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From left to right: three alloys (beryllium copper, Inconel, steel) and three pure metals (titanium, aluminium, magnesium)

An alloy is a mixture of chemical elements of which in most cases at least one is a metallic element, although it is also sometimes used for mixtures of elements; herein only metallic alloys are described. Metallic alloys often have properties that differ from those of the pure elements from which they are made. The vast majority of metals used for commercial purposes are alloyed to improve their properties or behavior, such as increased strength, hardness or corrosion resistance. Metals may also be alloyed to reduce their overall cost, for instance alloys of gold and copper.

In an alloy, the atoms are joined by metallic bonding rather than by covalent bonds typically found in chemical compounds.[1] The alloy constituents are usually measured by mass percentage for practical applications, and in atomic fraction for basic science studies. Alloys are usually classified as substitutional or interstitial alloys, depending on the atomic arrangement that forms the alloy. They can be further classified as homogeneous (consisting of a single phase), or heterogeneous (consisting of two or more phases) or intermetallic. An alloy may be a solid solution of metal elements (a single phase, where all metallic grains (crystals) are of the same composition) or a mixture of metallic phases (two or more solutions, forming a microstructure of different crystals within the metal).

Examples of alloys include red gold (gold and copper), white gold (gold and silver), sterling silver (silver and copper), steel or silicon steel (iron with non-metallic carbon or silicon respectively), solder, brass, pewter, duralumin, bronze, and amalgams. Alloys are used in a wide variety of applications, from the steel alloys, used in everything from buildings to automobiles to surgical tools, to exotic titanium alloys used in the aerospace industry, to beryllium-copper alloys for non-sparking tools.

Characteristics

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Liquid bronze, being poured into molds during casting

An alloy is a mixture of chemical elements, which forms an impure substance (admixture) that retains the characteristics of a metal. Alloys are made by mixing two or more elements, at least one of which is a metal. This is usually called the primary metal or the base metal, and the name of this metal may also be the name of the alloy. The other constituents may or may not be metals but, when mixed with the molten base, they will be soluble and dissolve into the mixture.[2]

The mechanical properties of alloys will often be quite different from those of its individual constituents. A metal that is normally very soft (malleable), such as aluminium, can be altered by alloying it with another soft metal, such as copper. Although both metals are very soft and ductile, the resulting aluminium–copper alloy will have much greater strength.[3] Adding a small amount of non-metallic carbon to iron trades its great ductility for the greater strength of an alloy called steel. Due to its very-high strength, but still substantial toughness, and its ability to be greatly altered by heat treatment, steel is one of the most useful and common alloys in modern use. By adding chromium to steel, its resistance to corrosion can be enhanced, creating stainless steel,[4] while adding silicon will alter its electrical characteristics, producing silicon steel.[5]

A brass lamp

Like oil and water, a molten metal may not always be miscible with another element. For example, lithium, magnesium, or silver are almost completely insoluble with pure iron.[6] Even when the constituents are soluble, each will usually have a saturation point, beyond which no more of the constituent can be added. Iron, for example, can stably hold a maximum of 6.67% carbon, forming a compound called cementite.[7]

Although the elements of an alloy usually must be soluble in the liquid state, they may not always be soluble in the solid state. If the metals remain soluble when solid, the alloy forms a solid solution, becoming a homogeneous structure consisting of identical crystals, called a phase.[8] If as the mixture cools the constituents become insoluble, they may separate to form two or more different types of crystals, creating a heterogeneous microstructure of different phases, some with more of one constituent than the other. However, in other alloys, the insoluble elements may not separate until after crystallization occurs. If cooled very quickly, they first crystallize as a homogeneous phase, but they are supersaturated with the secondary constituents. As time passes, the atoms of these supersaturated alloys can separate from the crystal lattice, becoming more stable, and forming a second phase that serves to reinforce the crystals internally.[9]

A gate valve, made from Inconel

Some alloys, such as electrum—an alloy of silver and gold—occur naturally.[10] Meteorites are sometimes made of naturally occurring alloys of iron and nickel, but are not native to the Earth.[11] One of the first alloys made by humans was bronze, which is a mixture of the metals tin and copper. Bronze was an extremely useful alloy to the ancients, because it is much stronger and harder than either of its components.[12] Steel was another common alloy. However, in ancient times, it could only be created as an accidental byproduct from the heating of iron ore in fires (smelting) during the manufacture of iron.[13] Other ancient alloys include pewter,[14] brass[15] and pig iron.[16]

In the modern age, steel can be created in many forms. Carbon steel can be made by varying only the carbon content, producing soft alloys like mild steel or hard alloys like spring steel. Alloy steels can be made by adding other elements, such as chromium, molybdenum, vanadium or nickel, resulting in alloys such as high-speed steel or tool steel. Small amounts of manganese are usually alloyed with most modern steels because of its ability to remove unwanted impurities, like phosphorus, sulfur and oxygen, which can have detrimental effects on the alloy.[17] However, most alloys were not created until the 1900s, such as various aluminium, titanium, nickel, and magnesium alloys.[18] Some modern superalloys, such as incoloy, inconel, and hastelloy, may consist of a multitude of different elements.[19]

An alloy is technically an impure metal, but when referring to alloys, the term impurities usually denotes undesirable elements. Such impurities are introduced from the base metals and alloying elements, but are removed during processing. For instance, sulfur is a common impurity in steel. Sulfur combines readily with iron to form iron sulfide, which is very brittle, creating weak spots in the steel.[20] Lithium, sodium and calcium are common impurities in aluminium alloys, which can have adverse effects on the structural integrity of castings. Conversely, otherwise pure-metals that contain unwanted impurities are often called "impure metals" and are not usually referred to as alloys. Impure metals such as cast iron or wrought iron are less controlled, but are often considered useful.[21]

Oxygen, present in the air, readily combines with most metals to form metal oxides; especially at higher temperatures encountered during alloying. Depending on the alloy, this can eventually result in a failure of the component being produced.[22] Great care is often taken during the alloying process to remove excess impurities, using fluxes, chemical additives, or other methods of extractive metallurgy.[23]

Theory

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Alloying a metal is done by combining it with one or more other elements. The most common and oldest alloying process is performed by heating the base metal beyond its melting point and then dissolving the solutes into the molten liquid, which may be possible even if the melting point of the solute is far greater than that of the base. For example, in its liquid state, titanium is a very strong solvent capable of dissolving most metals and elements. In addition, it readily absorbs gases like oxygen and burns in the presence of nitrogen. This increases the chance of contamination from any contacting surface, and so must be melted in vacuum induction-heating and special, water-cooled, copper crucibles.[24]

Interstitial diffusion through a cubic crystal lattice

Carbon has a very high melting-point and only does so under high atmospheric pressure,[25] so it was impossible for ancient civilizations to combine with iron as a liquid solute. However, alloying (in particular, interstitial alloying) may be performed with one or more constituents in a gaseous state, such as found in a blast furnace to make pig iron (liquid-gas), nitriding, carbonitriding or other forms of case hardening (solid-gas),[26] or the cementation process used to make blister steel (solid-gas).[27] It may also be done with one, more, or all of the constituents in the solid state, such as found in ancient methods of pattern welding (solid-solid), shear steel (solid-solid), or crucible steel production (solid-liquid), mixing the elements via solid-state diffusion.[28]

By adding another element to a metal, differences in the size of the atoms create internal stresses in the lattice of the metallic crystals; stresses that often enhance its properties. For example, the combination of carbon with wrought iron produces steel, which is stronger than iron, its primary element.[29] The electrical and thermal conductivity of alloys is usually lower than that of the pure metals.[citation needed] The physical properties, such as density, reactivity, Young's modulus of an alloy may not differ greatly from those of its base element, but engineering properties such as tensile strength,[30] ductility, and shear strength may be substantially different from those of the constituent materials. This is sometimes a result of the sizes of the atoms in the alloy, because larger atoms exert a compressive force on neighboring atoms, and smaller atoms exert a tensile force on their neighbors,[31] helping the alloy resist deformation. Sometimes alloys may exhibit marked differences in behavior even when small amounts of one element are present. For example, impurities in semiconducting ferromagnetic alloys lead to different properties, as first predicted by White, Hogan, Suhl, Tian Abrie and Nakamura.[32][33]

Unlike pure metals, most alloys do not have a single melting point, but a melting range during which the material is a mixture of solid and liquid phases (a slush). The temperature at which melting begins is called the solidus, and the temperature when melting is just complete is called the liquidus.[34] For many alloys there is a particular alloy proportion (in some cases more than one), called either a eutectic mixture or a peritectic composition, which gives the alloy a unique and low melting point, and no liquid/solid slush transition.[35][36]

Heat treatment

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Allotropes of iron, (alpha iron and gamma iron) showing the differences in atomic arrangement
Photomicrographs of steel. Top photo: Annealed (slowly cooled) steel forms a heterogeneous, lamellar microstructure called pearlite, consisting of the phases cementite (light) and ferrite (dark). Bottom photo: Quenched (quickly cooled) steel forms a single phase called martensite, in which the carbon remains trapped within the crystals, creating internal stresses

