= 62 wt% Ni-38 wt% Cu.



Similar documents
9.11 Upon heating a lead-tin alloy of composition 30 wt% Sn-70 wt% Pb from 150 C and utilizing Figure

Alloys & Their Phase Diagrams

Introduction to Materials Science, Chapter 9, Phase Diagrams. Phase Diagrams. University of Tennessee, Dept. of Materials Science and Engineering 1

CHAPTER 9 Part 1. = 5 wt% Sn-95 wt% Pb C β. = 98 wt% Sn-2 wt% Pb. = 77 wt% Ag-23 wt% Cu. = 51 wt% Zn-49 wt% Cu C γ. = 58 wt% Zn-42 wt% Cu

Iron-Carbon Phase Diagram (a review) see Callister Chapter 9

BINARY SYSTEMS. Definition of Composition: Atomic (molar) fraction. Atomic percent. Mass fraction. Mass percent (weight percent)

Lecture 19: Eutectoid Transformation in Steels: a typical case of Cellular

Binary phase diagrams

Chapter 8. Phase Diagrams

Heat Treatment of Steel

Chapter Outline: Phase Transformations in Metals

Phase Equilibria & Phase Diagrams

Phase. Gibbs Phase rule

m sugar + m water (wt%) = 77 wt% = m sugar g 100 m' sugar m' sugar g 100

Heat Treatment of Steels : Spheroidize annealing. Heat Treatment of Steels : Normalizing

In order to solve this problem it is first necessary to use Equation 5.5: x 2 Dt. = 1 erf. = 1.30, and x = 2 mm = m. Thus,

The atomic packing factor is defined as the ratio of sphere volume to the total unit cell volume, or APF = V S V C. = 2(sphere volume) = 2 = V C = 4R

Module 34. Heat Treatment of steel IV. Lecture 34. Heat Treatment of steel IV

Phase Transformations in Metals and Alloys

The mechanical properties of metal affected by heat treatment are:

LABORATORY EXPERIMENTS TESTING OF MATERIALS

Fundamentals of the Heat Treating of Steel

Chapter Outline. Diffusion - how do atoms move through solids?

CHAPTER 8. Phase Diagrams 8-1

THREE MAIN SOLIDIFICATION REACTIONS OF VANADIUM MODIFIED T1 TUNGSTEN HIGH SPEED TOOL STEEL. Hossam Halfa

Massachusetts Institute of Technology Department of Mechanical Engineering Cambridge, MA 02139

REACTIONS IN THE SN CORNER OF THE CU-SN-ZN ALLOY SYSTEM

WJM Technologies excellence in material joining

8. Technical Heat Treatment

Experiment: Heat Treatment - Quenching & Tempering

Materials Issues in Fatigue and Fracture

Crystal Structure of Aluminum, Zinc, and their Alloys By: Omar Fajardo Sebastian Henao Devin Baines ENGR45, F2014, SRJC

DIFFUSION IN SOLIDS. Materials often heat treated to improve properties. Atomic diffusion occurs during heat treatment

Improved Broaching Steel Technology

Der Einfluss thermophysikalischer Daten auf die numerische Simulation von Gießprozessen

CONCEPT CHECK QUESTIONS AND ANSWERS. Chapter 2 Atomic Structure and Interatomic Bonding

MSE PRECIPITATION HARDENING IN 7075 ALUMINUM ALLOY

Martensite in Steels

14:635:407:02 Homework III Solutions

Defects Introduction. Bonding + Structure + Defects. Properties

Objectives/Introduction Extraction of zinc Physical properties of zinc Zinc casting alloys Wrought zinc alloys Engineering design with zinc alloys

Continuous Cooling Transformation (CCT) Diagrams

Thermodynamic database of the phase diagrams in copper base alloy systems

Simulations of the Effect of Section Size and Cooling on Sigma Phase Formation in Duplex Stainless Steels

CHROMIUM STEEL POWDERS FOR COMPONENTS. JEANETTE LEWENHAGEN Höganäs AB, Sweden

μ α =μ β = μ γ = =μ ω μ α =μ β =μ γ = =μ ω Thus for c components, the number of additional constraints is c(p 1) ( ) ( )

