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UT IMPORTANT THEORY / NUMERICALS / LOGICS
HIGH LIGHTS
1. Ultrasonic Wave Energy
Energy α Z A2
Energy α
ZA2
– (1)
Energy α
P2
– (2) A = Amplitude
Z P = Pressure of piezoelectric Crystal
Z = Acoustic ImpedanceA = AmplitudeP = Pressure of piezoelectric Crystal
P α ZA – (3)
(Note : Two questions may come from these formulas)
• Elastic force = The force keeps the atoms of a body in a defined pattern• Sound = Vibration transmitted point to point• Sound waves are also called elastic wave or mechanical wave. Related Terms with sound A, E, P, V• Velosity depends on elastic cons. & density (Note : Question may come from this concept)• Frequency of a given sound is always constant
2. Wave Mode
a. Longitudinal / Compressional / Pressure (VL)
In this mode propagation of wave is parallel to the dispersion of automs.
b. Transverse / Shear (VT)
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UT IMPORTANT THEORY / NUMERICALS / LOGICS
Only exist in solid, wave propagation perpendicular to this dispersion of atoms.
Polimarisation is possible only in shear wave.
VT ≈ 0.5VL
__________ (4)
3. Surface wave / Reyleigh Wave (VR)• Partical Motion of surface wave is elliptical• As the depth increased the degree of energy decreased drastically.• Penetrates upto one wave length
VR = 0.9 VT ________ (5)
4. Plate Wave / Lamb Wave• This kind of wave is being generated by special method. Better to consult ASM Vol. 17 for details.• This is of two type
• Velosity of plate wave depends on Type of lamb wave Frequency Thickness Elastic constant & Density
Z = VxD _____________ (6)
RE = (Z2-z1)2 _____________ (7)(Z2+z1)2
Medium RE TEWater / Persfex 0.1 0.9
Water / Al 0.7 0.3Water / Steel 0.9 0.1
dB = 20 log10(A2/A1) – (8) ZC
= ZP x Zm
Zc = geometrical means of Zp & ZmZp = Impedance of Probe
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Symmetrical Plate WaveUpsymmetrical Plate Wave
UT IMPORTANT THEORY / NUMERICALS / LOGICS
Zm = Impedance of MetalZc = Impedance of Couple
Acoustic Mismatch (Z2-Z1) RE increases
Unit of Z = kg/m2s
[Elastic Arisotropy & Acoustic Arisotropy]
Concept: When layer of couplant is less than λ, the energy loss depends on the layer of couplant.
At couplant thickness λ/4, the maximum transmission is taken placeAt couplant thickness λ/2, the minimum transmission is taken place
SNELL’S LAW
Sinθ1=
Sinθ2
9
V1 V2
1. Concept of Critical Angle
Condition - (1) Longitudinal wave generates in the probe which in the second media (material to be tented) produces two different wave mode (VL & Vs)
Condition - (2)
θc1 is called 1st Critical Angle
ie.
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Sinθc1=
Sin900
VL1 VL2
UT IMPORTANT THEORY / NUMERICALS / LOGICS
Condition - (3)
θc2 is called 2nd Critical Angle
Ie.
i
When V2 > V1 beam will be DIVERGED in second media
i
When V2 < V1 beam will be DIVERGED in second media
Concept of lensed probe (Mainly used in Immersion Testing)
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Sinθci =V1
10V2
Sinθc2=
Sin900
VL1 VL2
Sinθc2 =V1
11V2
F =•• R X VL (LENSE)
12
VL – VW
(Water)
UT IMPORTANT THEORY / NUMERICALS / LOGICS
OFF-SET DISTANCE FINDING METHOD
AB = DOA = D/2 = RAC = MN = OFFSET DISTANCE = X
Pto 13 Photo 13
Sinθ AC=
XOA R
ie.