Alloying elements are added to a base metal, to induce hardness, toughness, ductility, or other desired properties. Many metals and alloys can be work hardened by creating defects in their crystal structure. These defects are created during plastic deformation by hammering, bending, extruding, et cetera, and are permanent unless the metal is recrystallized.[37] Otherwise, some alloys can also have their properties altered by heat treatment. Nearly all metals can be softened by annealing, which recrystallizes the alloy and repairs the defects, but not as many can be hardened by controlled heating and cooling.[38] Many alloys of aluminium, copper, magnesium, titanium, and nickel can be strengthened to some degree by some method of heat treatment, but few respond to this to the same degree as does steel.[39]

The base metal iron of the iron-carbon alloy known as steel, undergoes a change in the arrangement (allotropy) of the atoms of its crystal matrix at a certain temperature (usually 820 °C (1,500 °F) or more, depending on carbon content).[40] This allows the smaller carbon atoms to enter the interstices of the iron crystal. When this diffusion happens, the carbon atoms are said to be in solution in the iron, forming a particular single, homogeneous, crystalline phase called austenite. If the steel is cooled slowly, the carbon can diffuse out of the iron and it will gradually revert to its low temperature allotrope. During slow cooling, the carbon atoms will no longer be as soluble with the iron, and will be forced to precipitate out of solution, nucleating into a more concentrated form of iron carbide (Fe3C) in the spaces between the pure iron crystals. The steel then becomes heterogeneous, as it is formed of two phases, the iron-carbon phase called cementite (or carbide), and pure iron ferrite.[41] Such a heat treatment produces a steel that is rather soft. If the steel is cooled quickly, however, the carbon atoms will not have time to diffuse and precipitate out as carbide, but will be trapped within the iron crystals. When rapidly cooled, a diffusionless (martensite) transformation occurs, in which the carbon atoms become trapped in solution. This causes the iron crystals to deform as the crystal structure tries to change to its low temperature state, leaving those crystals very hard but much less ductile (more brittle).[42]

While the high strength of steel results when diffusion and precipitation is prevented (forming martensite), most heat-treatable alloys are precipitation hardening alloys, that depend on the diffusion of alloying elements to achieve their strength. When heated to form a solution and then cooled quickly, these alloys become much softer than normal, during the diffusionless transformation, but then harden as they age.[43] The solutes in these alloys will precipitate over time, forming intermetallic phases,[44] which are difficult to discern from the base metal. Unlike steel, in which the solid solution separates into different crystal phases (carbide and ferrite), precipitation hardening alloys form different phases within the same crystal. These intermetallic alloys appear homogeneous in crystal structure, but tend to behave heterogeneously, becoming hard and somewhat brittle.[39]

In 1906, precipitation hardening alloys were discovered by Alfred Wilm. Precipitation hardening alloys, such as certain alloys of aluminium, titanium, and copper, are heat-treatable alloys that soften when quenched (cooled quickly), and then harden over time.[45] Wilm had been searching for a way to harden aluminium alloys for use in machine-gun cartridge cases. Knowing that aluminium-copper alloys were heat-treatable to some degree, Wilm tried quenching a ternary alloy of aluminium, copper, and the addition of magnesium, but was initially disappointed with the results. However, when Wilm retested it the next day he discovered that the alloy increased in hardness when left to age at room temperature, and far exceeded his expectations. Although an explanation for the phenomenon was not provided until 1919, duralumin was one of the first "age hardening" alloys used, becoming the primary building material for the first Zeppelins, and was soon followed by many others.[46] Because they often exhibit a combination of high strength and low weight, these alloys became widely used in many forms of industry, including the construction of modern aircraft.[47]

Mechanisms

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Different atomic mechanisms of alloy formation, showing pure metal, substitutional, interstitial, and a combination of the two

When a molten metal is mixed with another substance, there are two mechanisms that can cause an alloy to form, called atom exchange and the interstitial mechanism. The relative size of each element in the mix plays a primary role in determining which mechanism will occur. When the atoms are relatively similar in size, the atom exchange method usually happens, where some of the atoms composing the metallic crystals are substituted with atoms of the other constituent. This is called a substitutional alloy. Examples of substitutional alloys include bronze and brass, in which some of the copper atoms are substituted with either tin or zinc atoms respectively.[48]

In the case of the interstitial mechanism, one atom is usually much smaller than the other and can not successfully substitute for the other type of atom in the crystals of the base metal. Instead, the smaller atoms become trapped in the interstitial sites between the atoms of the crystal matrix. This is referred to as an interstitial alloy. Steel is an example of an interstitial alloy, because the very small carbon atoms fit into interstices of the iron matrix.[48]

Stainless steel is an example of a combination of interstitial and substitutional alloys, because the carbon atoms fit into the interstices, but some of the iron atoms are substituted by nickel and chromium atoms.[39]

History and examples

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A meteorite and a hatchet that was forged from meteoric iron. Evidence of the Widmanstätten patterns from the original meteorite used to make the hatchet's head can be seen on its surface.

Meteoric iron

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The use of alloys by humans started with the use of meteoric iron, a naturally occurring alloy of nickel and iron. It is the main constituent of iron meteorites. As no metallurgic processes were used to separate iron from nickel, the alloy was used as it was.[49] Meteoric iron could be forged from a red heat to make objects such as tools, weapons, and nails. In many cultures it was shaped by cold hammering into knives and arrowheads. They were often used as anvils. Meteoric iron was very rare and valuable, and difficult for ancient people to work.[50]

Bronze and brass

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Bronze axe 1100 BC
14th century brass tray stand

Iron is usually found as iron ore on Earth, except for one deposit of native iron in Greenland, which was used by the Inuit.[51] Native copper, however, was found worldwide, along with silver, gold, and platinum, which were also used to make tools, jewelry, and other objects since Neolithic times. Copper was the hardest of these metals, and the most widely distributed. It became one of the most important metals to the ancients. Starting around 10,000 years ago in the highlands of Anatolia (Turkey), humans learned to smelt metals such as copper[52] and tin from ore. Early bronze alloys used copper and arsenic, but the latter can be toxic to the metal-workers. Around 2500 BC, people began alloying tin and copper to form bronze, which was much harder than its ingredients.[53] However, tin was rare, being found mostly in Great Britain.

In the Middle East, people began alloying copper with zinc to form brass.[54] Ancient civilizations took into account the mixture and the various properties it produced, such as hardness, toughness and melting point, under various conditions of temperature and work hardening, developing much of the information contained in modern alloy phase diagrams.[55] For example, arrowheads from the Chinese Qin dynasty (around 200 BC) were often constructed with a hard bronze-head, but a softer bronze-tang, combining the alloys to prevent both dulling and breaking during use.[56]

Amalgams

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Mercury has been smelted from cinnabar for thousands of years. Mercury dissolves many metals, such as gold, silver, and tin, to form amalgams (an alloy in a soft paste or liquid form at ambient temperature). Amalgams have been used since 200 BC in China for gilding objects such as armor and mirrors with precious metals. The ancient Romans often used mercury-tin amalgams for gilding their armor. The amalgam was applied as a paste and then heated until the mercury vaporized, leaving the gold, silver, or tin behind.[57] Mercury was often used in mining, to extract precious metals like gold and silver from their ores.[58]

Precious metals

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Electrum, a natural alloy of silver and gold, was often used for making coins

Many ancient civilizations alloyed metals for purely aesthetic purposes. In ancient Egypt and Mycenae, gold was often alloyed with copper to produce red-gold, or iron to produce a bright burgundy-gold. Gold was often found alloyed with silver or other metals to produce various types of colored gold. These metals were also used to strengthen each other, for more practical purposes. Copper was often added to silver to make sterling silver, increasing its strength for use in dishes, silverware, and other practical items.[59]

Quite often, precious metals were alloyed with less valuable substances as a means to deceive buyers.[59] Around 250 BC, Archimedes was commissioned by the King of Syracuse to find a way to check the purity of the gold in a crown, leading to the famous bath-house shouting of "Eureka!" upon the discovery of Archimedes' principle.[60]

Pewter

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The term pewter covers a variety of alloys consisting primarily of tin. As a pure metal, tin is much too soft to use for most practical purposes. However, during the Bronze Age, tin was a rare metal in many parts of Europe and the Mediterranean, so it was often valued higher than gold[citation needed]. To make jewellery, cutlery, or other objects from tin, workers usually alloyed it with other metals to increase strength and hardness. These metals were typically lead, antimony, bismuth or copper.[61] These solutes were sometimes added individually in varying amounts, or added together, making a wide variety of objects, ranging from practical items such as dishes, surgical tools, candlesticks or funnels, to decorative items like ear rings and hair clips.

