11. Directional PropertiesDirectional Properties
Both strength and ductility are affected by the rolling
direction of the metal. The three axes of rolling
direction are referred to as the X, Y, and Z directions.
12. Rolling DirectionsRolling Directions
X Direction Best Strength & Ductility
Y Direction 10 - 30% Less Strength
20 - 50% Less Ductility
2 Direction Still Lower Strength & Ductility
24. Ductile - to - BrittleDuctile - to - Brittle
Transition TemperatureTransition Temperature
“The temperature at which a metal fracture mode
changes from ductile to brittle”
29. Chemical PropertiesChemical Properties
• Metals are mixtures of elements, and are referred to
as alloys
• Minor changes in alloy composition can have major
effects on alloy properties such as mechanical
strength, corrosion resistance
30. Common Steel AlloysCommon Steel Alloys
Common Name C % Typical Use Weldability
Ingot iron .03* Deep drawing Excellent
Low C .15* Electrodes Excellent
Mild Steel .15-.30 Structural Good
Medium C .30-.50 Machinery Fair
High C .50-1.0 Springs, dies Poor
* Single values are maximums
31. Low Alloy SteelsLow Alloy Steels
• High strength, low alloy
• Automotive & machinery
• Low temperature
• Elevated temperature
32. High Alloy SteelsHigh Alloy Steels
• Corrosion resistant
• High temperature
• High strength
34. Elements in Steels - 1 of 2Elements in Steels - 1 of 2
• C - Most important
• S - Undesirable
• P - Undesirable
• Si - Deoxidizer
• Mn - Combines with S
• Cr - Hardenability, Corrosion Resistance
35. Elements in Steels - 2 of 2Elements in Steels - 2 of 2
• Mo - Hardenability
• Ni - Toughness, Ductility
• Al - Deoxidizer
• V - Hardenability
• Nb - Stabilizer
46. Area of a Circular Cross SectionArea of a Circular Cross Section
Example 1Example 1
Area (circle) = π x Radius2
= R2
= π x Diameter2
= D2
4 4
Sample Diameter, D = 0.505 in.
Sample Radius, R = 0.2525 in.
Area = 3.1416 x 0.25252
Area = 0.20 in2
52. Percent ElongationPercent Elongation
Original gage length = 2.0 in.
Final gage length = 2.6 in.
%Elongation = final length - original length x 100
original length
%Elongation = 2.6 - 2.0 x 100 = 30%
2.0
53. Percent Reduction of AreaPercent Reduction of Area
Original area = 0.2 in.2
Final area = 0.1 in. 2
%Reduction of area (%RA) = ?
%RA = original area - final area x 100
original area
%RA = 0.2 - 0.1 x 100 = 50%
0.2
76. Fatigue TestingFatigue Testing
• Prepare samples
• Test series of various loads
• Test to failure, record cycles
• Test at maximum load vs no failure
• Plot data
• Determine endurance limit
77. Chemical TestingChemical Testing
Determines Chemistry of MetalsDetermines Chemistry of Metals• Spectrographic
• Combustion (CO, CO2 determination)
• Wet chemistry (titration)
• X-Ray fluorescence (XRF)
82. Heat Treatment - 1 of 3Heat Treatment - 1 of 3
• Mechanical properties are often very dependent upon
heat treat condition
• Many types of heat treatment
• Determine heat treat condition prior to welding on
base metal or mech. testing
• Consider effects of welding on heat treat condition
and mechanical properties
83. Heat Treatment - 2 of 3Heat Treatment - 2 of 3
Heat Treatments For Steels:
• Preheating
• Stress Relieving
• Normalizing
• Annealing
• Quenching and Tempering
• Others
84. Heat Treatment - 3 of 3Heat Treatment - 3 of 3
Heat Treatments For Stainless Steels:
• Preheating
• Stress Relieving
• Solution Annealing, Water Quench (Solution
Treatment)
• Quenching and Tempering
• Others
More on heat treating in Module 8
Hinweis der Redaktion
WIT Pg. 6-1
Instructor Should Explain:
This Module Will Cover Mechanical and Chemical Properties of Base and Filler Metals As Well As Destructive Testing. This Will Help to Provide a Base for the Information Provided in Module 8, “Welding Metallurgy for the Welding Inspector”.
WIT Pg. 6-1
Instructor Should Explain:
Items listed on slide are critical for proper use in fabrication.
