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MATERIAL LOGAM
ISMOJO, ST.,MT
Penilaian
• Ujian Tengah Semester (UTS) = 30%
• Ujian Akhir Semester (UAS) = 40%
• Tugas-tugas = 20%
• Kuis = 10%
• Yang berhak mengikuti ujian akhir semester: kehadiran ≥ 70%
Referensi
• W.F. Smith, “Principles of Materials Science and Engineering”, McGraw-Hill, Singapore, 1990.
• S.H. Avner, ”Introduction to Physical Metallurgy”, McGraw-Hill, Tokyo, 1974.
• D.S. Clark, W.R. Varney, ”Physical Metallurgy for Engineers”, Van-Nostrand Reinhold Co., New York, 1952.
• B.J. Moniz, ”Metallurgy”, 2nd edition, ATP, Homewood, Illinois, 1994.
• Reed-Hill, Robert E., Reza Abbaschian, and Lara Abbaschian. Physical Metallurgy Principles. 4th ed. Stamfor
Materials Sciences adalah suatu aspek yang mempelajari karakteristik material secara keilmuan dan teknologi yang dapat digunakan untuk membuat material atau bahan teknik.
Materials SciencesMaterials Sciences
Metallurgical Metallurgical EngineeringEngineering
Composite Composite EngineeringEngineering
Polymer Polymer EngineeringEngineering
Materials Materials EngineeringEngineering
Ceramic Ceramic EngineeringEngineering
1. Metallurgical Engineering• Mempelajari karakteristik logam dan paduannya, merupakan ilmu tertua
yang mempelajari material teknik.• Perkembangan metalurgi selama 150 tahun terakhir membaginya menjadi
3 bagian utama, yaitu :a. Metalurgi Ekstraksi (mempelajari bagaimana mengekstraksi
dan memurnikan suatu logam dari bijihnya).b. Metalurgi Fisik (mempelajari pengaruh struktur mikro terhadap
sifat-sifat logam, memodifikasi struktur mikro).c. Metalurgi Mekanik (mempelajari teknik pembuatan dan gaya-
gaya yang bekerja untuk membentuk suatu logam menjadi produk tertentu).
2. Ceramic Engineering• Mempelajari perkembangan dan produksi suatu produk yang terbuat dari
bahan non-metalik, inorganik dengan pembakaran pada temperatur tinggi.
3. Polymer Engineering
• Mempelajari perkembangan produk yang terbuat dari bahan sintetis organik.
• Polimer terdiri atas Thermosetting dan Thermoplastic.
4. Composite Engineering
• Mempelajari penerapan gabungan material untuk memperoleh sifat-sifat yang tidak dimiliki oleh masing-masing bahan.
• Kombinasi yang dilakukan bisa logam, keramik, polimer (metal matrix composite/MMC; polymer matrix composite/PMC; ceramic matrix composite/CMC, dll).
5. Materials Engineering
• Mengevaluasi karakteristik sifat-sifat yang dimiliki oleh material. Ini berhubungan dengan penggantian material yang dapat memperbaiki kemampuan dan menurunkan harga komponen.
Spektrum pengetahuan material, Spektrum pengetahuan material, penggabungan pengetahuan penggabungan pengetahuan material dari ilmu material dan material dari ilmu material dan material teknik menjadikan material teknik menjadikan rekasayawan dapat mengubah rekasayawan dapat mengubah material menjadi produk yang material menjadi produk yang berguna bagi masyarakat.berguna bagi masyarakat.
Diagram yang menggambarkan Diagram yang menggambarkan bagaimana ilmu dan teknik material bagaimana ilmu dan teknik material terbentuk dari rangkaian pengetahuan terbentuk dari rangkaian pengetahuan dari ilmu-ilmu dasar dan berbagai dari ilmu-ilmu dasar dan berbagai disiplin ilmu pengetahuan.disiplin ilmu pengetahuan.