The earliest examples of pewter come from ancient Egypt, around 1450 BC. The use of pewter was widespread across Europe, from France to Norway and Britain (where most of the ancient tin was mined) to the Near East.[62] The alloy was also used in China and the Far East, arriving in Japan around 800 AD, where it was used for making objects like ceremonial vessels, tea canisters, or chalices used in shinto shrines.[63]

Iron

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Puddling in China, c. 1637. Opposite to most alloying processes, liquid pig-iron is poured from a blast furnace into a container and stirred to remove carbon, which diffuses into the air forming carbon dioxide, leaving behind a mild steel to wrought iron

The first known smelting of iron began in Anatolia, around 1800 BC. Called the bloomery process, it produced very soft but ductile wrought iron. By 800 BC, iron-making technology had spread to Europe, arriving in Japan around 700 AD. Pig iron, a very hard but brittle alloy of iron and carbon, was being produced in China as early as 1200 BC, but did not arrive in Europe until the Middle Ages. Pig iron has a lower melting point than iron, and was used for making cast-iron. However, these metals found little practical use until the introduction of crucible steel around 300 BC.[55]

These steels were of poor quality, and the introduction of pattern welding, around the 1st century AD, sought to balance the extreme properties of the alloys by laminating them, to create a tougher metal. Around 700 AD, the Japanese began folding bloomery-steel and cast-iron in alternating layers to increase the strength of their swords, using clay fluxes to remove slag and impurities. This method of Japanese swordsmithing produced one of the purest steel-alloys of the ancient world.[55]

While the use of iron started to become more widespread around 1200 BC, mainly because of interruptions in the trade routes for tin, the metal was much softer than bronze. However, very small amounts of steel, (an alloy of iron and around 1% carbon), was always a byproduct of the bloomery process. The ability to modify the hardness of steel by heat treatment had been known since 1100 BC, and the rare material was valued for the manufacture of tools and weapons.[64]

Because the ancients could not produce temperatures high enough to melt iron fully, the production of steel in decent quantities did not occur until the introduction of blister steel during the Middle Ages. This method introduced carbon by heating wrought iron in charcoal for long periods of time, but the absorption of carbon in this manner is extremely slow thus the penetration was not very deep, so the alloy was not homogeneous. In 1740, Benjamin Huntsman began melting blister steel in a crucible to even out the carbon content, creating the first process for the mass production of tool steel. Huntsman's process was used for manufacturing tool steel until the early 1900s.[64]

The introduction of the blast furnace to Europe in the Middle Ages meant that people could produce pig iron in much higher volumes than wrought iron. Because pig iron could be melted, people began to develop processes to reduce carbon in liquid pig iron to create steel. Puddling had been used in China since the first century, and was introduced in Europe during the 1700s, where molten pig iron was stirred while exposed to the air, to remove the carbon by oxidation. In 1858, Henry Bessemer developed a process of steel-making by blowing hot air through liquid pig iron to reduce the carbon content. The Bessemer process led to the first large scale manufacture of steel.[64]

Steel is an alloy of iron and carbon, but the term alloy steel usually only refers to steels that contain other elements— like vanadium, molybdenum, or cobalt—in amounts sufficient to alter the properties of the base steel. Since ancient times, when steel was used primarily for tools and weapons, the methods of producing and working the metal were often closely guarded secrets. Even long after the Age of Enlightenment, the steel industry was very competitive and manufacturers went through great lengths to keep their processes confidential, resisting any attempts to scientifically analyze the material for fear it would reveal their methods. For example, the people of Sheffield, a center of steel production in England, were known to routinely bar visitors and tourists from entering town to deter industrial espionage. Thus, almost no metallurgical information existed about steel until 1860. Because of this lack of understanding, steel was not generally considered an alloy until the decades between 1930 and 1970 (primarily due to the work of scientists like William Chandler Roberts-Austen, Adolf Martens, and Edgar Bain), so "alloy steel" became the popular term for ternary and quaternary steel-alloys.[65][66]

After Benjamin Huntsman developed his crucible steel in 1740, he began experimenting with the addition of elements like manganese (in the form of a high-manganese pig-iron called spiegeleisen), which helped remove impurities such as phosphorus and oxygen; a process adopted by Bessemer and still used in modern steels (albeit in concentrations low enough to still be considered carbon steel).[64] Afterward, many people began experimenting with various alloys of steel without much success. However, in 1882, Robert Hadfield, being a pioneer in steel metallurgy, took an interest and produced a steel alloy containing around 12% manganese. Called mangalloy, it exhibited extreme hardness and toughness, becoming the first commercially viable alloy-steel.[67] Afterward, he created silicon steel, launching the search for other possible alloys of steel.[68]

Robert Forester Mushet found that by adding tungsten to steel it could produce a very hard edge that would resist losing its hardness at high temperatures. "R. Mushet's special steel" (RMS) became the first high-speed steel.[68] Mushet's steel was quickly replaced by tungsten carbide steel, developed by Taylor and White in 1900, in which they doubled the tungsten content and added small amounts of chromium and vanadium, producing a superior steel for use in lathes and machining tools. In 1903, the Wright brothers used a chromium-nickel steel to make the crankshaft for their airplane engine, while in 1908 Henry Ford began using vanadium steels for parts like crankshafts and valves in his Model T Ford, due to their higher strength and resistance to high temperatures.[46] In 1912, the Krupp Ironworks in Germany developed a rust-resistant steel by adding 21% chromium and 7% nickel, producing the first stainless steel.[68]

A typical example of a modern alloy is 304 grade stainless steel which is commonly used for kitchen utensils, pans, knives and forks. Sometime also known as 18/8, it as an alloy consisting broadly of 74% iron, 18% chromium and 8% nickel. The chromium and nickel alloying elements add strength and hardness to the majority iron element, but their main function is to make it resistant to rust/corrosion.

Others

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Due to their high reactivity, most metals were not discovered until the 19th century. A method for extracting aluminium from bauxite was proposed by Humphry Davy in 1807, using an electric arc. Although his attempts were unsuccessful, by 1855 the first sales of pure aluminium reached the market. However, as extractive metallurgy was still in its infancy, most aluminium extraction-processes produced unintended alloys contaminated with other elements found in the ore; the most abundant of which was copper. These aluminium-copper alloys (at the time termed "aluminium bronze") preceded pure aluminium, offering greater strength and hardness over the soft, pure metal, and to a slight degree were found to be heat treatable.[69] However, due to their softness and limited hardenability these alloys found little practical use, and were more of a novelty, until the Wright brothers used an aluminium alloy to construct the first airplane engine in 1903.[46] During the time between 1865 and 1910, processes for extracting many other metals were discovered, such as chromium, vanadium, tungsten, iridium, cobalt, and molybdenum, and various alloys were developed.[70]

Prior to 1910, research mainly consisted of private individuals tinkering in their own laboratories. However, as the aircraft and automotive industries began growing, research into alloys became an industrial effort in the years following 1910, as new magnesium alloys were developed for pistons and wheels in cars, and pot metal for levers and knobs, and aluminium alloys developed for airframes and aircraft skins were put into use.[46] The Doehler Die Casting Co. of Toledo, Ohio were known for the production of Brastil, a high tensile corrosion resistant bronze alloy.[71][72]

See also

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References

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Bibliography

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Revisions and contributorsEdit on WikipediaRead on Wikipedia
from Grokipedia
An alloy is a mixture composed of two or more elements, at least one of which is a metal, typically formed to exhibit enhanced properties such as greater strength, , , or compared to its individual components. These materials are fundamental to and , where they enable the development of versatile substances used across industries, from to . By combining metals like and tin to form or iron with carbon to create , alloys have revolutionized human technology by addressing limitations of pure metals, such as or low melting points. The history of alloys dates back over 5,000 years to around 3300 B.C., when ancient civilizations in the first combined and tin to produce , a harder and more durable material that marked the transition from the to the . This innovation facilitated the creation of advanced tools, weapons, and artifacts, profoundly influencing societal development and trade. Subsequent milestones include the around 1200 B.C., with iron-carbon alloys like emerging for their superior strength, and modern advancements in the , such as nickel-based superalloys capable of withstanding temperatures up to 2,300 °F without deforming, which have become essential for high-efficiency power generation and jet engines. Alloys are broadly classified into ferrous types, which contain iron as the primary component (e.g., steels and cast irons), and non-ferrous types, lacking iron (e.g., aluminum, , and ). On a structural level, they can be substitutional, where atoms of similar size replace one another in the crystal lattice (as in , a -zinc mixture), or interstitial, where smaller atoms occupy spaces between larger host atoms (as in , with carbon in an iron matrix). These categories allow for tailored properties: for instance, , an iron alloy with 18% and 8% , offers exceptional resistance due to a protective layer. In engineering applications, alloys are indispensable for their ability to balance mechanical properties like tensile strength and while maintaining conductivity and formability. Common examples include for marine hardware and sculptures due to its castability and resistance to , for musical instruments owing to its acoustic qualities and malleability, and in components for their high strength-to-weight ratio and heat tolerance. Superalloys, such as those based on with aluminum or additions, support critical infrastructure like gas turbines in power plants, enabling higher operating temperatures and improved energy efficiency. Overall, ongoing research continues to innovate alloy compositions for sustainable uses, including lightweight materials for electric vehicles and recyclable options to reduce environmental impact.