Again,
OR
OR
OR
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n = • VL (LENSE)13
VL – VW
(Water)
f =•
Rn
14n – 1
X= Sinθ 15 R
Sinθ=
Sinr
VW VM
Sinθ =VW
X Sinr
16VM
X=
Sinr
R VM
x = RVW
Sinr
17VM
UT IMPORTANT THEORY / NUMERICALS / LOGICS
xm = focal spot in metal
(Convergent beam with greater refraction angle)
18 Fw = Focal Length in water xw
= Water path
19 Nm = Near filed in metal Nw = Near Field in water
COME BACK TO LIMITED ANGLE (θ)
20
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xm = Fw-XwVW
VM
Nm = (Nw–Xm)X
VW
VM
Sinθ =IDOD
Sinθ =IDOD
=OD-2T
OD
= 1 - 2TOD
or,= 1 -
2TOD
T = Thickness of pipei.e., ID = OD-2T
Focal spot in water
(Incase metal piece is not placed inside water; focal point distance was FW)
UT IMPORTANT THEORY / NUMERICALS / LOGICS
Again
VLM = longitudinal Velocity in WaterVTM = Transverse Velocity in Hollowbar inside the water.
or
IMMERSION METHOD
Minimum water path = 1/4t + ½” of water when the immersed material is steel.
Acoustic Lense:
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or, T = (Sinθ –
1) X
OD21
2
Sinθ =x XID OD/2
Sinθ =2x •
22OD
Sinθ=
SinrLW VTM
Sinθ =
SinrVLW
23VTM
Min. water path =
Material Thickne
ss X
Vw 24
VM
UT IMPORTANT THEORY / NUMERICALS / LOGICS
Come Back to Snell’s Law:
ie.
An example based on eqn. 25
• Incase sound travels 10mm in water, what will be the equivalent traveling distance in steel.
So, Dist. Steel =
PHASE REVERSAL
If Z2 < Z1 RP is –ve & this is called phase reversal.
When Z2 < Z1 Wall is called Soft wall When Z1 < Z2 this is called Hard wall
Phase Reversal takes place in soft wall condition
Radiofrequency (RF)
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Sinθ1=
Sinθ2 = Velosity = Dist. (Thk) X TimeV1 V2
Or time = Velosity Thickness
VLW=
VL Steel25
Dist (W) Dist. Steel
VL Water
=VL Steel
10 Dist. Steel
10 XVL Steel
mmVL Water
10X6.0 mm
•
= 40 mm1.5
RP =Z2 –
Z1Z2 +
Z1
Z1 •
• wallZ2
UT IMPORTANT THEORY / NUMERICALS / LOGICS
Hard Wall
Soft Wall (Phase Reversal)
Passage through material
Pure Absorption Due to 1. Elastic Hystarasis 2. Thermal Condition 3. Internal Friction
Loss of Energy
Loss of Energy due to scatter at grain boundary Energy α e-(αa x) (1)
Loss of energy at scatter Energy α e-(αe - αs)x (2)
Adding (1) & (2)
Energy & e-(αa + αs)x (αa + αs) = attenuation coefficient x = distance
(with distance increase, sensitivity decrease)
26
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Sinθ/2 1.22 λD
UT IMPORTANT THEORY / NUMERICALS / LOGICS
27
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N =D2
4λ
UT IMPORTANT THEORY / NUMERICALS / LOGICS
0
1 2
Note: f2 – f1 = Band Width
28
Amplitude α D2 (D=Probe Dia)
Important ConceptAmplitude α
1Dist2
GIVE ATTENTION TO FOLLOWING IMPORTANT CONCEPTS
E λ P R S DZ
N BS
SPEED
FREQUENCY DIA OF PROBE
Note:E λ P R S D
ZN B
SENERGY
Wave length
Penetratio
n
Scatter at Grain Boundary
Sensitivity
Dead Zone
Near Zone
Beam Spread
• Scatter (λ) ↑ Grain Size ↑• Damping ↑ Pulse Lengh Pulse Energy • Due to damping pulse energy decreases and band width increases• Pulse width to half of the wave length is called the maximum damping• Highly damped probes called broad band probe
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Quality factor (QF)
=f0
f2 – f1
UT IMPORTANT THEORY / NUMERICALS / LOGICS
• Very high damped probes called sock wave probe.
• Damping ↑ QF • Roof angle of TR probe ↑ dead zone effective range • TR probe has better signal to Noice Ratio• QF ↑ Penetration ↑• For coarse Grain Higher Dampened probe Required• Broad Band Beam Required Broad Beam amplifier• Tighter or narrow beam probe is giving better lateral resolution• Higher the damping better depth resolution. Therefore broad band will have small pulse
length and provide better depth resolution• In shock wave probe, Dead zone is very less (about 2mm only), shock wave probe is very
high damping probe & best for surface resolution• Delay block is having better near surface resolution• Higher damping shorter the pulse duration, shorter the dead zone. Higher the damping,
Higher the band width and lower the QF, lower the dead zone, lower the pulse duration.