Flow chart pembuatan suatu komponen
Gambar diatas mengkaitkan berbagai hal yang harus diperhatikan oleh seorang perancang dalam membuat suatu komponen atau konstruksi.
9
Contoh-contoh produk :Early food containers of glass & steel use common ceramic and metal materials of the late 19th & early 20th centuries
The new containers are lightweight, will not break, and offer long shelf life for their contents
Advances in materials technology brought on new containers made of two-piece Al and steel cans and “barrier” packages made of laminated composites of plastics, aluminum, and paper.
Decorated Foil Pouches for Food and Drink • 1XXX represents the commercially
pure aluminum.
High formability, corrosion resistance and electrical conductivity
Electrical, chemical applications
• The 1XXX series would not be used where strength is a prime consideration.
• For the applications where extremely high corrosion resistance, formability and/or electrical conductivity are required (foil and strip for packaging)
1060 or 11101060 or 1110
JembatanJembatan
PipelinePipeline
DumptruckDumptruck
Pesawat Pesawat terbangterbang
Jaringan Jaringan listriklistrik
Peralatan Peralatan dapurdapur
RodagigiRodagigiKereta Kereta listriklistrik
Baut dan Baut dan murmur
ElektroElektroniknik
Pembuatan Pesawat Pembuatan Pesawat terbangterbang
Komponen Komponen mesinmesin
Komponen Komponen mesin hasil mesin hasil
corancoran
Pembuatan mobilPembuatan mobil
Komponen Komponen mesinmesin
Sudu turbin Sudu turbin
16
Patung tembaga Patung tembaga paduanpaduan
Pakaian Pakaian perangperang
Mobil masa depanMobil masa depan
Ford contour dengan bahan Ford contour dengan bahan dari aluminium ekstrusidari aluminium ekstrusi
Bronze Bronze MaskMask
Komponen produk Komponen produk pengecoranpengecoran
Chemical Physical Mechanical Manufacturing considerations
Composition
Microstructure
Phases
Grain size
Corrosion resistance
Inclusions
Melting point
Glass transition (polymers/glasses)
Magnetic
Electrical
Optical
Acoustic
Gravimetric
Color
Tensile/compressive properties
Toughness
Ductility
Fatigue
Hardness
Creep resistance
Shear strength
Available shapes
Available sizes
Available surface texture
Manufacturing tolerances
Composition
Fillers/additives
Crystallinity
Molecular weight
Flammability
Spatial configuration
Chemical resistance
Tensile/compressive properties
Heat distortion
Pressure-velocity limit
Toughness
Stress rupture resistance
Creep resistance
Manufacturing tolerances
Stability
Available sizes
Composition
Porosity
Grain size
Crystal structure
Corrosion resistance
Phases
Tensile/compressive properties
Fracture toughness
Transverse rupture
Hardness
Available shapes
Available sizes
Available surface texture
Manufacturing tolerances
Composition matrix:filler
Matrix/filler bond
Volume fraction of fillers
Reinforcement type
Chemical resistance
Tensile/compressive properties
Fracture toughness
Creep resistance
Reinforcement orientation
Available shapes
Available sizes
Manufacturing tolerances
Stability
Material Properties
Metals
Plastics
Ceramics
Composites
19
Diktator material = SOLVENT
Material terlarut = SOLUTE
Pada logam berlaku larutan padat (solid solution).
Dengan demikian solvent dan solute keduanya adalah padatan.
Pelarutan terjadi pada temperatur tinggi, dimana kedua padatan berubah menjadi cair. Untuk baja, pada temperatur tinggi, besi (Fe) dapat melarutkan banyak unsur-unsur khususnya karbon. Fe menjadi diktator. Sejumlah kecil C, S atau Mn menjadi unsur yang terlarut.
kusharjanto, metalurgi-unjani 20
Struktur partikel atom mirip dengan sistim tata surya
Secara umum struktur atom terdiri dari inti atau nucleus (proton dan neutron) yang dikelilingi oleh elektron.