Definition and Fundamentals

Definition and Composition

An alloy is defined as a homogeneous or heterogeneous of two or more elements, with at least one being a metal, resulting in a that exhibits distinct from those of its individual constituents. This combination typically enhances desirable characteristics such as strength, durability, or corrosion resistance compared to pure metals, though the primary focus here is on compositional aspects. At the atomic level, alloys form through various structures depending on how solute atoms interact with the host metal lattice. In substitutional solid solutions, solute atoms of similar size replace host atoms in the crystal lattice, as seen in where atoms substitute for atoms in a face-centered cubic structure. Interstitial solid solutions occur when smaller solute atoms, such as or , occupy spaces between host atoms without displacing them, often leading to lattice distortion. Intermetallic compounds form ordered structures with specific stoichiometric ratios, where atoms arrange in a distinct crystal lattice different from the parent metals, exhibiting compound-like properties. Eutectic mixtures, conversely, consist of two or more phases in a lamellar or irregular microstructure that solidifies simultaneously from the melt at a fixed composition and temperature, without forming a single . The extent of solid solubility in alloys is governed by the , which provide empirical criteria for substitutional solutions. These rules stipulate that for significant solubility, the atomic size difference between solute and solvent must be less than 15%; the crystal structures must be identical; the electronegativities must be similar to ensure comparable bonding; and the valences should be similar, with solvents often accommodating solutes of higher valence more readily. Violations of these conditions often limit solubility and promote or compound formation. Alloy compositions are quantified using weight percent (wt%), atomic percent (at%), and , each serving distinct analytical purposes. Weight percent expresses the mass ratio of an element to the total alloy , calculated as wt%=([mass](/page/Mass) of elementtotal [mass](/page/Mass))×100\text{wt\%} = \left( \frac{\text{[mass](/page/Mass) of element}}{\text{total [mass](/page/Mass)}} \right) \times 100. To convert to atomic percent, divide the number of atoms of each element by the total number of atoms and multiply by 100: at%=(atoms of elementtotal atoms)×100\text{at\%} = \left( \frac{\text{atoms of element}}{\text{total atoms}} \right) \times 100, requiring atomic weights to determine atom counts from masses. , equivalent to atomic fraction for elemental alloys, is the ratio of moles of an element to total moles, xi=ninjx_i = \frac{n_i}{\sum n_j}, and is dimensionless for thermodynamic calculations. For example, in a binary alloy, if the weight percent of solute A is known, atomic percent is derived by at% A=100×(wt% A/MA)(wt% A/MA)+(wt% B/MB)\text{at\% A} = \frac{100 \times (\text{wt\% A} / M_A)}{(\text{wt\% A} / M_A) + (\text{wt\% B} / M_B)}, where MM denotes . These metrics enable precise control over alloy design to achieve targeted enhancements in mechanical properties.

Classification of Alloys

Alloys are classified based on their atomic and microstructural arrangement, phase composition, and the primary metal serving as the base, providing a framework to understand their diverse behaviors and applications. This taxonomy highlights how compositional choices influence phase stability and overall characteristics, with thermodynamic considerations from phase diagrams briefly underscoring the conditions for phase formation.

Structural Classification

Structurally, alloys are categorized into alloys, alloys, and multiphase alloys. alloys form when solute atoms substitute into the lattice of a metal, creating a homogeneous single phase without forming new compounds, as seen in substitutional solutions like copper-nickel alloys where atoms of similar size dissolve completely. alloys, in contrast, consist of ordered compounds with fixed stoichiometric ratios, such as Ni3Al, where distinct atomic arrangements yield unique properties distinct from random s. Multiphase alloys exhibit multiple coexisting phases, including eutectic structures where a liquid decomposes into two solid phases upon cooling, like the lead-tin solder with alternating lamellae of lead and tin, or peritectic structures where a solid and liquid react to form a new solid phase, as in the iron-carbon system.

Phase-Based Classification

Phase-based classification divides alloys into single-phase and multiphase types, determined by the degree of between components. Single-phase alloys arise from complete mutual , resulting in a microstructure without secondary phases, as in systems where alloying elements fully incorporate into the lattice across all compositions and temperatures. Multiphase alloys occur with partial , leading to the of secondary phases or distinct regions, such as in aluminum-copper alloys where limited causes precipitates (CuAl2) to form during aging.

Base Metal Categories

Alloys are also grouped by their base metal, reflecting differences in processing and performance. Ferrous alloys are iron-based, encompassing steels (with carbon as the primary alloying element) and cast irons, which dominate structural applications due to iron's abundance and versatility. Non-ferrous alloys exclude iron as the major component and include bases like (e.g., brasses and bronzes), aluminum (e.g., ), magnesium, and , valued for corrosion resistance and lightweight properties. Refractory alloys feature high-melting-point base metals such as , (e.g., superalloys like ), , and , designed for extreme temperature environments like turbines.

Special Classes

High-entropy alloys represent a special class defined by multiple principal elements (typically five or more) in near-equiatomic proportions, which maximize configurational to stabilize simple phases over complex intermetallics. Amorphous alloys, or metallic , form a non-crystalline structure lacking long-range atomic order, achieved through rapid solidification that bypasses and growth of crystals, as exemplified by Fe-based with superior magnetic properties.

Properties

Mechanical Properties

Mechanical properties of alloys encompass the behaviors exhibited under applied forces, including resistance to deformation, , and failure. These properties are critical for determining the suitability of alloys in structural applications, where they must withstand various loading conditions without permanent distortion or breakage. Key mechanical properties include tensile strength, which measures the maximum stress a material can endure while being stretched before fracturing; yield strength, defined as the stress at which a material begins to deform plastically; and , quantified using scales such as Brinell (via indentation with a or ball) or Rockwell (using or ball indenters). refers to the extent of plastic deformation before , often expressed as the percentage elongation in a tensile test, while indicates the ability to absorb energy and deform plastically without fracturing, assessed through impact tests like the Charpy method. Alloying significantly influences these properties through mechanisms such as , where solute atoms distort the solvent lattice, impeding dislocation motion and thereby increasing strength while often preserving . For instance, the addition of solute elements can elevate yield and tensile strengths by creating local strain fields that resist deformation. Additionally, plays a pivotal role via the Hall-Petch relationship, which describes how yield strength increases inversely with the of the average grain diameter: σy=σ0+kd1/2\sigma_y = \sigma_0 + k d^{-1/2} Here, σy\sigma_y is the yield strength, σ0\sigma_0 is a friction stress, kk is the strengthening coefficient, and dd is the grain diameter; finer grains enhance strength by providing more boundaries that block propagation. Under cyclic loading, alloys exhibit behavior characterized by progressive damage leading to at stresses below the yield strength. life is represented by S-N curves, which plot stress amplitude (S) against the number of cycles to (N), revealing an endurance limit—the maximum stress below which the material can endure infinite cycles without in many alloys. At elevated temperatures, creep becomes dominant, involving time-dependent deformation under constant stress; primary mechanisms include creep, where atomic enables material flow, and climb, allowing dislocations to bypass obstacles through vacancy-mediated movement. These processes accelerate at high temperatures, limiting the use of alloys in hot environments unless designed for creep resistance. Standardized testing methods ensure consistent evaluation of these properties, as outlined in standards. Tensile and yield strengths are determined via uniaxial tension tests (ASTM E8/E8M), hardness via indentation ( for Brinell, ASTM E18 for Rockwell), ductility through elongation measurement in tensile tests, and toughness using Charpy impact testing (ASTM E23), which quantifies energy absorption by a notched specimen struck by a . These protocols apply to a wide range of metallic alloys, providing reliable data for engineering design.

Physical and Chemical Properties

Alloys exhibit a range of thermal properties that differ from those of their constituent pure metals, influenced by composition and microstructure. In eutectic alloys, such as those formed by silver and , the is depressed below that of the individual components due to a reduction in free energy from atomic mixing, enabling lower-temperature processing. Thermal conductivity in metallic alloys often follows the Wiedemann-Franz law, which relates it proportionally to electrical conductivity and temperature, as observed in aluminum alloys where electronic contributions dominate . Thermal expansion coefficients vary widely; for instance, controlled-expansion alloys like (Fe-Ni) have low values around 1-2 × 10^{-6}/°C, minimizing dimensional changes under temperature fluctuations, while aluminum alloys reach 20-25 × 10^{-6}/°C. Electrical properties of alloys generally show higher resistivity than pure metals because alloying introduces scattering centers that impede flow, as demonstrated in surveys of metals like and its alloys where resistivity increases with solute content. Certain alloys, such as niobium-titanium (Nb-Ti), display with critical temperatures around 9-10 K at , making them suitable for high-field applications due to robust pairing of s. Magnetic behavior in alloys like iron-nickel (Fe-Ni) can exhibit strong , with compositions near 65% Fe showing high saturation magnetization and temperatures above 500°C, attributed to exchange interactions in the face-centered cubic . Chemically, alloys often demonstrate enhanced resistance through passivation, as in stainless steels containing at least 10.5% , where a thin Cr₂O₃ layer forms spontaneously on the surface, inhibiting further oxidation in aqueous environments. Oxidation behavior depends on alloying elements; for example, chromia-forming alloys develop protective scales that slow oxygen ingress, though at high temperatures, volatile species like CrO₃ can lead to breakaway oxidation. In scenarios, alloys' positions in the determine their potential; active alloys like zinc-aluminum rank anodic (more negative potentials, e.g., -1.00 to -1.10 V vs. Ag/AgCl in ), accelerating when coupled with nobler materials such as . Density, or specific gravity, in alloys typically falls between that of their components, reflecting volume fractions and atomic packing; for instance, (Cu-Zn) has a specific gravity of about 8.4-8.7, lower than pure (8.96) due to zinc's lighter . , particularly reflectivity, vary with composition in gold-silver alloys; pure reflects over 95% of visible with a yellowish hue, while increasing silver content shifts reflectivity toward silver's higher values (98% in the visible) and whiter appearance, altering color for applications like jewelry.