GENERATION OF PULSE
1. Magnetostriction (40/50 kpsi)
2. EAMT probe
No need to touch the job
3. Phase Array
Photo
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UT IMPORTANT THEORY / NUMERICALS / LOGICS
4. Piezo electric effectPiezo electric effect Defecting ultrasound
Photo
QUARTS CLASICFICATION
1) Lithium Sulphate2) Barium Titanate & Lead Zirconate Titanate > Ceramic Crystal
USING OF CERAMIC CRYSTAL
Ceramic crystals are made by powder metallurgy process. After the shaping of barium Titanate and leas zinconate Titanate, the are gone through a high pressure and high temperature & under a high electric field. This is called polling. Therfore by poling the crystals are oriented in manner as per the figure. In an effect during the application of pressure they can contract & expand in longitudinal direction.
In case they are not going through poling, the crystals are not kept in such manner and as a result during the application of pressure (current), the expansion of different crystal particles will be in different direction and ultimately there shall not be any generation of pulse.
Photo
This vibration is called the fundamental frequency if Ø > 10t at fundamental frequency
then t = λ / 2 29
l =4λ = 30
2
n = 1, 2, 3, 4, 5….
When n = 1, this is fundamental frequency & when n is other than l, it is called harmonic
tC =λ
=Vc
312 2fc
Vc = Velosity of sound in crystal material.
1. Through Transmission
Max. intensity at fundamental frequency. Now a days it is trying to make all the probes at its natural frequency.
t= n
λ2
f1 = V
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UT IMPORTANT THEORY / NUMERICALS / LOGICS
n • 322t
f2 =
(n+1)
v
• 332t
Photo
2. Resonance
Resonance method used for the measurement even for low thickness other application of this method is to check the bounding condition.
3. Pulse Echo (**)
Pulse Repetitions Rate – It PRR is very high, ghost echo may appear (PRR, PRF)
Photo
PRR CALCULATION (IMMERSION TEST)
The reflected beam should be arrest by the probe.
Vel =DistanceTime
Formula (36) is for one pulse but generally minimum 3 pulse on interrogation are required. Therefore the modified formula is:
Note : n = No of Pulses
Again go back to clause 3 (**) above;
In order to avoid ghost echo next pulse should come after dying of the first echo.
Time between pulses velocity
=
DistanceTime
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Vscan =Ø + d
34
time
Time =1 35
PRR
Vscan = (Ø + d)
* PRR
36
Time =(Ø + d) PRR 37
n
UT IMPORTANT THEORY / NUMERICALS / LOGICS
Vm = 2 x thk job38
Time
T = 2 x n x tjob 39
Vm
Next Signal should appear after ‘n’ echo taken place
T = 2 x n x tjob 40
Vm
PRR = Vm41
2 x n x tjob
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UT IMPORTANT THEORY / NUMERICALS / LOGICS
Internal Mode Conversion
Internal Mode conversion
PHOTO
PHOTO
PHOTO
So for root crack 600 probe should not be used but for lack of side wall fusion 600 probe is ideal.
Beam profile of normal beam probe
PHOTO
Sound goes all the where due to interference
Constructive Interference at the nature axis
Beam profile is result of sound interference
Probe should have highest sensitivity at the centre
Transmission zone roughly two times the near zone
Beam profile
Sin r/2 = K. λ42
D
OR
Sin r/2 = K. V job43
D DC fc
At Near Field zone sensitivity is less as the location & size identification is critical.
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UT IMPORTANT THEORY / NUMERICALS / LOGICS
PHOTO
DGS (Dis. Gain, size) is a multiple DAG Curve.
In DGS, only FBH are used whereas in DAC SDH, notches, FBH are used.
In FBH 1mm = 20% then 2mm = 80%
but in SDH, no formula exists. Only we can say instead of 1 mm in 2 mm amplitude will be increased.
dB = 20log A1 43A2
PHOTO
dB Ration2 1.25 : 16 2 : 120 6 : 126 19.9 : 144 158:160 1000:1
Why TR probe is not having any initial Echo
PHOTO In Normal Beam initial pulse is going directly to amplifier and also going from normal beam. Due to its one part directly transfer to amplifier, initial pulse is appearing
PHOTO But as per the second figure in TR probe, no pulse can go directly to the amplifier. It has to go through Transmitter to job to Receiver to Amplifier. That is the reason there is no initial echo.