Proton = partikel bermuatan positif
Neutron = netral
Elektron = bermuatan negatif
Jumlah proton = jumlah elektron
Setiap kulit pada orbit elektron mengandung sejumlah elektron, misalnya pada kulit pertama (terdekat dengan inti) = 2 elektron, kedua = 8 elektron, ketiga = 18 elektron, keempat = 32 elektron
Jika kulit terluar telah terpenuhi jumlah elektronnya, maka unsur akan menjadi stabil dan tidak akan bereaksi dengan unsur lain membentuk senyawa atau molekul. Contoh: gas inert argon dan helium digunakan sebagai gas pelindung dalam proses pengelasan, karena tidak bereaksi dengan logam untuk membentuk senyawa intermetalik yang tidak diinginkan.
Jika kulit terluar belum terpenuhi jumlah elektronnya, maka akan berikatan dengan unsur lain untuk membentuk senyawa atau molekul.
1.Ikatan kuat (primary bonding): melibatkan pembagian elektron (ikatan ion, kovalen dan logam).
2.Ikatan sekunder (secondary bonding): melibatkan tarik menarik atom-atom yang relatif lemah dan tidak ada pembagian atau pertukaran elektron (ikatan van der waals).
Salah satu dasar untuk mengklasifikasi material adalah ikatan kimia.
Dua jenis ikatan kimia:
kusharjanto, metalurgi-unjani 23
SystemEnergy
Distance between atoms
Repulsive energy
Separated atomsBond
EnergyStable
unstable
Ikatan (Ikatan (BondingBonding))Jika atom-atom mempunyai jarak yang cukup jauh, maka akan terjadi interaksi yang lemah.
Menurunnya jarak antar atom, energi-pun akan turun dan sistem menjadi lebih stabil.
Atom-atom akan mencapai jarak optimal pada level energi terendah.
Ikatan terjadi jika jarak antar atom cukup untuk menghasilkan tarik menarik.
Jika jarak atom terlalu dekat terjadi tolak menolak.
• Terjadi ketika valensi elektron meninggalkan masing-masing
atom dan digunakan bersama di antara semua atom dalam
bentuk awan elektron bebas.• Terdapat pada unsur-unsur logam yang hanya mempunyai 1,
2 atau 3 elektron dikulit terluarnya.• Melimpahnya proton, atom-atom bermuatan ion-ion positif.• Elektron-elektron yang mengambang membentuk awan-awan
elektron, sehingga elektron mudah bergerak.• Adanya elektron-elektron bebas menyebabkan konduktivitas
panas dan listriknya tinggi.
Ikatan logam (metallic Bonding)
What is a metal?
Metals
• Metals: combination of metallic elements (free electrons) good conductors of electricity and heat not transparent to visible light strong and ductile
• A metal is defined as an opaque, lustrous elemental chemical substance that is a good conductor of heat and electricity, and when polished, a good reflector of light. (ASM Definition)
The Periodic Table
Transition Metals
Metals
Metal Alloys
• Ferrous Alloys
– Classification of Steels
– Designation of Steels
• Nonferrous Alloys
– Aluminum
– Copper
– Magnesium
– Titanium
– Refractory metals
– Superalloys
– Noble metals
Metal Alloys
Classification of Ferrous Alloys Metal Alloys
Ferrous Nonferrous
Steels Cast Irons
Low Alloy
Low-carbon Medium-carbon High-carbon
High Alloy
PlainHigh
strength, low alloy
Heat treatable
Plain ToolPlain Stainless
Gray iron
Ductile iron
White iron
Malleable iron
• Based on carbon content
– Pure iron (< 0.008wt% C)
From the phase diagram, it is composed almost exclusively of the ferrite phase at room temperature.