Theory of Alloy Formation

Phase Diagrams and Thermodynamics

The stability of phases in alloys is determined by thermodynamic principles, primarily through the minimization of the G=[H](/page/Enthalpy)TSG = [H](/page/Enthalpy) - TS, where HH is the , TT is the absolute , and SS is the . For processes such as phase transformations or solute mixing in alloys, the change in Gibbs free energy ΔG=Δ[H](/page/Enthalpy)TΔS\Delta G = \Delta [H](/page/Enthalpy) - T \Delta S dictates spontaneity: a negative ΔG\Delta G indicates a stable configuration, while positive values signify instability. In binary alloy systems, the driving force for mixing originates from the enthalpy of solution ΔH\Delta H, which can be negative (exothermic, promoting due to attractive interactions) or positive (endothermic, hindering mixing), counterbalanced by the always-positive entropic term TΔST \Delta S that favors disorder and configurational in solid solutions. These principles underpin the construction of phase diagrams, which represent equilibrium states by plotting the lowest-energy phases as functions of , composition, and . Binary phase diagrams illustrate these thermodynamic behaviors across different alloy types. In isomorphous systems, complete mutual solubility occurs in both liquid and solid states, as exemplified by the Cu-Ni alloy, where both elements share a face-centered cubic (FCC) crystal structure and similar atomic radii, resulting in a continuous solid solution phase α\alpha without intermediate compounds; the diagram features a lens-shaped region between the liquidus and solidus lines, reflecting gradual partitioning of components during solidification. Eutectic systems, such as Pb-Sn solders, exhibit limited solid solubility and feature an invariant eutectic point where a liquid of specific composition (e.g., 61.9 wt% Sn at 183°C) decomposes directly into two distinct solid phases (α\alpha-Pb and β\beta-Sn) upon cooling, driven by the convergence of Gibbs free energies of the phases at that point. Peritectic diagrams involve an invariant reaction where a solid phase reacts with a liquid to form a new solid phase, as observed in portions of the Cu-Zn system (e.g., at 598°C and 78.6 wt% Zn), where the thermodynamics favor the peritectic product due to lower free energy compared to the reactants. Systems with intermediate phases, often stoichiometric compounds like intermetallics, appear as vertical lines or plateaus in the diagram, subdividing the binary system into pseudo-binary segments; these phases form when the Gibbs free energy minimum occurs at off-stoichiometric compositions, stabilizing ordered structures with unique properties. Within two-phase regions of these diagrams, the relative proportions of coexisting phases are quantified using the , a mass-balance principle derived from . The weight fraction of the α\alpha phase, for instance, is calculated as: Wα=CβC0CβCαW_\alpha = \frac{C_\beta - C_0}{C_\beta - C_\alpha} where C0C_0 represents the overall alloy composition, and CαC_\alpha and CβC_\beta are the equilibrium compositions of the α\alpha and β\beta phases at a given , respectively; this "inverse lever" analogy ensures conservation of solute across the tie line connecting the phase boundaries. During cooling, equilibrium paths trace the phase boundaries, but practical nonequilibrium solidification—due to finite rates—introduces deviations such as coring (dendritic segregation where solute-rich solidifies last at interdendritic regions, creating composition gradients within grains) and macrosegregation (bulk-scale solute redistribution), which elevate local free energies and can lead to metastable microstructures. These effects are particularly pronounced in systems with partition coefficients k<1k < 1, where slower-diffusing solutes concentrate in the remaining . Phase diagrams thus provide a foundational tool for predicting and mitigating such behaviors in alloy processing.

Strengthening Mechanisms

Strengthening mechanisms in alloys primarily revolve around impeding the motion of dislocations, which are line defects in the crystal lattice responsible for plastic deformation. Dislocation theory posits that the ease of slip along crystallographic planes governs an alloy's ductility and strength; under applied stress, dislocations glide and multiply, enabling permanent shape change, but interactions with obstacles increase the stress required for further movement. Solute atoms, precipitates, grain boundaries, and other microstructural features act as barriers, elevating the yield strength by mechanisms that either distort the lattice or create interfaces that dislocations must overcome or bypass. This foundational understanding stems from early models by Orowan, Polanyi, and Taylor in the 1930s, which explained slip as cooperative atomic displacements mediated by dislocations. Solid solution strengthening occurs when solute atoms of different sizes or electronic structures are incorporated into the host lattice, generating local strain fields that interact with dislocations. Smaller or larger solute atoms cause tetragonal or hydrostatic distortions, respectively, forcing dislocations to expend energy to navigate these fields, thereby increasing the critical resolved shear stress. The strengthening effect scales with the solute concentration and modulus mismatch, often following a square-root dependence for low concentrations, as observed in dilute alloys like copper-zinc brasses. Chemical interactions, such as those between dislocations and interstitial solutes like carbon in iron, can also pin dislocations via Cottrell atmospheres, further enhancing strength at low temperatures. The strengthening effect increases with the degree of atomic size mismatch between solute and solvent atoms, which generates local strain fields that interact with dislocations. However, the maximum achievable solute concentration—and thus the strengthening—is limited by phase thermodynamics, including the , which require an atomic size difference of less than about 15% for extensive solid solubility. Precipitation hardening, also known as age hardening, exploits the formation of fine, coherent or semi-coherent precipitates from supersaturated solid solutions, which create stress fields that strongly impede dislocation motion. In aluminum-copper alloys, for instance, copper atoms cluster into Guinier-Preston zones, evolving into θ'' and then θ' phases (Al₂Cu), with the coherent θ' precipitates providing peak strengthening by forcing dislocations to bow around them via Orowan looping or shear through the particles. The kinetics of precipitation involve nucleation and growth, influenced by time-temperature-transformation (TTT) diagrams that map metastable and stable phase formation, allowing control over precipitate size and distribution for optimal strength. Strengthening peaks when precipitate spacing is minimal (around 10-50 nm), but overaging leads to incoherent θ phase growth, reducing effectiveness as dislocations bypass larger particles more easily. This mechanism has been seminal since Wilm's 1911 discovery and detailed in studies of Al-Cu systems. Work hardening, or strain hardening, arises from the progressive accumulation and tangling of dislocations during deformation, which increases the density of internal barriers and elevates the flow stress. As plastic strain increases, dislocations multiply via Frank-Read sources and interact to form junctions, sessile locks, and subgrain boundaries, raising the average stress needed for further glide—often described by a power-law relationship σ = σ₀ + Kε^n, where n is the strain-hardening exponent. In face-centered cubic alloys like nickel, this leads to significant strengthening at room temperature, but the effect saturates at high strains due to dynamic recovery. Alloying elements can enhance work hardening by slowing dislocation annihilation, though precipitates may reduce it by providing bypass routes. This mechanism is ubiquitous in cold-worked metals but temporary, as annealing restores ductility. Dispersion strengthening employs finely dispersed, thermodynamically stable second-phase particles that are insoluble in the matrix, pinning dislocations over extended periods even at elevated temperatures. Unlike precipitates, these dispersions (e.g., ThO₂ particles in ) do not coarsen significantly, maintaining Orowan stresses where dislocations loop around particles, with strengthening Δσ ≈ (Gb / λ) ln(r / b), λ being interparticle spacing. Thoriated tungsten exemplifies this, achieving high-temperature creep resistance in lamp filaments due to thoria's high melting point and low diffusivity, preventing recovery. This approach is vital for refractory alloys, offering strength up to 0.5 T_m without relying on solid solubility. Grain boundary strengthening leverages the barriers posed by high-angle grain boundaries to dislocation transmission, as described by the Hall-Petch relation: σ_y = σ_0 + k d^{-1/2}, where d is grain diameter, σ_0 the friction stress, and k a constant reflecting boundary locking. Smaller grains increase boundary density, forcing dislocations to pile up and activate sources in adjacent grains via stress concentrations, enhancing yield strength—e.g., reducing d from 100 μm to 1 μm can double strength in . In nanotwinned alloys, coherent twin boundaries act similarly, providing ultrahigh strength (up to 1 GPa in ) while preserving ductility, as twins block dislocations without fully halting them, enabling detwinning for deformation. This is evident in electrodeposited nanotwinned , where twin spacing below 15 nm yields exceptional properties. However, at nanoscale (<10 nm), inverse Hall-Petch softening may occur due to grain boundary sliding. These mechanisms often interplay, but they impose trade-offs, notably between strength and ductility, as excessive barriers promote early void nucleation at interfaces, leading to embrittlement. For example, high solute or precipitate content strengthens but reduces uniform elongation by localizing strain; nanotwinned structures mitigate this by allowing twin-mediated plasticity. Balancing these requires microstructural optimization to avoid intergranular fracture or solute segregation-induced brittleness.