The Effect of Heat Treatment Atmosphere on Hardening of Surface Region of H13 Tool Steel. Dominique AU

EFFECT OF COPPER ALLOY ADDITION METHOD ON THE DIMENSIONAL RESPONSE OF SINTERED FE-CU-C STEELS

HIGH STRENGTH DUCTILE IRON PRODUCED BY THE ENGINEERED COOLING: PROCESS CONCEPT

Chapter 5: Diffusion. 5.1 Steady-State Diffusion

Influence of Steel Scrap on Microstructure and Mechanical Properties of Spheroidal Graphite Cast Iron

HEAT TREATMENT OF STEEL

INFLUENCE OF THERMOMECHANICAL TREATMENT ON THE STEEL C45 FATIGUE PROPERTIES

Weld Cracking. An Excerpt from The Fabricators' and Erectors' Guide to Welded Steel Construction. The James F. Lincoln Arc Welding Foundation

LN Introduction to Solid State Chemistry. Lecture Notes No. 10 PHASE EQUILIBRIA AND PHASE DIAGRAMS

RAPIDLY SOLIDIFIED COPPER ALLOYS RIBBONS

Time Temperature Transformation (TTT) Diagrams

Chem 420/523 Chemical Thermodynamics Homework Assignment # 6

A Comparison of FC-0208 to a 0.3% Molybdenum Prealloyed Low-Alloy Powder with 0.8% Graphite

Lecture: 33. Solidification of Weld Metal

Effect of Small Additions of Boron on the Mechanical Properties and Hardenability of Sintered P/M Steels

Week 2: Steel. Steel Topics. Introduction to Iron and Steel. Introduction to Iron and Steel. A Selection of Mechanical Properties (from Gordon (1979))

The study about as cast microstructure and solidification

FATIGUE BEHAVIOUR ANALYSIS OF DIFFERENTLY HEAT TREATED MEDIUM CARBON STEEL. Master of Technology (Res.) Metallurgical and Materials Engineering

Chapter Outline Dislocations and Strengthening Mechanisms

Lecture 3: Models of Solutions

EUTECTIC TRANSFORMATION IN DUCTILE CAST IRON. PART I THEORETICAL BACKGROUND

Chapter Outline Dislocations and Strengthening Mechanisms

MATERIAL SPECIFICATIONS CATALOGUE

SOLIDIFICATION. (a)formation of stable nuclei. Growth of a stable nucleus. (c) Grain structure

Mechanical Properties of Metals Mechanical Properties refers to the behavior of material when external forces are applied

INFLUENCE OF Cr, Mn AND Mo ON STRUCTURE AND PROPERTIES OF V MICROALLOYED MEDIUM CARBON FORGING STEELS

Problems in Welding of High Strength Aluminium Alloys

Kinetics of Phase Transformations: Nucleation & Growth

Lecture 4: Thermodynamics of Diffusion: Spinodals

Introduction To Materials Science FOR ENGINEERS, Ch. 5. Diffusion. MSE 201 Callister Chapter 5

Welding. ArcelorMittal Europe Flat Products. Definitions of welding and weldability. Consequences of welding

Influence of Solder Reaction Across Solder Joints

Interface Reaction and Mechanical Properties of Lead-free Sn Zn Alloy/Cu Joints

X15TN TM. A high hardness, corrosion and fatigue resistance martensitic grade CONTINUOUS INNOVATION RESEARCH SERVICE.

Strengthening. Mechanisms of strengthening in single-phase metals: grain-size reduction solid-solution alloying strain hardening

Chemical reactions allow living things to grow, develop, reproduce, and adapt.

Thermo-Calc Software. Data Organization and Knowledge Discovery. Paul Mason Thermo-Calc Software, Inc. Thermo-Chemistry to Phase Diagrams and More

Ch. 4: Imperfections in Solids Part 1. Dr. Feras Fraige

North American Stainless

Base Materials (Fe Base Alloys And Superalloys)

2 MATTER. 2.1 Physical and Chemical Properties and Changes

Name Electrochemical Cells Practice Exam Date:

Martensite transformation, microsegregation, and creep strength of. 9 Cr-1 Mo-V steel weld metal

Soldering Definition and Differences

Name Date Class CHAPTER 1 REVIEW. Answer the following questions in the space provided.