– Steels (0.008 ~ 2.14wt% C)
In most steels the microstructure consists of both and Fe3C phases.
Carbon concentrations in commercial steels rarely exceed 1.0 wt%.
– Cast irons (2.14 ~ 6.70 wt% C)
Commercial cast irons normally contain less than 4.5wt% C
Classification of Ferrous Alloys
The iron–iron carbide phase diagram.
L + Fe3C
2.14 4.30
6.70
M
N
C
PE
O
G
F
H
Cementite Fe3C
x
x’
0.022
0.76
• The carbon content is normally less than 1.0 wt%.
• Plain carbon steels: containing only residual concentrations of impurities other than carbon and a little manganese
About 90% of all steel made is carbon steel.
• Alloy steels: more alloying elements are intentionally added in specific concentrations.
• Stainless steels
Ferrous Alloys — Steels
Standar material (materials standards)
Standar material dikembangkan oleh pemerintah, industri, baik secara nasional maupun internasional.
Standar adalah dokumen kesepakatan yang merupakan piranti/perangkat tolok ukur sifat-sifat, karakteristik atau suatu prosedur yang telah berjalan.
Standar biasanya dikembangkan oleh suatu komite yang terdiri dari para profesional dibidangnya.
Langkah pertama dalam pengembangan suatu standar adalah membuat suatu draft yang dibahas oleh sebuah komite yang nantinya akan disahkan menjadi suatu standar yang berlaku secara nasional maupun internasional.
Pengembangan proses membutuhkan waktu yang lama, tetapi dokumen akhir yang telah selesai dibahas merepresentasikan suatu konsensus dari opini komite dan memperhatikan kenyataan diindustri saat itu.
Suatu standar harus ditinjau secara berkala (minimum sekali dalam lima tahun) untuk menentukan apakah dipertahankan atau diperbaiki.
Jika suatu standar ditetapkan sudah tidak relevan lagi, maka standar tersebut harus dihapus.
Ada tiga kelas standar:
1. Spesifikasi (specification)
2. Metoda pengujian (test method)
3. Rekomendasi penggunaan (recommended practice)
Sebuah kode berisi ketiga kelas standar dan mengikat secara hukum.
1. Spesifikasi
Merupakan pernyataan bahwa suatu produk harus sesuai antara keperluan teknis dan komersial. Contohnya baja paduan dan baja tahan karat untuk baut yang bekerja pada operasi temperatur tinggi mengikuti ASTM A 193.
2. Metoda pengujian
Sekumpulan/seperangkat perintah atau cara-cara untuk mengidentifikasi, melakukan pengukuran atau mengevaluasi sifat-sifat material. Contohnya pengujian impak untuk material logam menggunakan ASTM E 23.
3. Rekomendasi penggunaan/aplikasi
Sekumpulan/seperangkat perintah atau cara-cara dalam melaksanakan satu atau lebih pengoperasian atau fungsi selain dari identifikasi, pengukuran atau mengevaluasi material. Contohnya rekomendasi penggunaan untuk persiapan permukaan baja atau material keras yang lainnya dengan menggunakan penyemprotan air sebelum dilapis atau lapis ulang mengikuti NACE RP-01-72.
4. Kode
Sekumpulan standar atau seperangkat peraturan yang harus ditaati. Contohnya ASME Boiler and Pressure Vessel Code, dimana didalamnya terdapat peraturan untuk proses perlakuan panas setelah pengelasan dari bejana tekan yang berkaitan dengan jenis dan ketebalan material.