Processing and Heat Treatment

Common Processing Techniques

Alloys are primarily fabricated from raw materials through melting and casting processes, which involve heating metals to their liquid state and solidifying them into desired shapes. Arc melting utilizes an electric arc between a consumable electrode and the melt to achieve high temperatures, suitable for reactive alloys like titanium, enabling precise control over composition and minimizing contamination. Induction melting, on the other hand, employs electromagnetic induction to heat the charge in a crucible, offering efficient melting for large volumes of non-reactive alloys such as steels and offering advantages in energy efficiency and uniform heating. These methods often incorporate vacuum or inert atmospheres to prevent oxidation and gas entrapment during solidification. Directional solidification is a specialized casting technique that controls the solidification front to produce single-crystal structures, achieved by withdrawing the mold from a hot zone or using chill plates to promote unidirectional growth, which enhances mechanical properties by eliminating grain boundaries. This process is critical for high-performance components requiring superior creep resistance. Casting defects like shrinkage porosity can be mitigated through riser designs that provide additional molten metal reservoirs. Deformation processes shape alloys by applying mechanical forces, categorized into hot working and cold working. Hot working, performed above the recrystallization temperature (typically 0.6–0.7 times the absolute melting point), includes , , and , which refine grain structure and improve ductility without significant work hardening. For instance, hot rolling reduces thickness by passing the alloy through rotating rolls at elevated temperatures, while involves compressive deformation using hammers or presses to form complex shapes with directional properties. Cold working, conducted at or near room temperature, imparts higher strength through strain hardening but requires annealing to restore ductility; common methods include cold rolling for sheet production and for profiles. Powder metallurgy offers an alternative route for alloys, particularly those with high melting points or requiring uniform microstructures, starting with atomized metal powders that are consolidated without full melting. Sintering heats the compacted powder below its melting point to promote diffusion bonding and densification, achieving near-full density while retaining fine grain sizes. Hot isostatic pressing (HIP) applies simultaneous high pressure (up to 200 MPa) and temperature (often 1000–1200°C) in an inert gas atmosphere to eliminate residual porosity, making it ideal for superalloys and refractory metals. Joining techniques enable the assembly of alloy components, with welding methods like tungsten inert gas (TIG) welding using a non-consumable tungsten electrode and inert shielding gas to produce high-quality welds in aluminum and stainless steel alloys, minimizing heat-affected zones. Friction stir welding, a solid-state process, involves a rotating tool that generates frictional heat to plastically deform and join materials without melting, suitable for lightweight alloys like aluminum-magnesium to avoid cracking. Brazing employs a filler metal with a lower melting point than the base alloys, heated in a furnace under vacuum or inert gas to wet and bond surfaces. Diffusion bonding achieves metallurgical joining through atomic diffusion at elevated temperatures (0.5–0.7 times melting point) under uniaxial pressure, preserving original microstructures in titanium and superalloys. Quality control in alloy processing focuses on reducing defects such as porosity and inclusions to ensure structural integrity. Vacuum melting and inert atmospheres, like , prevent gas absorption and oxidation, significantly lowering hydrogen-induced porosity in castings. Inclusion removal is achieved through techniques like electroslag remelting, which filters non-metallic particles during secondary melting, while porosity is further minimized in powder routes via HIP, achieving densities exceeding 99%. Processing parameters, including atmosphere purity and cooling rates, directly influence phase distribution, as controlled solidification promotes uniform microstructures.

Heat Treatment Methods

Heat treatment methods for alloys involve controlled thermal cycles applied after initial forming to modify microstructure, relieve internal stresses, and optimize mechanical properties such as hardness, ductility, and toughness. These processes exploit phase transformations and diffusion to achieve desired material behaviors without altering the overall composition. Common methods include annealing, hardening, solution treatment with aging, and specialized treatments like normalizing and cryogenic processing, each tailored to specific alloy systems like steels or aluminum alloys. Annealing encompasses several sub-processes aimed at softening the material and relieving stresses induced by prior deformation or casting. Recovery occurs at relatively low temperatures, where stored energy from cold working is released through dislocation rearrangement without significant microstructural change, improving ductility in alloys like low-carbon steels. Recrystallization follows at higher temperatures, forming new strain-free grains that replace deformed ones, as seen in process annealing of ferrous alloys heated to around 1000°F and cooled freely. Grain growth then enlarges these grains for further homogenization. Full annealing involves heating hypoeutectoid steels above the A3 line (e.g., 25-50°F above for carbon steels) followed by slow furnace cooling to produce coarse pearlite and soft ferrite, enhancing machinability. In contrast, stress-relief annealing heats below the A1 temperature (e.g., ~1000°F) to minimize distortion without phase changes, commonly applied to welded alloy components. Hardening processes in steels focus on forming martensite, a hard, supersaturated phase, through rapid cooling. Austenitizing first heats the alloy above the A3 or Acm line (e.g., 1530°F for 0.5% carbon steel) to fully dissolve carbon into austenite, preparing for transformation. Quenching then rapidly cools the austenite past the nose of the time-temperature-transformation (TTT) curve—typically in water, oil, or brine—to suppress pearlite or bainite formation and yield martensite, achieving maximum hardness dependent on carbon content (up to 65 HRC for high-carbon steels). Tempering subsequently reheats the quenched martensite to 400-1200°F for 1-2 hours, precipitating fine carbides to balance hardness and toughness while reducing brittleness; for example, low-temperature tempering (300-700°F) retains high hardness in tool steels. These treatments enhance strengthening mechanisms like solid solution and precipitation hardening in ferrous alloys. Solution treatment and aging, key for precipitation-hardenable non-ferrous alloys such as aluminum series (e.g., 2xxx, 6xxx, 7xxx), dissolve alloying elements into a supersaturated solid solution followed by controlled precipitation. Solution treatment heats the alloy to 488-540°C (e.g., 515-540°C for Al-Cu systems) for 20-65 minutes depending on thickness, then quenches rapidly to retain solutes at room temperature, forming Guinier-Preston zones during natural aging or stable precipitates like Mg₂Si or CuAl₂ during artificial aging at 120-400°C for 1-36 hours. This process significantly increases strength by impeding dislocation motion through coherent precipitates, as in 6061-T6 aluminum aged at 160°C for 18 hours. Overaging, however, occurs with excessive time or temperature, coarsening precipitates into less effective equilibrium phases (e.g., θ in Al-Cu), reducing peak strength but improving corrosion resistance in tempers like T7. Specialized heat treatments address specific microstructural needs. Normalizing heats alloys above the A3 or Acm line (e.g., 1500-1725°F for carbon steels) and air-cools to refine grain size and homogenize structure, producing finer pearlite than annealing for improved uniformity in structural steels like AISI 1030. Spheroidizing annealing, ideal for machinability in high-carbon steels (>0.60% C), heats just below A1 (e.g., 1300-1500°F) with prolonged holding (15-24 hours) to form globular carbides in a ferrite matrix, softening the alloy for cold drawing or machining as in AISI 1040. Cryogenic treatment cools quenched steels to -150°C or lower (e.g., liquid nitrogen) for 2-20 hours to transform retained austenite into martensite, reducing dimensional instability; in martensitic stainless steel 13Cr-2Ni-2Mo, this can decrease retained austenite content while promoting carbide precipitation for enhanced wear resistance.

Historical Development

Ancient and Pre-Industrial Alloys

The earliest known use of iron in human artifacts dates to prehistoric Egypt, where nine small tubular beads discovered in burials at Gerzeh, dated to approximately 3200 BCE, were crafted from hammered meteoritic iron. These beads, shaped by careful cold-working without melting, exhibit a characteristic high nickel content of around 7-10%, along with other trace elements like cobalt and germanium, which distinguish them from terrestrial iron ores and confirm their extraterrestrial origin from iron meteorites. This early exploitation of meteoric iron highlights its rarity and prestige in ancient societies, where it was likely valued for its celestial association and used in elite funerary contexts before smelting technology enabled widespread terrestrial iron production. The advent of intentional alloying marked a pivotal advancement in prehistoric , beginning with bronze in the during the late 5th to early 4th millennium BCE. -copper alloys, formed by ores naturally rich in or by deliberate addition of arsenical compounds, produced a harder, more castable material than pure , enabling the creation of sharper tools and ornaments. This innovation, evident in artifacts from Sumerian sites like Telloh and around 4000-3500 BCE, spread across and , fostering technological and cultural exchanges but also posing health risks due to toxic fumes during production. By the early BCE, bronze had transitioned to tin bronze as the dominant alloy, with the first deliberate copper-tin mixtures appearing in around 3000 BCE, as seen in tools and weapons from the . Tin bronze offered superior strength, corrosion resistance, and workability—typically with 5-10% tin content—revolutionizing warfare, agriculture, and trade during the , as exemplified by the standardized spearheads and axes that empowered Mesopotamian city-states. In parallel developments, other copper-based alloys emerged in various regions, including brass, a copper-zinc mixture, with early evidence of deliberate production in ancient India around the 4th century BCE. Artifacts from sites like Taxila and the Gangetic plain show zinc contents up to 20-30%, achieved through co-smelting copper with zinc-rich ores or calamine, yielding a more malleable and corrosion-resistant metal suited for decorative items and utensils. This innovation, predating widespread European brass-making, supported India's vibrant trade networks and artisanal traditions, though zinc's volatility during smelting limited early scalability. In East Asia, particularly in China, cast iron—a ferrous alloy with 2-4% carbon—was developed around the 8th to 5th century BCE through innovative blast furnace techniques that allowed molten iron to be poured into molds, enabling the mass production of complex tools, weapons, and vessels far earlier than in other regions. This advancement marked a significant shift in pre-industrial metallurgy, supporting agricultural and military expansions during the Warring States period. Concurrently, mercury-based amalgams appeared for decorative purposes, with fire gilding—applying a gold-mercury paste to copper or bronze surfaces and heating to evaporate the mercury—documented in ancient Rome by the 1st century CE. Roman artisans used this technique to gild statues, jewelry, and architectural elements, such as those in the Baths of Caracalla, creating a luxurious gold-like finish that enhanced the empire's aesthetic and symbolic displays of power, despite the hazardous mercury vapors involved. Precious metal alloys also played a crucial role in ancient economies and symbolism, particularly , a naturally occurring gold-silver alloy mined in around 600 BCE. Composed of roughly 45-55% gold and the rest silver, electrum was the material for the world's first coined , including the Lydian staters featuring a motif, which standardized value and facilitated trade across the Mediterranean and . To expand minting capacity amid growing demand, Lydian rulers like practiced debasement by alloying electrum with additional silver or , reducing intrinsic value while maintaining nominal weights, a practice that influenced subsequent Greek and Persian coinage systems but eroded trust when detected through testing. This manipulation underscored electrum's cultural impact, transforming it from a raw Anatolian resource into a cornerstone of early and interstate .