Structure Dependent Properties Include:
-Strength-Ductility-Hardness
-Toughness -Fatigue
Analysis Dependent Properties Include:
-Corrosion Resistance
-Electrical Conductivity
-Modulus of Elasticity
WIT Pg. 6-1
Instructor Should Explain:
A Load May Be Applied in Different Ways Including:
-Tensile-Shear
-Torsional-Impact
-Fatigue-Compression
The Reaction of a Material to a Load Is Stress. A Load of 30 Tons on a Cross-Section of 1 Sq. Inch Will Induce in the Material a Stress of 30 Tons/Sq. In.
WIT Pg. 6-1
Instructor Should Explain:
Ultimate Tensile Strength - The Maximum Load Carrying Capacity Of A Material. (Calculated)
Yield Strength - The Strength Level At Which Permanent Deformation Begins. (Derived)
WIT Pg. 6-2, Fig. 6.1
Instructor Should Explain:
Elastic - Like Rubber Band
Plastic - Like “Silly Putty”
(Use “Silly Putty” to Demonstrate Plastic Behavior)
Refer Students To Fig. 6.1, Pg. 6-2 - Illustration of Elastic Behavior Of Metals
WIT Pg. 6-3, Fig 6.1
Instructor Should Explain:
Note Each Item and Direction of Change
Also, When The Temperature Of A Metal Is Lowered The Opposite Occurs:
Strength Increases
Hardness Increases
Ductility Decreases
WIT Pg. 6-3
Instructor Should Explain:
Give Examples:
Metals With High Ductility (Ductile)
Low Ductility (Brittle)
Next Slide Shows Brittle Vs. Ductile Failure
Use “Silly Putty” to Show Ductile Material.
WIT Pg. 6-5, Fig. 6.3
Instructor Should Explain:
V Notch Impact Samples - Fracture Faces
Left - Brittle
Right - Ductile
Point Out to Students:
The Brittle Material Exhibits Little or No Deformation Before Fracture (left)
The Ductile Material Shows Deformation (right)
WIT Pg. 6-3
Instructor Should Explain:
Ductility May Be Defined As:
Percent Elongation (% El)
Percent Reduction (% RA)
Will Learn to Calculate in Both U. S. And Metric
WIT Pg. 6-4
Instructor Should Explain:
Rolling Directions:
X Direction - Rolling Direction
Y Direction - Transverse
Z Direction - Through Thickness
WIT Pg. 6-4
Instructor Should Explain:
Strength & Ductility Vs. Rolling Directions:
X Direction - Highest
Y Direction - Up To 25% Less
Z Direction - Up To 50% Less
WIT Pg. 6-4
Instructor Should Explain:
A Common Measurement for Metals
BHN X 500 = Approximate Tensile Strength
WIT Pg. 6-5, Fig. 6.4
Instructor Should Explain:
Differentiate Between Indenters Types
Left - 1/16” Diameter Hard Ball
Right - “Brale” Type - Diamond Tip
Refer Students To Fig. 6.4, Pg. 6-5 - Shows Hardness Tests, Indenters And Shapes Of Indentations
WIT Pg. 6-5, Fig. 6.4
Instructor Should:
Discuss Indenter Type Shown In Slide
WIT Pg. 6-6
Instructor Should Explain:
Note: Absorb Energy and Without Fracture
Refer To Fig. 6.5, Pg. 6-6 - Stress-Strain Vs. Toughness Curves
Given by The Area Under Stress-Strain Curve Or Determined by Impact Testing Such As Charpy V- Notch or CTOD Testing.
WIT Pg. 6-5, 6
Instructor Should Explain:
A Notch Is Typically a Surface Indentation: Which Has the Ability to Concentrate Stress.
Examples:
Scratches
Weld Ripples
Undercut
Many More
WIT Pg. 6-6, Fig. 6.6
Instructor Should Explain:
Give Examples Of:
Stress Risers Causing Premature Failures
Various Conditions Producing Stress Risers
WIT Pg. 6-6, Fig. 6.6
Instructor Should explain:
Need to Know This Term
Determined by Charpy Testing at Different Temperatures and Plotting Data
Welding Can Increase the Ductile to Brittle Transition Temperature - Vital to Observe Welding Procedure Conditions
WIT Pg. 6-7, Fig. 6.7
Instructor Should Explain:
Typically, Fatigue Failures Occur at Lower Stresses Than for Non-Cyclic Stresses
Refer Students To Fig. 6.7, Pg. 6-7
Use Bailing Wire As An Example
WIT Pg. 6-7
Instructor Should Explain:
Know Definition
Refer To Fig. 6.7, Pg. 6-7 :
Discuss - Endurance Limit Steel Vs. Aluminum
WIT Pg. 6-7
Instructor Should Explain:
Plotted Results of Charpy Test, Stress Level Vs #Cycles to Failure:
For 1047, No Failures Will Occur Regardless of #Cycles for Stress Levels of About 43 ksi and Below.