ASTM A 193
SPECIFICATIONFOR ALLOY STEEL AND STAINLESS STEEL BOLTING MATERIAL FOR
HIGH-TEMPERATURE SERVICE
ASTM E 23
TEST METHODNOCTHED BAR IMPACT TESTING OF METALLIC MATERILAS
NACE RP-01-72
RECOMMENDED PRACTICESURFACE PREPARATION OF STEEL AND OTHER HARD MATERIALS
ASMEBoiler and Pressure Vessel Code
CODESECTION VIII, DIVISION 1, PARAGRAPH UCS-56
POST-WELD HEAT TREATMENT OF CARBON STEEL PRESSURE VESSELS
Contoh-contoh standar:
1. AISI (American Iron and Steel Institute)
2. SAE (Society of Automotive Engineers)
3. ASTM (American Society for Testing and Materials)
4. UNS (Unified Numbering System)
5. NACE (National Association of Corrosion Engineers)
6. AWS (American Welding Society)
7. AA (Aluminum Association)
8. API (American Petroleum Institute)
9. ASME (American Society of Mechanical Engineers)
Kesemuanya berada dibawah naungan ANSI (American National Standards Institute)
Organisasi-organisasi Profesional
Standar setiap negara:
Negara SingkatanAustria ONORMBelgia NBNBulgaria BDSCanada CSACzechoslovakia CSNPerancis AFNORJerman DINJepang JISInggris BSIndonesia SNIPolandia PNItalia UNIRumania STASSpanyol UNESwedia SSRusia GOSTEropa bersatu EURONORMHungaria MSZ
• A four-digit number: the first two digits indicate the alloy content; the last two, the carbon concentration
• For plain carbon steels, the first two digits are 1 and 0; alloy steels are designated by other initial two-digit combinations (e.g., 13, 41, 43)
• The third and fourth digits represent the weight percent carbon multiplied by 100
For example, a 1040 steel is a plain carbon steel containing 0.40 wt% C.
The Designation of Steels
• A four-digit number: the first two digits indicate the alloy content; the last two, the carbon concentration
The Designation of Steels
4141 40 40
Identifies major alloying element(s)
Percentage of carbon
Steel AlloysSteel Numerical Name Key Alloys
10XX, 11 XX Carbon only 13XX Manganese
23XX, 25 XX Nickel 31XX, 33XX, 303XX Nickel-Chromium
40XX Mo 41XX Cr-Mo
43XX & 47XX Ni-Cr-Mo 44XX Mn-Mo 48XX Ni-Mo
50XX, 51XX, 501XX, 521XX, 514XX, 515XX
Cr 61XX Cr-V
81XX, 86XX, 87XX, 88XX Ni-Cr-Mo 92XX Si-Mn
93XX, 98XX Ni-Cr-Mo 94XX Ni-Cr-Mo-Mn
XXBXX Boron XXLXX Lead
94XX Ni-
Sistem kodifikasi baja (lanjutan)
AISI/SAE and UNS Designation Systems and Composition Ranges for Plain Carbon Steel and Various Low-Alloy Steels
• Low-carbon steels
– Less than 0.25 wt%C
• Medium-carbon steels
– 0.25 ~ 0.60 wt%C
• High-carbon steels
– 0.60 ~ 1.4 wt%C
Classification of Steels
The iron–iron carbide phase diagram.
L + Fe3C
2.14 4.30
6.70
M
N
C
PE
O
G
F
H
Cementite Fe3C
x
x’
0.022
0.76
• Less than 0.25 wt%C
• Unresponsive to heat treatments intended to form martensite; strengthening is accomplished by cold work
• Microstructures: ferrite and pearlite
• Relatively soft and weak, but having outstanding ductility and toughness
• Typically, y = 275 MPa, UT = 415~550 MPa, and ductility = 25%EL
• Machinable, weldable, and, of all steels, are the least expensive to produce
• Applications: automobile body components, structural shapes, and sheets used in pipelines, buildings, bridges, etc.