Alloys in the Industrial Era

The Industrial Era marked a transformative period in alloy development, driven by mechanized production and empirical , which enabled large-scale manufacturing to support railroads, machinery, and . Wrought iron, a nearly pure form of iron with low carbon content, had been the dominant structural material prior to the mid-19th century, but its limitations in strength and scalability spurred innovations in production. The , patented by in 1856, revolutionized steelmaking by using air blasts to oxidize impurities in molten , rapidly converting it to while controlling carbon levels to achieve desired properties like and . This method dramatically reduced costs and increased output, allowing U.S. steel production to rise from 13,000 tons in 1860 to over one million tons by 1879. Building on the , the open-hearth method, developed in the , further advanced production by melting iron in a shallow, regenerative furnace that used gaseous fuel for precise control over composition and temperature, producing higher-quality in larger batches. Alloying elements were increasingly incorporated; for instance, the addition of around enhanced steel's toughness by deoxidizing the melt and counteracting brittleness from impurities, enabling reliable tonnage production for industrial applications. These advancements shifted from artisanal practices to scientific , with post-1900 thermodynamic principles aiding alloy design. Pewter, a malleable tin-lead alloy traditionally used for and decorative items, saw refinement in the through standardized compositions—typically 80-90% tin and 10-20% lead—to improve properties and durability amid rising industrial demand. Tin-lead solders, with similar ratios (often 60% tin and 40% lead), became essential for joining metals in , , and , their low (around 183°C) facilitating widespread use following the 19th-century invention of the for precise application. As concerns over lead toxicity grew, lead-free alternatives emerged, such as —a tin-antimony-copper alloy with a brighter finish and no lead—gaining popularity by the mid-19th century for . The Hall-Héroult process, independently invented in 1886 by and Paul Héroult, enabled commercial aluminum production through of alumina dissolved in , reducing costs and making aluminum viable for industrial use. This breakthrough facilitated the development of aluminum alloys, notably —an age-hardenable Al-Cu-Mg-Mn alloy invented by Alfred Wilm in 1909—which offered high strength-to-weight ratio due to , revolutionizing construction in the early . Stainless steel emerged in 1913 when metallurgist at Brown Firth Research Laboratories in discovered that adding 12.8% to (with 0.24% carbon) imparted exceptional resistance by forming a passive layer. This martensitic alloy, initially tested for barrels but noted for its acid resistance, quickly found applications in and chemical , marking a key advance in durable alloys.

Notable Alloy Examples

Ferrous Alloys

Ferrous alloys are metallic materials in which iron serves as the primary constituent, typically alloyed with carbon and other elements to achieve desired mechanical properties such as strength, , and resistance. These alloys are broadly categorized into steels, with carbon content below approximately 2%, and cast irons, with higher carbon levels exceeding 2%. The addition of elements like , , and enhances specific attributes, including and , making ferrous alloys essential in structural, automotive, and tooling applications. Carbon steels form the foundational group of ferrous alloys, distinguished primarily by their carbon content, which directly influences , strength, and . Low-carbon steels, containing less than 0.3% carbon, exhibit excellent and fracture resistance but lower strength, rendering them suitable for applications requiring formability, such as pipelines and structural components. Medium-carbon steels, with 0.3-0.6% carbon, offer a balance of strength, , and moderate , making them ideal for machinery parts like crankshafts and railway wheels. High-carbon steels, exceeding 0.6% carbon, provide superior and wear resistance at the expense of , and are commonly used in cutting tools, springs, and wear-resistant surfaces. Alloy steels incorporate deliberate additions of elements such as (Cr), (Ni), and (Mo) to carbon steels, improving properties like , resistance, and high-temperature performance beyond what plain carbon steels offer. enhances and resistance, often at levels of 0.5-1.5%, while improves toughness and low-temperature strength, typically added at 1-5%. boosts overall strength and resistance to temper embrittlement, commonly at 0.1-0.5%. A representative example is AISI 4140 steel, with approximately 0.4% carbon, 1% Cr, and 0.2% Mo, valued for its balanced strength and toughness in gears, shafts, and axles. Tool steels like D2, featuring high content around 12% alongside 1.5% carbon, excel in abrasion resistance and are widely used for dies and cutting tools due to their ability to retain hardness at elevated temperatures. Cast irons represent high-carbon alloys with 2-4.5% carbon and typically 1-3% , cast into shapes due to their , and valued for their castability, , and cost-effectiveness. Gray cast iron, characterized by flake in a ferritic-pearlitic matrix, offers good and thermal conductivity but is weak and brittle in tension, finding primary use in blocks and bases for its properties. White cast iron, with carbon predominantly as (Fe₃C) due to low (<1%), is extremely hard and brittle, serving as an intermediate for further processing or in applications requiring wear resistance like grinding balls. Ductile cast iron, also known as nodular iron, features spheroidal nodules formed by magnesium addition (around 0.05%), which significantly enhances ductility and strength compared to gray iron, enabling its use in demanding components such as crankshafts and hydraulic cylinders. Stainless steels, a subset of ferrous alloys containing at least 10.5% chromium to form a passive oxide layer for corrosion resistance, are further divided into variants based on microstructure and alloying. Austenitic stainless steels, stabilized by nickel (typically 8-10%), remain face-centered cubic at all temperatures and are non-magnetic, with AISI 304 (18% Cr, 8% Ni) being a common grade for its excellent formability and corrosion resistance in chemical processing and food equipment. Ferritic stainless steels, with 10.5-27% Cr and low carbon (<0.1%), are body-centered cubic, magnetic, and offer good ductility and thermal conductivity but limited hardenability, used in automotive exhausts and appliances. Martensitic stainless steels, containing 11-17% Cr and higher carbon (0.1-1.2%), can be hardened by heat treatment to achieve high strength, suitable for cutlery and turbine blades. Duplex stainless steels combine austenitic and ferritic phases (roughly 50/50), providing superior strength and resistance to stress corrosion cracking compared to single-phase variants, often employed in marine and chemical environments. Their pitting resistance is quantified by the pitting resistance equivalent number (PREN), calculated as PREN = %Cr + 3.3×%Mo + 16×%N, where higher values indicate better localized corrosion resistance in chloride-rich settings.

