dimple
25μm
(b) 組織
図.Two phase stainless steel (25% Cr-5% Ni steel)
Shallow
Microvoid along
grain boundary
Crack growth inside
Grain boundary
Elongated dimple
Microscopic fracture surfaceⅤ(Brittle fracture②)
20μm
図.High Cr ferrite steel(475℃ageing
Brittle fracture surface ②
Tongue appearance
… Twin deformation related
τ τ
Bound. Bound.
Twin
Fracture analysisⅠ
① Wire Rope failure to catch shark
Wire Rope ⇒ Macroscopic Large Necking
Ductile fracture Microscopic Dimple
5μm 10μm
(a) Equiaxed dimple (b) Elongated dimple
図.Microscopic appearance of wire-rope
Fracture anaysisⅡ
② Rail fracture surface
10μm
(a) Striation
Beach mark
(a)
(b)
Chevron pattern
(b) River pattern
15μm
(a) … Fatigue
(b) … Brittle fracture
Fracture anaysisⅢ
③ Bolt fracture surface for ship
Measurement of striation space
Fatigue crack growth rate
Beach mark
10μm
図.Bolt(SUS304)microscopic appearance
Striation
Under cyclic loading
Fatigue facture
Ductile fractureⅣ
◎ Microstructure effect
Void formation ⇒ Inclusion
・Content
・Distribution
・Size, Geometry
● Globular martensite
○ Ferriteト‐globular perrite
Sulfide
△ Ferrite‐layer perrite
Inclusion(2 phase) Vol.%
Duct
ilit
y
Sample geometry、Stress condition
Ductile fracture model
(McClintock)
Brittle fractureⅥ ①)
[Ⅰ] Mechanical factor ①
・ Low temperature
・ Loading rate
・ Notch
・ Thickness
Constrain of plastic
deformation
Locally stress increases
Brittle
Sharpy impact tester
Hammer
α β
h1
h2
Measure
Notched specimen
Potential energy of Hammer
Toughness evaluation
Sharpy impact test
Remained Energy after impact
Absorbed energy of material
+
=
(Toughness)
Brittle fractureⅦ
[Ⅰ] Mechanical factors ② (Ductile-Brittle Transition Behavior)
Rate of reduction
of area
Tensile test
Brittle
Ductile
-200 -150 -50 -100 0 50 100 150
0
20
60
40
80
0
80
160
40
120
Temperature ℃
Red
uct
ion
of
are
a %
Ab
sorp
tion
en
ergy
J
Ductile-Brittle Transition
Absorption energy
Impact test
Ductile-Brittle Transition
Temperature
Brittle fractureⅧ [Ⅰ] Mechanical factors ③
(Question) Which is the best steel for tanker?
Each steel is the same strength.
(a) (b) (c)
Temperature ℃
Ab
sorp
tio
n e
ner
gy
J
D.-B. transition temp. must be low
Temperature decreases
High risk of brittle fracrure
Ductile Brittle
Oil
Natural Gas Gas ⇒ Liquid
Under low temperature
Material must keep ductile
・ Notch effect
Notch induces Stress concentration and high three axis stress condition
・ Plate thickness
Thickness increases, Three axis stress condition becomes high.
(Ex. : Titanic sinked in 1912.4.14)
Brittle fractureⅨ
P, C, O, H etc.
Low toughness
σ
σ
Cleavage plane
[Ⅱ] Microstructure effect ① (Crystal structure, Chemical composition)
bcc crystal (Mild steel)
fcc crystal
(Cu、Al、Ni、18%Cr-8%Ni stainless steel)
Difficult brittle
Low temperature brittle
LiquidO2 orLiquidN2 vessel
C、P
Transition temp.
Ni、Mn
Brittle
Increase Urge
Decrease Restraint
Brittle fractureⅩ [Ⅱ] Microstructure ② (Carbon steel)
Temperature ℃
Ch
arp
y i
mp
act
en
erg
y
J
High carbon
High Transition temperature
Low absorption energy
Brittleness
C content of carbon steel
General
High strength Brittle
Fine grain
High strength Improvement of toughness +
Creep fractureⅠ(Creep phenomenon)
(Ex.
W Heating
Under a stress and temperature
Plastic deformation is induced.
Creep?
Failure
Time t
Str
ain
ε
Accelerated creep
Softening
Transient creep
Work hardening
Steady creep
Deformation depends on time
and loading
Work hardening Softening) Cancellation
Deformation ~ Stress and Time
High temperature
Creep fractureⅡ(Creep strength)
Failure
Time t
Str
ain
ε
Steady creep
Creep rate
Creep rate at steady creep stage
Small creep rate
Time to tolerance strain
=long using period
Creep strength
A constant stress of 100MPa
103 Hours
Strain=0.01%
(例)
Creep strength =100MPa at 0.01% / 103 h
Creep fractureⅢ [Ⅰ] Effects of temperature and stress [Ⅱ] Microstructure effect
Time
Str
ain
Stress increase
Temperature increase
Temperature and stress increases
Steady creep is dominant
Creep rate increases
Creep strength decreases
Time ℃
Ste
ad
y c
reep
ra
te %/
hr
Fcc crystal
High creep strength
Large Activated energy
Creep fractureⅣ
[Ⅲ] Grain size
Grain size refinement
Normal temperature=Low
Strengthening
Refinement strength
Creep strength decreases
Under high temperature
Grain boundary slip
High temperature
・ Substitutional element
Interaction between dislocation or vacancy is restrained
And then creep strength increases.
・ Stacking fault energy decreases, creep strength increases
Creep fractureⅤ
A
B C
A
B C
C
B
A
A
B C
⇒
A
B C
⇒
C
B
A
⇒
Void
Particle Cavity
Cavity
Grain boundary
W type cracking r type cracking
Two type intergranural cracking at high temperature creep