A eutectic system or eutectic mixture is a homogeneous mixture that has a melting point lower than those of the constituents.[1] The lowest possible melting point over all of the mixing ratios of the constituents is called the eutectic temperature. On a phase diagram, the eutectic temperature is seen as the eutectic point (see plot on the right).
Non-eutectic mixture ratios have different melting temperatures for their different constituents, since one component's lattice will melt at a lower temperature than the other's. Conversely, as a non-eutectic mixture cools down, each of its components solidifies into a lattice at a different temperature, until the entire mass is solid.
Not all binary alloys have eutectic points, since the valence electrons of the component species are not always compatible in any mixing ratio to form a new type of joint crystal lattice. For example, in the silver-gold system the melt temperature (liquidus) and freeze temperature (solidus) "meet at the pure element endpoints of the atomic ratio axis while slightly separating in the mixture region of this axis".[2]
In the real world, eutectic properties can be used to advantage in such processes as eutectic bonding, where silicon chips are bonded to gold-plated substrates with ultrasound, and eutectic alloys prove valuable in such diverse applications as soldering, brazing, metal casting, electrical protection, fire sprinkler systems, and nontoxic mercury substitutes. By managing phase transformation during solidification, a suitable eutectic alloy can be made stronger than any of its individual components, a valuable property in an extreme application such as the hypereutectic cast aluminum pistons used in the high-revving twin-turbo intercooled DOHC Cadillac Blackwing V8 introduced in 2018.
The term was coined in 1884 by British physicist and chemist Frederick Guthrie (1833–1886). The word originates . Before his studies, chemists assumed "that the alloy of minimum fusing point must have its constituents in some simple atomic proportions", which was indeed proven to be not the case.[3]
The eutectic solidification is defined as follows:[4]
Liquid \xrightarrow[cooling]{eutectic\atoptemperature
This type of reaction is an invariant reaction, because it is in thermal equilibrium; another way to define this is the change in Gibbs free energy equals zero. Tangibly, this means the liquid and two solid solutions all coexist at the same time and are in chemical equilibrium. There is also a thermal arrest for the duration of the phase change during which the temperature of the system does not change.[4]
The resulting solid macrostructure from a eutectic reaction depends on a few factors, with the most important factor being how the two solid solutions nucleate and grow. The most common structure is a lamellar structure, but other possible structures include rodlike, globular, and acicular.[5]
Compositions of eutectic systems that are not at the eutectic point can be classified as hypoeutectic or hypereutectic:
As the temperature of a non-eutectic composition is lowered the liquid mixture will precipitate one component of the mixture before the other. In a hypereutectic solution, there will be a proeutectoid phase of species β whereas a hypoeutectic solution will have a proeutectic α phase.[4]
Eutectic alloys have two or more materials and have a eutectic composition. When a non-eutectic alloy solidifies, its components solidify at different temperatures, exhibiting a plastic melting range. Conversely, when a well-mixed, eutectic alloy melts, it does so at a single, sharp temperature. The various phase transformations that occur during the solidification of a particular alloy composition can be understood by drawing a vertical line from the liquid phase to the solid phase on the phase diagram for that alloy.
Some uses for eutectic alloys include:
The primary strengthening mechanism of the eutectic structure in metals is composite strengthening (See strengthening mechanisms of materials). This deformation mechanism works through load transfer between the two constituent phases where the more compliant phase transfers stress to the stiffer phase.[14] By taking advantage of the strength of the stiff phase and the ductility of the compliant phase, the overall toughness of the material increases. As the composition is varied to either hypoeutectic or hypereutectic formations, the load transfer mechanism becomes more complex as there is a load transfer between the eutectic phase and the secondary phase as well as the load transfer within the eutectic phase itself.
A second tunable strengthening mechanism of eutectic structures is the spacing of the secondary phase. By changing the spacing of the secondary phase, the fraction of contact between the two phases through shared phase boundaries is also changed. By decreasing the spacing of the eutectic phase, creating a fine eutectic structure, more surface area is shared between the two constituent phases resulting in more effective load transfer.[15] On the micro-scale, the additional boundary area acts as a barrier to dislocations further strengthening the material. As a result of this strengthening mechanism, coarse eutectic structures tend to be less stiff but more ductile while fine eutectic structures are stiffer but more brittle. The spacing of the eutectic phase can be controlled during processing as it is directly related to the cooling rate during solidification of the eutectic structure. For example, for a simple lamellar eutectic structure, the minimal lamellae spacing is:[16]
| ||||
λ |
Where is
\gamma
Vm
TE
\DeltaH
\DeltaT0
Strengthening metallic eutectic phases to resist deformation at high temperatures (see creep deformation) is more convoluted as the primary deformation mechanism changes depending on the level of stress applied. At high temperatures where deformation is dominated by dislocation movement, the strengthening from load transfer and secondary phase spacing remain as they continue to resist dislocation motion. At lower strains where Nabarro-Herring creep is dominant, the shape and size of the eutectic phase structure plays a significant role in material deformation as it affects the available boundary area for vacancy diffusion to occur.[17]
When the solution above the transformation point is solid, rather than liquid, an analogous eutectoid transformation can occur. For instance, in the iron-carbon system, the austenite phase can undergo a eutectoid transformation to produce ferrite and cementite, often in lamellar structures such as pearlite and bainite. This eutectoid point occurs at 723C and 0.76 wt% carbon.[18]
A peritectoid transformation is a type of isothermal reversible reaction that has two solid phases reacting with each other upon cooling of a binary, ternary, ..., n-ary alloy to create a completely different and single solid phase. The reaction plays a key role in the order and decomposition of quasicrystalline phases in several alloy types.[19] A similar structural transition is also predicted for rotating columnar crystals.