Low-Carbon Steels
Composition of Five Plain Low-Carbon Steels
Mechanical Characteristics of Hot-Rolled Material and Typical Applications for Various
Plain Low-Carbon Steels
• 0.25 ~ 0.60 wt%C
• May be heat treated by austenitizing, quenching, and then tempering to improve their mechanical properties
• Microstructure: tempered martensite
• Stronger than low-carbon steels
• Applications: railway wheels and tracks, gears, crankshafts, and other machine parts
Medium-Carbon Steels
Typical Applications and Mechanical Property Ranges for Oil-Quenched and Tempered Plain Carbon
a Classified as high-carbon steels
• 0.60 ~ 1.4 wt%C
• Used in a hardened and tempered condition
• Hardest, strongest, and yet least ductile; especially wear resistant and capable of holding a sharp cutting edge
• Containing Cr, V, W, and Mo; these alloying elements combine with carbon to form very hard and wear-resistant carbide compounds (e.g., Cr23C6, V4C3, and WC)
• Applications: cutting tools and dies for forming and shaping materials, knives, razors, hacksaw blades, springs, and high-strength wire
High-Carbon Steels
Designations, Compositions, and Applications for Six Tool Steels
• Alloying elements: Cu, V, Ni, & Mo (total ~10wt%)
• Higher strength than low-carbon steels
• Most may be strengthened by heat treatments
• Ductile, fomable, machinable
• Tensile strength: > 480 MPa
High-Strength, Low-Alloy Steels
A Comparison of the Advantages Offered by Carbon Steel and Alloy SteelCarbon Steel Alloy Steel
Lower cost Higher strength
Greater availability Better wear
Toughness
Special high temperature
behavior
Better corrosion
resistance
Special electrical
properties 94XX Ni-
• Alloy steel is more expensive than carbon steel; it should be used only when a special property is needed.
What makes stainless steels “stainless”?
• Stainless steels are selected for their excellent resistance to corrosion.
• Stainless steels are divided into three classes: martensitic, ferritic, or austenitic
• The predominant alloying element is chromium; a concentration of at least 11 wt% Cr is required
– It permits a thin, protective surface layer of chromium oxide to form when the steel is exposed to oxygen.
– The chromium is what makes stainless steel stainless!
Stainless Steels
1) Relatively high density
2) Comparatively low electrical conductivity
3) Susceptibility to corrosion in some common environments
• Cast alloys — alloys that are so brittle that forming or shaping by appreciable deformation is not possible
• Wrought alloys — alloys that are amenable to mechanical deformation
Ferrous Alloys — Their Limitations
• Aluminum and aluminum alloys are the most widely used nonferrous metals.
• Properties
– Low density (2.7 g/cm3), as compared to 7.9 g/cm3 for steel
– High electrical and thermal conductivity
– Resistant to corrosion in some common environments
– Easily formed and thin Al foil sheet may be rolled
– Al has an FCC crystal structure; its ductility is retained even at very low temperatures
– Limitation: low melting temperature (660°C)
Aluminum and its Alloys
• Aluminum alloys: strengthened by cold working and alloying (Cu, Mg, Si, Mn, and Zn)
– Nonheat-treatable: single phase, solid solution strengthening
– Heat treatable: precipitation hardening (MgZn2)
• Applications: aircraft structural parts, beverage cans, bus bodies, and automotive parts (engine blocks, pistons, and manifolds)
– Engineering materials for transportation to effectively reduce fuel consumption
– Specific strength: the tensile strength-specific gravity ratio
Aluminum and its Alloys (Cont’d)
Aluminum Alloy Desginations
Material Number
Al (99.00% minimum and greater)
1XXX
Al alloys are grouped by major alloying elements
Copper 2XXX
Manganese 3XXX
Silicon 4XXX
Magnesium 5XXX
Magnesium and Silicon 6XXX 94XX Ni-
Aluminum’s use in vehicles is rapidly increasing due to a heightened need for fuel efficient, environmentally friendly vehicles
• Aluminum can provide a weight savings of up to 55 percent compared to an equivalent steel structure, while matching or exceeding crashworthiness standards of similarly sized steel structures.