How to manage wave solder alloy contaminations. Gerjan Diepstraten & Harry Trip Cobar Europe BV Balver Zinn

Effect of cooling rate on hardness and microstructure of AISI 1020, AISI 1040 and AISI 1060 Steels

Type: Single Date: Homework: READ 12.8, Do CONCEPT Q. # (14) Do PROBLEMS (40, 52, 81) Ch. 12

CHEM 105 HOUR EXAM III 28-OCT-99. = -163 kj/mole determine H f 0 for Ni(CO) 4 (g) = -260 kj/mole determine H f 0 for Cr(CO) 6 (g)

Transcription:

9-2 9.2 (a) From Figure 9.8, the maximum solubility of Pb in Sn at 100 C corresponds to the position of the β (α + β) phase boundary at this temperature, or to about 2 wt% Pb. (b) From this same figure, the maximum solubility of Sn in Pb corresponds to the position of the α (α + β) phase boundary at this temperature, or about 5 wt% Sn.

9-14 9.12 Upon cooling a 50 wt% Ni-50 wt% Cu alloy from 1400 C and utilizing Figure 9.3a: (a) The first solid phase forms at the temperature at which a vertical line at this composition intersects the L (α + L) phase boundary--i.e., at about 1320 C. (b) The composition of this solid phase corresponds to the intersection with the L (α + L) phase boundary, of a tie line constructed across the α + L phase region at 1320 C--i.e., C α 62 wt% Ni-38 wt% Cu. (c) Complete solidification of the alloy occurs at the intersection of this same vertical line at 50 wt% Ni with the (α + L) α phase boundary--i.e., at about 1270 C. (d) The composition of the last liquid phase remaining prior to complete solidification corresponds to the intersection with the L (α + L) boundary, of the tie line constructed across the α + L phase region at 1270 C--i.e., C L is about 37 wt% Ni-63 wt% Cu.

9-15 9.13 This problem asks us to determine the phases present and their concentrations at several temperatures, as an alloy of composition 52 wt% Zn-48 wt% Cu is cooled. From Figure 9.19: At 1000 C, a liquid phase is present; W L 1.0 At 800 C, the β phase is present, and W β 1.0 At 500 C, β and γ phases are present, and W γ C 0 C β 52 49 C γ C β 58 49 0.33 W β 1.00 0.33 0.67 At 300 C, the β' and γ phases are present, and W β' C γ C 0 59 52 C γ C β' 59 50 0.78 W γ 1.00 0.78 0.22

9-32 Development of Microstructure in Isomorphous Alloys 9.25 (a) Coring is the phenomenon whereby concentration gradients exist across grains in polycrystalline alloys, with higher concentrations of the component having the lower melting temperature at the grain boundaries. It occurs, during solidification, as a consequence of cooling rates that are too rapid to allow for the maintenance of the equilibrium composition of the solid phase. (b) One undesirable consequence of a cored structure is that, upon heating, the grain boundary regions will melt first and at a temperature below the equilibrium phase boundary from the phase diagram; this melting results in a loss in mechanical integrity of the alloy.

9-35 Development of Microstructure in Eutectic Alloys 9.28 Upon solidification, an alloy of eutectic composition forms a microstructure consisting of alternating layers of the two solid phases because during the solidification atomic diffusion must occur, and with this layered configuration the diffusion path length for the atoms is a minimum.

9-36 9.29 A phase is a homogeneous portion of the system having uniform physical and chemical characteristics, whereas a microconstituent is an identifiable element of the microstructure (that may consist of more than one phase).