Non-Ferrous Alloys

Non-ferrous alloys, based on metals other than iron, are prized for their reduced density, enhanced corrosion resistance, and superior electrical or thermal conductivity, enabling diverse applications in lightweight structures, electronics, and harsh environments. These alloys are typically categorized by their primary base metal, such as copper, aluminum, magnesium, titanium, or nickel, each offering distinct property profiles tailored to specific needs like machinability, strength-to-weight ratio, or high-temperature stability. Copper-based alloys combine excellent electrical and thermal conductivity with good corrosion resistance, making them ideal for electrical components, plumbing, and marine hardware. Brasses, copper-zinc alloys, are divided into alpha and beta phases depending on zinc content. Alpha brasses, containing up to 36% zinc, exhibit high ductility and formability, suitable for applications requiring bending or deep drawing, such as decorative fittings and rubber bonding. Beta brasses, with higher zinc levels forming a two-phase structure, provide superior machinability for precision components like screws and gears, though they risk dezincification in acidic or saline conditions when zinc exceeds 20%. Bronzes, primarily copper-tin alloys, deliver enhanced strength, toughness, and wear resistance over brasses, with applications in high-load scenarios. Phosphor bronzes, incorporating small phosphorus additions (0.01-0.35%), improve castability and fatigue strength, making them a staple for bearings, bushings, and springs that endure compressive stresses and friction. These alloys resist corrosion from salts and organic acids, supporting use in valves and marine propellers. Cupronickels, copper-nickel alloys with 2-30% nickel, stand out for their exceptional seawater corrosion resistance and biofouling inhibition, alongside high thermal conductivity and elevated-temperature strength. Common compositions like 90-10 or 70-30 Cu-Ni are employed in heat exchangers, condenser tubes, and desalination plants, where they withstand impingement and stress-corrosion cracking effectively. Aluminum-based alloys leverage a low density of about 2.7 g/cm³ for high strength-to-weight performance, with wrought and cast variants serving structural roles. The wrought 2xxx series, alloyed mainly with 1-10% copper, achieves high strength through heat treatment but offers moderate corrosion resistance, finding use in aerospace for aircraft skins and fuselages (e.g., 2024 alloy with 4.4% Cu). The 6xxx series, featuring magnesium and silicon (forming Mg₂Si), balances moderate strength with excellent corrosion resistance and extrudability, ideal for automotive body panels and architectural frames (e.g., 6061 with 1% Mg and 0.6% Si). Cast aluminum alloys like A356 (7% Si, 0.3% Mg) provide good fluidity for complex shapes and high ductility post-heat treatment, supporting automotive parts such as cylinder heads and wheels. Heat-treatable aluminum alloys, including the 2xxx, 6xxx, and cast A356, derive strength from precipitation hardening: solution treatment at 488–540°C dissolves alloying elements, quenching retains the supersaturated solid solution, and aging (natural or artificial at 115–190°C) precipitates fine particles for peak strength (e.g., T6 temper for A356 at 155°C for 3–5 hours). Non-heat-treatable alloys, such as the 1xxx, 3xxx, and 5xxx series, rely instead on strain hardening through cold working to enhance properties without thermal precipitation. Magnesium alloys emphasize extreme lightweighting with densities around 1.8 g/cm³, outperforming aluminum in specific strength for transportation. AZ91, containing 8.7% Al and 0.9% Zn, delivers a tensile strength of ~230 MPa and good castability via die-casting, used in automotive transmission housings, steering components, and aerospace brackets where weight savings reduce fuel consumption. Its moderate corrosion resistance, stemming from a protective oxide layer, is often augmented by coatings to suit humid or saline exposures. Titanium alloys provide an optimal blend of strength, low density (4.5 g/cm³), and biocompatibility, excelling in demanding conditions. Ti-6Al-4V, with 6% aluminum as an alpha stabilizer and 4% vanadium as a beta stabilizer, features a dual-phase alpha-beta microstructure (beta transus at approximately 995°C) that yields ultimate tensile strength of 900–1000 MPa and yield strength of ~830 MPa after annealing. This high strength-to-weight ratio, coupled with fatigue resistance and operation up to 400°C, positions it as the workhorse for aerospace airframes, turbine blades, and compressor disks. Nickel-based alloys dominate in corrosive, high-temperature realms due to their austenitic structures and alloying versatility. Monel 400 (66–67% Ni, 31.5–33% Cu, 2.5% Fe max) offers robust corrosion resistance in marine settings, with seawater attack rates under 0.025 mm/year and immunity to stress cracking, plus retained toughness at cryogenic temperatures (e.g., 180 ft-lb Charpy at -78°C). It serves in shipbuilding for pumps, valves, and shafts, as well as sour gas handling in oil refineries. Inconel 600 (72% min Ni, 14–17% Cr, 6–10% Fe) withstands oxidation up to 1093°C and maintains tensile strength of 550–690 MPa at room temperature, dropping controllably to 100 MPa at 980°C, with excellent resistance in both oxidizing and reducing atmospheres. This enables its use in aerospace gas turbines, chemical reactors, and heat-treatment furnaces, where thermal stability and fabricability are critical.

Modern Alloys and Applications

Advanced Alloy Types

Superalloys represent a class of advanced materials engineered for extreme environments, particularly in aerospace and power generation, where they withstand high temperatures, stresses, and corrosive conditions. Nickel-based superalloys, such as Inconel 718, derive their high-temperature strength from precipitation hardening, featuring a gamma matrix reinforced by gamma prime (γ') phase precipitates of Ni₃(Al,Ti) and gamma double prime (γ'') phase of Ni₃Nb, enabled by niobium additions. These precipitates provide exceptional creep resistance, allowing Inconel 718 to maintain structural integrity at temperatures up to 700°C under sustained loads. Cobalt-based superalloys, in contrast, offer superior melting points and oxidation resistance due to their face-centered cubic structure stabilized by elements like tungsten and chromium, making them suitable for hot-section components in gas turbines. Single-crystal variants of both nickel- and cobalt-based superalloys eliminate grain boundaries through directional solidification, enhancing creep resistance by minimizing intergranular diffusion and cavitation in turbine blades operating above 1000°C. Shape memory alloys exhibit unique thermomechanical behaviors arising from reversible phase transformations, enabling applications in actuators and medical devices. The prototypical example is Nitinol, a near-equiatomic nickel-titanium (NiTi) alloy, which undergoes a martensitic transformation between a high-temperature austenite phase (B2 structure) and a low-temperature martensite phase (B19'), allowing shape recovery upon heating after deformation. This shape memory effect stems from the diffusionless, reversible nature of the transformation, with transformation temperatures tunable via composition and processing to range from -100°C to 100°C. Superelasticity in Nitinol occurs above the austenite finish temperature, where stress induces martensite formation, enabling recoverable strains up to 8-10% without permanent deformation, due to the reversible austenite-martensite interface motion. High-entropy alloys (HEAs) are multicomponent systems with near-equiatomic compositions of five or more principal elements, promoting high configurational entropy to stabilize simple solid-solution phases over intermetallics. The canonical HEA, CoCrFeNiMn (often termed the Cantor alloy), features a face-centered cubic structure with lattice distortions from elemental size mismatches, contributing to solid-solution strengthening and enhanced mechanical properties. A key attribute is sluggish diffusion, where atomic mobility is reduced compared to conventional alloys—diffusion coefficients in CoCrFeNiMn are significantly lower than in pure FCC metals—owing to the complex chemical gradients and vibrational entropy effects, which enhance phase stability and creep resistance at elevated temperatures up to 800°C. As of 2025, ongoing research has advanced HEAs for applications in nuclear fusion reactors, improving radiation tolerance and high-temperature performance. Amorphous alloys, particularly bulk metallic glasses (BMGs), lack long-range atomic order, resulting in unique properties like high elastic limits and corrosion resistance. Zirconium-based BMGs, such as Zr₅₂.₅Cu₁₇.₉Ni₁₄.₆Al₁₀Ti₅ (a zirconium-based bulk metallic glass), achieve critical casting diameters of up to 7 mm through rapid cooling that suppresses crystallization, yielding a monolithic amorphous structure with elastic strains up to 2%, far surpassing crystalline metals, due to the absence of dislocations and reliance on shear band formation for deformation. Nanocrystalline alloys extend this paradigm by combining nanoscale grains (typically 10-100 nm) with amorphous or crystalline phases, produced via severe plastic deformation techniques like high-pressure torsion, which impose strains >5 to refine microstructures without melting. In alloys like nanocrystalline Ni-Fe or Zr-based systems, this yields ultra-high strength (up to 2 GPa) from , while maintaining through controlled recovery during processing.

Industrial and Emerging Applications

In aerospace applications, titanium alloys are widely utilized in engine components due to their exceptional strength-to-weight ratio, toughness, and ability to withstand high temperatures without creeping, enabling efficient performance in demanding environments. Aluminum alloys form the backbone of aircraft airframes, comprising approximately 80% of the structure by weight, which facilitates significant weight reductions—up to 20-30% compared to traditional materials—while maintaining structural integrity for fuel efficiency. In the automotive sector, high-strength steels are employed in crash structures such as side impact beams and pillars to enhance energy absorption and occupant safety, allowing vehicles to meet stringent crash test standards with lighter designs that improve fuel economy by 5-10%. Copper alloys serve as primary materials in for their superior electrical conductivity, often achieving up to 100% of the International Annealed Copper Standard, which minimizes energy loss in and distribution systems. In , lead-free , predominantly tin-silver-copper compositions, are standard for assembling printed circuit boards, providing reliable joints that withstand cycling and vibration without environmental hazards from lead. For , lithium alloy anodes, such as those incorporating aluminum or , enable higher energy densities in rechargeable batteries—with theoretical capacities exceeding 3000 mAh/g (e.g., ~3579 mAh/g for -based alloys)—compared to anodes (372 mAh/g), supporting advancements in electric vehicles and portable devices. Titanium alloys are favored for biomedical implants like hip replacements and dental fixtures owing to their outstanding and resistance in physiological environments, reducing rejection rates and promoting . Cobalt-chromium alloys are commonly used in prosthetics such as joint replacements for their high wear resistance and mechanical strength, enduring millions of load cycles with minimal degradation. Degradable magnesium alloys offer a temporary solution for orthopedic implants, gradually dissolving in the body over 6-12 months to eliminate the need for secondary surgeries while supporting through controlled . In additive manufacturing, 316L alloys are increasingly printed via to create complex, porous structures for biomedical scaffolds and parts, achieving densities over 99% with tailored mechanical properties. Recycling alloys presents challenges in sorting diverse compositions and removing impurities like iron or , which can degrade mechanical properties by up to 20% if accumulated beyond 0.5 wt%, necessitating advanced spectroscopic techniques for efficient material recovery. Sustainable alternatives, including bio-alloys such as magnesium-titanium hybrids, are emerging for eco-friendly implants that biodegrade without toxic residues, aligning with goals by reducing reliance on rare earth elements.

References

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