Note: Al - 2014 -T6 - (Poor in Fatigue) Has No Endurance Limit Due to Effects of Work Hardening.
WIT Pg. 6-8
Instructor Should Explain:
For Example:
Iron Has a Tensile Strength Typically in the 30,000 lbs/psi Range.
By Adding 0.1% Of Carbon This Strength Can Be Almost Doubled.
WIT Pg. 6-9, Fig. 6.12
Instructor Should Explain:
Refer Students To Fig. 6.12, Pg. 6-10 - Low Alloy Steels
Example:
Car Parts - Made Of Low Alloy Steels - Energy Absorption By Metal Parts And Not “Body Parts” In Cars Has Saved Many Lives
WIT Pg. 6-9
Instructor Should Explain:
Cr, Ni, W, V added
304 SST
Hastelloy C
WIT Pg. 6-10, Fig. 6.13
Instructor Should Explain:
5 Major Types of SST - Describe Each & Properties
Austentic - 304, 316
Martensitic - 410, 420
Ferritic - 430
PH - 17-4, 15-5
Duplex- 2205
Refer To Fig. 6.13, Pg. 6-9
Point Out Alloy Group # System Developed By AISI (American Iron And Steel Institute)
WIT Pg. 6-10, 11
Instructor Should:
Discuss Effects of Various Alloying Elements on Properties of Steel
WIT Pg. 6-12
Instructor Should:
Review Each Element
WIT Pg. 6-12
Instructor Should Explain:
Air contains - O2, N2
Moisture contains - H2, O2
Gases Typically Found in the Arc Area - H2, O2, N2
Can Be Prevented Using:
Special Fluxes
Shielding Gases
WIT Pg. 6-12, Fig. 6.14
Instructor Should Explain:
Al Alloys Very Complex - Above Series, Heat Treatable:
2024 - T4
6024 - T6
Differentiate Between:
Heat Treatable
Non-Heat Treatable
Refer to Fig. 6.15, Pg. 6-13 - Point Out Temper Designations for (Heat Treatable Alloys)
WIT Pg. 6-12, Fig. 6.14
Instructor Should Explain:
Non-Heat Treatable:
1100 - Pure Aluminum
5356 - Filler Metal
Refer To Fig. 6.15, Pg. 6-13 - Point Out Temper Designations For (Non-Heat Treatable Alloys)
WIT Pg. 6-13
Instructor Should Explain:
Nickel Has the Ability to Form Stable Alloys With Many Other Metals.
These Alloys Exhibit Corrosion Resistance and Toughness at Low Temperature and Good Scaling Resistance at Elevated Temperatures.
WIT Pg. 6-13
Instructor Should Explain:
Alloys Of Copper - Divided Into 8 Groups:
Coppers
High Copper Alloys
Brasses (Cu - Zn)
Bronzes (Cu - Sn)
Copper-Nickels (Cu - Ni)
Copper-Nickel-Zinc Alloys (Nickel Silvers)
Leaded Coppers
Special Alloys
WIT Pg. 6-14
Instructor Should Explain:
Numerous Tests Used To Determine Mechanical And Chemical Properties Of Metals, “Properties” Include:
Chemistry
Hardness
Strength
Welding Inspector Should Know:
When Test Is Applicable
What Results Are Provided
How To Determine Results In Compliance With Specifications
WIT Pg. 6-14
Instructor Should Explain:
Nondestructive Testing:
Used As an Adjunct to Visual Inspection
Give Examples:
ND - Brinnel Test on 4’ X 8’ Plate 1” Thick
D - Brinnel Test on Face of Die Plate for Printing $20 Bills
NDE Testing - Discussed In Detail In Module 10
WIT Pg. 6-17, Fig. 6.17
Instructor Should Explain:
Describe Use:
Ultimate Tensile Strength
Yield Strength
Percent Elongation
Percent Reduction Of Area
Elastic Limit
Toughness
Refer To Fig. 6.18, Pg. 6-17
WIT Pg. 6-15, Fig. 6.16
Instructor Should Explain:
Simple Geometry
Uniform Cross Section
Reduced Section
Smooth Surface Finish
Gage Marks
The Tensile Test Gives the Tensile Strength of the Material Being Tested
Tensile Strength = Load/Area
WIT Pg. 6-15 (Blue Shaded Area)
Instructor Should Explain:
Review Sample Calculations
Explain What Pi Is: Any Circle’s Circumference Is Divided by Its Diameter. A Constant.
