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/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Production of Ni
• Properties of Ni
– FCC: tough,
– High- and low-temp
– High oxidation resistance
– Good resistance for most environments
– High cost
• Ni deposits
– Ni-Cu (Canada)
– Ni silicates (New Caledonia)
– Ni laterites (tropical and subtropical regions)
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Production of Nickel
Iron-ore
recovery
plantBessemer matte
Nickel
concentrate
Copper
concentrate
Iron sulfide
concentrate
(pyrrhotite)
Ni-Cu-Fe sulfide Froth flotation
Nickel and Copper sulfide
Nickel-copper alloy
Copper
products
Froth flotation
Copper
sulfide
Nickel sulfideNickel oxidePure nickel
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Commercially Pure Nickel
Chemical Composition
Typical Application
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Commercially Pure Nickel
• Nickel 200 alloy
– An solid solution
– Good properties
– Excellent resistance to many corrosive environment
– High strength at elevated temperatures
– Tough and ductile at low temperature
• Nickel 201 alloy
– Low-carbon contents (limited to %)
– Low work-hardening rate, increased
– Adaptable for spinning and cold-working operations
• Nickel 270 alloy
– High- (99.98 % Ni)
– Excellent thermal conductivity, high ductility
– Heavy cold deformation without annealing
Fig 11Microstructures
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Copper Alloys (Monels)
– Cu-Ni: completely
– : about 67% Ni and 33% Cu
Chem Comp and Typical Applications
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Copper Alloys (Monels)
• Monel 400
– High , weldability, excellent
resistance, toughness over
a wide range of temp
– under high-velocity
conditions
• Monel R-405
– addition to improve the
machining characteristics.
• Monel K-500
– Addition of 3.0% Al and 0.6% Ti to
form age-hardening precipitates of
Microstructure
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Chromium Alloys
Cr: An important alloying element for many corrosion-
resistant and high-temp- Ni base alloys
Phase Diagram
Chem Comp and Typical Applications
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Chromium Alloys
• Microstructure and Properties
– 600
• Standard engineering alloy for use in some
severely corrosive environments at elevated
temp
• 15.5% Cr and 8% : high strength and
workability
• Strengthened by (not heat-
treatable)
Fig 11
Fig 11
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Chromium Alloys
– Inconel 601
• 23% Cr, 14% Fe, 1.4% Al: heat and corrosion
resistance
• A protective film formation on the metal
surface during high-temp exposure
– Inconel 625
• 22% Cr, 5% Fe, 9% Mo, 3.6% Nb
• High strength (solid-solution strengthening effect of
Mo and Nb)
• High corrosion resistance to (Cr and Mo)
• Weldability (niobium carbide)
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Base Superalloys
• Superalloys
– High strength at high
– Good and resistance
– Superior resistance to and at elevated temp
– Nickel base, nickel-iron base, and cobalt base
Chem Comp and Typical Applications
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Base Superalloys
• Major phases present in nickel-base superalloys
– γ (gamma) phase: continuous matrix of
– γ’ (gamma prime) phase: major phase
– Carbides: mainly and
Microstructure
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Base Superalloys
• Problems
– Cellular M23C6 carbides: shortened rupture (elimination via heat treatment)
– σ (sigma) phase: low-temp , shortened rupture life
(overcome by changing the alloy chemistry)
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Base Superalloys
• γ phase
– Strengthened by of solid-solution elements (atomic factor)
– Electron hole number of elements Nv ↑ ↓ slip to occur difficult
– Slow-diffusing element (Mo, W) high-temp creep ↓
• γ’ phase
– FCC A3B-type precipitate (A = Ni, Co, Fe while B = Al, Ti, Nb)
– Homogeneous nucleation with low energy (0.1% mismatch)
– Extraordinary long-term
– Antiphase boundary (APB) in γ- γ’
alloys by dislocation interaction
– Temperature ↑ degree of in Ni3(Al,Ti)
increase in
– Morphology: sphere (small , 0.05%),
cube, semicoherent plates (above 1.25%)
Microstructure
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Base Superalloys
• Role of carbides in nickel-base heat-resistant alloys
– Carbon contents: wrought alloys (0.02 ~ 0.2%), cast alloys (0.6%)
– No carbides along the grain boundaries (GB) GB
– Continuous chains of carbides along the GB fracture
• Types of carbides
– carbides: M = Ti, Ta, Nb, W
• very stable
• restricting grain growth
• temp range where solidification begins
– carbides: M = Cr, Fe, W, Mo, Co
• complex cubic structure
• to precipitate along GB
• 760 ~ 980C
– M6C carbides: M = Mo, W
• complex cubic structure
• 815 ~ 980C
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Base Superalloys
• Topologically closed-packed (TCP) phases: σ, μ, Laves, χ– Thin parallel to the {111}γ rupture strengths, loss in rupture
– Changing chemical balance by removing refractory elements such as Cr, Mo, W
reduced solid-solution strengthening, γ/γ’ mismatch
Fig 11
/MS371/ Structure and Properties of Engineering Alloys/MS371/ Structure and Properties of Engineering Alloys
Nickel-Base Superalloys
• Microstructure of Inconel
– Precipitation- Ni-base superalloy
– Corrosion and oxidation
– High-temp strength (up to about 760~ °C)
– 4 types of heat treatment
• Solutionizing + air cooling → γ’ + (carbides)
• Solutionizing + air cooling + double-aging treatment
→ dense γ’ particles, stabilized GB carbides
• Solutionizing + air cooling + single-aging treatment
→ discontinuous carbides precipitates at GB
• Solutionizing + air cooling + overaging
→ coarse γ’ particles (undesirable)