Peritectic transformations are also similar to eutectic reactions. Here, a liquid and solid phase of fixed proportions react at a fixed temperature to yield a single solid phase. Since the solid product forms at the interface between the two reactants, it can form a diffusion barrier and generally causes such reactions to proceed much more slowly than eutectic or eutectoid transformations. Because of this, when a peritectic composition solidifies it does not show the lamellar structure that is found with eutectic solidification.
Such a transformation exists in the iron-carbon system, as seen near the upper-left corner of the figure. It resembles an inverted eutectic, with the δ phase combining with the liquid to produce pure austenite at 1495C and 0.17% carbon.
At the peritectic decomposition temperature the compound, rather than melting, decomposes into another solid compound and a liquid. The proportion of each is determined by the lever rule. In the Al-Au phase diagram, for example, it can be seen that only two of the phases melt congruently, AuAl2 and Au2Al, while the rest peritectically decompose.
The composition and temperature of a eutectic can be calculated from enthalpy and entropy of fusion of each components.[20]
The Gibbs free energy G depends on its own differential:
G=H-TS ⇒ \begin{cases} H=G+TS\\ \left(
\partialG | |
\partialT |
\right)P=-S \end{cases} ⇒ H=G-T\left(
\partialG | |
\partialT |
\right)P.
Thus, the G/T derivative at constant pressure is calculated by the following equation:
\left( | \partialG/T |
\partialT |
\right)P =
1 | \left( | |
T |
\partialG | |
\partialT |
\right)P-
1 | |
T2 |
G = -
1 | |
T2 |
\left(G-T\left(
\partialG | |
\partialT |
\right)P\right) =-
H | |
T2 |
.
The chemical potential
\mui
\mui=
\circ | |
\mu | |
i |
+RTln
ai | |
a |
≈
\circ | |
\mu | |
i |
+RTlnxi.
At the equilibrium,
\mui=0
\circ | |
\mu | |
i |
\mui=\mu
\circ | |
i |
+RTlnxi=0 ⇒
\circ | |
\mu | |
i |
=-RTlnxi.
Using and integrating gives
\left( | \partial\mui/T |
\partialT |
\right)P=
\partial | |
\partialT |
\left(Rlnxi\right) ⇒ Rlnxi= -
| |||||||
T |
+K.
The integration constant K may be determined for a pure component with a melting temperature
T\circ
H\circ
xi=1 ⇒ T=
\circ | |
T | |
i |
⇒ K=
| |||||||
|
.
We obtain a relation that determines the molar fraction as a function of the temperature for each component:
Rlnxi=-
| |||||||
T |
+
| |||||||
|
.
The mixture of n components is described by the system
\begin{cases} lnxi+
| |||||||
RT |
-
| |||||||
|
=0,\\
n | |
\sum\limits | |
i=1 |
xi=1. \end{cases}
\begin{cases} \foralli<n ⇒ lnxi+
| |||||||
RT |
-
| |||||||
|
=0,\\ ln\left(1-
n-1 | |
\sum\limits | |
i=1 |
xi\right)+
| |||||||
RT |
-
| |||||||
|
=0,\end{cases}
which can be solved by
\begin{array}{c} \left[{{\begin{array}{*{20}c} {\Deltax1}\\ {\Deltax2}\\ {\Deltax3}\\ \vdots\\ {\Deltaxn}\\ {\DeltaT}\\ \end{array}}}\right]=\left[{{\begin{array}{*{20}c} {1/x1}&0&0&0&0&{-
| |||||||
RT2 |
.\left[{{\begin{array}{*{20}c} {\ln x_1 + \frac{H_1 ^\circ }{RT} - \frac{H_1^\circ }{RT_1^\circ }} \\ {\ln x_2 + \frac{H_2 ^\circ }{RT} - \frac{H_2^\circ }{RT_2^\circ }} \\ {\ln x_3 + \frac{H_3 ^\circ }{RT} - \frac{H_3^\circ }{RT_3^\circ }} \\ \vdots \\ {\ln x_{n - 1} + \frac{H_{n - 1} ^\circ }{RT} - \frac{H_{n - 1}^\circ }{RT_{n - 1}^\circ }} \\ {\ln \left({1 - \sum\limits_{i = 1}^{n - 1} {x_i } } \right) + \frac{H_n ^\circ }{RT} - \frac{H_n^\circ }{RT_n^\circ }} \\ \end{array} }} \right] \end