WIT Pg. 6-15 (Blue Shaded Area)
Instructor Should Explain:
Alternate # 2
Area = 0.785 X D2
4 = 0.785
WIT Pg. 6-16 (Blue Shaded Area)
Instructor Should Explain:
Review
WIT Pg. 6-19, Fig. 6. 21
Instructor Should Explain:
Used for Deterring Yield Point
Usually Offset at 0.2% (0.002 IN/IN)
Line Parallel to Elastic Limit
Intersection With Curve Is Y. P.
Explain How the Yield Point Is Determined by the Offset Method
WIT Pg. 6-19, Fig. 6. 22
Instructor Should Explain:
Two Steels:
- One Very Strong, but Brittle
- One Weaker, but Ductile
Compare the Values Shown in the Diagram
WIT Pg. 6-20 (Blue Shaded Area)
Instructor Should Explain:
Gage Mark Put on Tensile Sample Prior to Testing
Review Calculations
WIT Pg. 6-20 (Blue Shaded Area)
Instructor Should Explain:
Measure and Calculate X-Section Area Before Testing
Test
Re-Measure and Calculate New, Reduced X-Section Area After Break
Review Calculations
WIT Pg. 6-20
Instructor Should Explain:
Shows Measuring Diameter of Indention
Test Measures Resistance to Indentation
WIT Pg. 6-22, Fig. 6.24 & 6.26
Instructor Should Explain:
Discuss Steps Involved in Process Refer to Pg. 6-25, Fig. 6.26
WIT Pg. 6-24, Fig. 6.25
Instructor Should Explain:
Two Major Types
Vickers
Knoop
Slide Shows Lab Unit
WIT Pg. 6-24
Instructor Should:
Note: Use of Tables or Calculations Necessary
WIT Pg. 6-24
Instructor Should:
Describe Each
WIT Pg. 6-27, Fig. 6.28
Instructor Should Explain:
Review Items
Charpy V-Notch - Most Common
Also, Mention Charpy Keyhole - More Expensive to Make Samples
Refer to Specimen Fig. 6.28, Pg. 6-27
WIT Pg. 6-27, Fig. 6.28
Instructor Should Explain:
Slide Shows Charpy V-Notch Specimens
- Shape of “V” Precise
WIT Pg. 6-27, Fig. 6.28
Instructor Should Explain:
Discuss Procedure and Test Steps
Note: Anvil Strikes Sample on Side Opposite V-Notch and Breaks It.
WIT Pg. 6-28
Instructor Should Explain:
Describe Each
Also,
Where to Look to Determine % Shear
Plot & Check Resulting Curve
WIT Pg. 6-29, Fig. 6.31
Instructor Should Explain:
Ductile and Brittle
Point Out The Amount of Ductility in the Above Samples
Ferrous Charpy Specimens Broken at 20o Temperature Intervals With a 0o Transition Temperature.
WIT Pg. 6-29
Instructor Should Explain:
Describe Each Type of Test and the Results Usually Achieved
WIT Pg. 6-30, Fig. 6.32
Instructor Should:
Note Weld Locations Shown by Etching.
Point Out the Area Where the Maximum Bending Is Applied to Each Specimen:
Face Bends
Root Bends
Side Bends
WIT Pg. 6-31, Fig. 6.35
Instructor Should Explain:
Note Weld
Differentiate Between:
Face Bend
Root Bend
WIT Pg. 6-30, Fig. 6.33 & 6.34
Instructor Should Explain:
Describe Use:
The Size of Sample That Can Be Tested
Placement of Specimen
WIT Pg. 6-30, Fig. 6.34
Instructor Should Explain:
Review Use
WIT Pg. 6-30
Instructor Should:
Discuss Procedure - Cover Each Item On Slide
WIT Pg. 6-31, Fig. 6.36
Instructor Should Explain:
D1.1
API 1104 Method
Prepare Sample
Break Sample
Evaluate Fracture
WIT Pg. 6-31, Fig. 6.37
Instructor Should:
Discuss Results of Nick-Break Test As Shown on Slide
WIT Pg. 6-31
Instructor Should:
Discuss Procedure
Cover Each Item On the Slide