• The Ford Motor Company now has aluminum-intensive test vehicles on the road, providing 46% weight savings in the structure, with no loss in crash protection.
Aluminum plate is used in the manufacture of aircraft and for fuel tanks in spacecraft
• Aircraft manufacturers use high-strength alloys (principally alloy 7075) to strengthen aluminum aircraft structures.
• Alloy 7075 has zinc and copper added for ultimate strength, but because of the copper it is very difficult to weld.
• 7075 has the best machinability and results in the finest finish.
Lightweight aluminum is a good material for conductor cables
• Electrical transmission lines are the largest users of aluminum rod/bar/wire products.
• In fact, this is the one market in which aluminum has virtually no competition from other metals.
• Aluminum is simply the most economical way to deliver electrical power.
Compositions, Mechanical Properties, and Typical Applications for Some Aluminum Alloys
• Unalloyed copper:
– So soft and ductile that it is difficult to machine
– Unlimited capacity to be cold worked
– Highly resistant to corrosion in diverse environments
• Copper alloys: strengthened by cold working and/or solid-solution alloying.
• Bronze and brass are two common copper alloys.
• Applications: costume jewelry, cartridge casings, automotive radiators, musical instruments, electronic packaging, and coins
Copper and its Alloys
• Bronze is an alloy of copper and tin.
– The first metal purposely alloyed by the smith
– May contain up to 25% tin
Bronze and Brass
• Brass is an alloy of copper and zinc.
– Contain 5-30% zinc
– The zinc increases the strength of the copper.
– Ductility and formability are also increased.
Bronze Mask
Cu-Zn Phase Diagram
• Properties
– Lowest density (1.7 g/cm3) of all the structural metals
– Mg has a HCP crystal structure; relatively soft and has a low elastic modulus (45 GPa)
– At room temperature difficult to deform; only small degrees of cold work may be imposed without annealing
– Most fabrication is by casting or hot working at temperatures between 200 and 350°C
– Low melting temperature (651°C)
– Relatively unstable and especially susceptible to corrosion in marine environments
• Applications: aircraft and missile application, automobiles, and in audio-video-computer-communications equipment
Magnesium and its Alloys
• Relatively new engineering materials that possess an extraordinary combination of properties
– Low density (4.5 g/cm3)
– High melting temperature (1668°C), high elastic modulus (107 GPa)
– Extremely strong: 1400 MPa tensile strength at room temperature, highly ductile and easily forged and machined
– Limitations
Chemical reactivity with other materials at elevated temperatures
Cost
• Applications: airplane structures, space vehicles, and in the petroleum and chemical industries
Titanium and its Alloys
Compositions, Mechanical Properties, and Typical Applications for Some Titanium Alloys
Alloy Type
Common Name (UNS
Numbser)
Composition (wt%)
Condition Tensile
Strength (MPa)
Yield Strength
(MPa)
Ductility (%EL)
Ti-6Al-4V (R564000)
6Al, 4V, balance Ti
Annealed 947 877 14
94XX Ni-
• Typical Applications: High-strength prosthetic implants, chemical-processing equipment, airframe structural components
• Titanium has become the leading structural metallic biomaterial and 50 years of clinical performance has proven its value.
• There are a few generic characteristics that biomaterials need to possess for applications as long-term implantable devices.
– must have the appropriate mechanical properties, taking into account the stress levels and frequencies that will be encountered and the expectations of stress transfer within the relevant part of the body
– must be sufficiently corrosion resistant, taking into account the duration of implantation and the consequences of any corrosion should it take place
– should have adequate biological safety
Titanium Biomaterials (e.g. Ti-6Al-4V)
• Superlative combinations of properties
– Nickel-based alloys
– Other alloying elements: Nb, Mo, W, Ta, Cr, and Ti
e.g. IN792: Ni-12Cr-10Co-2Mo-4W-3.5Al-4Ti-4Ta- 0.01B-0.09Zr-0.1C-0.5Hf
• Applications: aircraft turbine components
– Turbine blades and discs, high creep and oxidation resistance at elevated temperatures (1000°C)
– Must withstand exposure to severely oxidizing environments and high temperatures for reasonable time periods
– Density is an important consideration because centrifugal stresses are diminished in rotating parts when the density is reduced.