9-56 The Iron-Iron Carbide (Fe-Fe 3 C) Phase Diagram Development of Microstructure in Iron-Carbon Alloys 9.46 This problem asks that we compute the mass fractions of α ferrite and cementite in pearlite. The lever-rule expression for ferrite is W α C Fe3 C C 0 and, since C Fe3 C 6.70 wt% C, C 0 0.76 wt% C, and C α 0.022 wt% C W α 6.70 0.76 6.70 0.022 0.89 Similarly, for cementite W Fe3 C C 0 C α 0.76 0.022 6.70 0.022 0.11

9-57 9.47 (a) A hypoeutectoid steel has a carbon concentration less than the eutectoid; on the other hand, a hypereutectoid steel has a carbon content greater than the eutectoid. (b) For a hypoeutectoid steel, the proeutectoid ferrite is a microconstituent that formed above the eutectoid temperature. The eutectoid ferrite is one of the constituents of pearlite that formed at a temperature below the eutectoid. The carbon concentration for both ferrites is 0.022 wt% C.

9-59 9.49 In this problem we are given values of W α and W Fe3 C (0.86 and 0.14, respectively) for an ironcarbon alloy and then are asked to specify the proeutectoid phase. Employment of the lever rule for total α leads to W α 0.86 C Fe3 C C 0 6.70 C 0 6.70 0.022 Now, solving for C 0, the alloy composition, leads to C 0 0.96 wt% C. Therefore, the proeutectoid phase is Fe 3 C since C 0 is greater than 0.76 wt% C.

9-62 9.51 We are called upon to consider various aspects of 6.0 kg of austenite containing 0.45 wt% C, that is cooled to below the eutectoid. (a) Ferrite is the proeutectoid phase since 0.45 wt% C is less than 0.76 wt% C. (b) For this portion of the problem, we are asked to determine how much total ferrite and cementite form. For ferrite, application of the appropriate lever rule expression yields W α C Fe3 C C 0 6.70 0.45 6.70 0.022 0.94 which corresponds to (0.94)(6.0 kg) 5.64 kg of total ferrite. Similarly, for total cementite, W Fe3 C C 0 C α 0.45 0.022 6.70 0.022 0.06 Or (0.06)(6.0 kg) 0.36 kg of total cementite form. (c) Now consider the amounts of pearlite and proeutectoid ferrite. Using Equation 9.20 W p C 0 ' 0.022 0.45 0.022 0.58 This corresponds to (0.58)(6.0 kg) 3.48 kg of pearlite. Also, from Equation 9.21, W α' 0.76 0.45 0.42 Or, there are (0.42)(6.0 kg) 2.52 kg of proeutectoid ferrite. (d) Schematically, the microstructure would appear as:

9-63

9-64 9.52 The mass fractions of proeutectoid ferrite and pearlite that form in a 0.35 wt% C iron-carbon alloy are considered in this problem. From Equation 9.20 W p C 0 ' 0.022 0.35 0.022 0.44 And, from Equation 9.21 (for proeutectoid ferrite) W α' 0.76 C 0 ' 0.76 0.35 0.56

9-68 9.56 In this problem we are asked to consider 1.5 kg of a 99.7 wt% Fe-0.3 wt% C alloy that is cooled to a temperature below the eutectoid. (a) Equation 9.21 must be used in computing the amount of proeutectoid ferrite that forms. Thus, W α' 0.76 C 0 ' 0.76 0.30 0.622 Or, (0.622)(1.5 kg) 0.933 kg of proeutectoid ferrite forms. (b) In order to determine the amount of eutectoid ferrite, it first becomes necessary to compute the amount of total ferrite using the lever rule applied entirely across the α + Fe 3 C phase field, as W α C Fe3 C C 0 ' 6.70 0.30 6.70 0.022 0.958 which corresponds to (0.958)(1.5 kg) 1.437 kg. Now, the amount of eutectoid ferrite is just the difference between total and proeutectoid ferrites, or 1.437 kg 0.933 kg 0.504 kg (c) With regard to the amount of cementite that forms, again application of the lever rule across the entirety of the α + Fe 3 C phase field, leads to W Fe3 C C 0 ' C α 0.30 0.022 6.70 0.022 0.042 which amounts to (0.042)(1.5 kg) 0.063 kg cementite in the alloy.