PHOTO
PHOTO
PHOTO
PHOTOAt position (1) which is the second multiple echo from the delay block and in that position no defect
When a separate circuit produce current in phase & out phase, it changes the damping characteristic. When it is in phase with probe frequency, it shortend the probe length or it increases the pulse
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UT IMPORTANT THEORY / NUMERICALS / LOGICS
height and the probe is dampenedWhen it is in reverse phase, it shortened the pulse heightPHOTO Max. height at fundamental frequencyPHOTO When it is dampened, Broad band
results with low quality frequencyPHOTO Delay BackPHOTO Delay ThicknessPHOTO
At position (1) which is the second multiple echo from the delay block and in that position no defect from the job is detectable, that is the reason delay blocks are used for a specific thickness which is turn classified as equivalent thickness of material.
Reflector plate Echo Technique
For thin plate & composite section
PHOTO PHOTO
In immension test, contour surface deliver broad pulses, therefore for better result focused probes should be used during scanning of countour surfaces.
Paint Brush probe or Linear Mosaic probe
When multiple probes are in a line, this is called paint Brush probe / Mosaic probe.
THE CONFIGURATION OF A MOSAIC PROBE
PHOTO
“Mosaic” for a known area to be tested.
SCANNING SPEED CALCULATION (For Plate)
PHOTO W = Width of the plateL = Length
So area scanned / see = s x w Total area = L x W
Time = L x WS x W
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PHOTO Case 1PHOTO Case 2PHOTOPHOTO
Countour connection lesnse where the countour of the probe is equal to the curvature of the pipe.This is also a countour corrective probeThis is a focusing probeLine focusing probe
UT IMPORTANT THEORY / NUMERICALS / LOGICS
Effective scan area = Probe area – overlap So, W = Probe Ø – overlap
SCANNING SPEED CALCULATION (BAR / TUBE)
PHOTO Circumference Speed(Sc) =
∏ x D x RPM
Linear Scanning Speed (Sl) =
W x RPM
W = Scanning Index = (Probe Diameter Overlap)
Time Taken (T)
=
S47
L
A-SCAN
PHOTO
• Synchronizer Circuit also called Timer Circuit / Clock Circuit. It controls the PRR• Pulser – It gives a higher voltage pulse to the probe (-ve voltage). Voltage Range used before pulser to
delay next voltage.• Sweep circuit – Range control is on the sweep circuit.• Receiver
PHOTOPHOTOPHOTORejects cut off equal heights from all echos.
AMPLIFIER BAND WIDTH
The range of frequency a amplifier can control is called Amplifier Band with.
Amplifier Band width – Narrow Band (2-4 Mhz)Amplifier Band width – Broad Band (0.5-4 Mhz)
Note: Amplifier width control is on the amplifier site & not change the probe frequency.
Broad band amplifier should use with the broad band width probe.
DYNAMIC RANGE OF DISPLAY
Ratio of defects that can be presented on the CRT called Dynamic Range of Display.
dB control helps to increase the dynamic range of display.
MONITER CIRCUIT / GATE CIRCUIT
To selectively monitor the part of the CRT and this is called Gating. Therefore two controls are the Gate start control or Gate Central Control
Page 19 of 21
UT IMPORTANT THEORY / NUMERICALS / LOGICS
Gate width
Gate threshold – It is a gate of ampude. Any defect amplitude beyond threshold will not make audiosound.
Node Error
PHOTO On amplification the cut of is shifted, this is called nodal error. In order to avoid nodal error, M/s. Should be calibrated on the peak of the amplitude.
(Detail of other connections to pulser in A-Scan system)
In A-Scan Amplifier connected to vertical plate & sweep Generator is connected to Horizondal.
PRR circuit may be separate or the part of clock / synchronizer.
B-Scan
PHOTO Sweep circuit is connected to vertical axis. Therefore in B-Scan only sweep line will be shown
X PositionSensor shows the position of the probe on x axis
PHOTO
PHOTO So B-Scanning gives the depth & size along the scanning direction.
PHOTO PHOTO
PHOTO PHOTO
PHTO
Good depth information may be possible on latest m/s with multiple gating x and color coding.
C scan also called P-Scan
Scanning angle consideration during scan from a Taper Surface
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UT IMPORTANT THEORY / NUMERICALS / LOGICS
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