Superalloys
Modern Civil Aircraft Engines
• Turbine blades in a jet engine experience:
• Mechanical forces:
– Creep
– Fatigue
– Thermomechanical fatigue
• High temperature environment
– Oxidation
– Hot corrosion
Material Strength with Increased Temperature
Titanium Alloy
Steel
Aluminum Alloy
Nickel Alloy
Ni-based superalloys are used for turbine blades
• Modern aeroengine design constantly seeks to increase the engine operating temperature to improve overall efficiency.
• The materials for turbine blades are required to perform at higher and higher temperatures.
• The use of advanced nickel-based alloys, together with innovative cooling design
Polycrystalline turbine blade
Improvement in High-Temperature Creep Resistance of Turbine Blades
Columnar grain structure produced by a directional solidification technique
Creep resistance is further enhanced with single-crystal blades.
Thermal Barrier Coatings (TBCs)
• Demands for higher efficiency and lower emission require higher operating temperatures in both
– aircraft engines
– land-base power-generation gas turbines
• The typical melting points of the superalloys used for the turbine components range from 1230 ~ 1315°C
• The temperature in a combustion gas environment is > 1370°C
Thermal Barrier Coatings (TBCs)
• The superalloy technology alone cannot provide new metals with the improved high-temperature performance.
– Composition & microstructure evolutions
– Cooling strategy
• The key to meeting these new demanding goals lies in providing an insulating ceramic thermal barrier coating (TBC) to lower the surface temperature of the superalloy underneath
TBCs offer an increase in operating temperature greater than what superalloys achieved over 25 years
1965 1976 1985
Superalloy Development
TBC Ben
efit
167°C (300°F) Ceramic
83°C (150°F) Metal
Eq
uiv
ale
nt
Me
tal T
em
pe
ratu
re
Durham et al., 1993
TBCs comprise metal & ceramic multilayers
Thermally Grown Oxide (TGO)
(1-10m)
Ceramic Top Coat (100-400m)(Y2O3-Stabilized ZrO2)
Bond Coat (~100m)
Substrate
Cooling Air
Hot Gases
A complex interplay occurs in TBCs
• Diffusion
• Oxidation
• Phase transformation
• Elastic deformation
• Plastic deformation
• Creep deformation
• Thermal expansion
• Thermal conduction
• Radiation
• Fracture
• Fatigue
• Sintering
Understanding and improving scale-metal adhesion are critical for design of TBCs
10 µm
EB-PVDYSZ
AluminaScale
Spallation Zone
(Ni,Pt)AlBond Coat
PictureCourtesy of GEAE
• Melting temperatures range between 2468°C for niobium (Nb) and 3410°C for tungsten (W)
– Interatomic bonding is extremely strong.
– Large elastic moduli and high strength and hardness at ambient and elevated temperatures
• Applications:
– Ta and Mo are alloyed with stainless steel to improve its corrosion resistance.
– Molybdenum alloys: extrusion dies and structural parts in space vehicles
– Tungsten alloys: filaments, X-ray tubes, welding electrodes
Refractory Metals
• Expensive (precious) and superior or notable (noble) in properties
– Soft, ductile, and heat resistant
• Silver, gold, platinum, palladium, rhodium, ruthenium, iridium, and osmium
• Silver and gold may be strengthened by solid-solution alloying with copper
– Sterling silver: Ag-Cu (~7.5 wt% Cu)
• Applications:
– Jewelry, integrated circuit electrical contacts, chemical laboratory equipment (Pt), catalyst, thermo-couples
Noble Metals