[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

CN102156184B - Method for predicting space between aluminium-silicon alloy eutectic structure lamellas - Google Patents

Method for predicting space between aluminium-silicon alloy eutectic structure lamellas Download PDF

Info

Publication number
CN102156184B
CN102156184B CN201010566116.3A CN201010566116A CN102156184B CN 102156184 B CN102156184 B CN 102156184B CN 201010566116 A CN201010566116 A CN 201010566116A CN 102156184 B CN102156184 B CN 102156184B
Authority
CN
China
Prior art keywords
alpha
beta
sin
phase
lambda
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201010566116.3A
Other languages
Chinese (zh)
Other versions
CN102156184A (en
Inventor
李强
曲迎东
李荣德
张超逸
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenyang University of Technology
Original Assignee
Shenyang University of Technology
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shenyang University of Technology filed Critical Shenyang University of Technology
Priority to CN201010566116.3A priority Critical patent/CN102156184B/en
Publication of CN102156184A publication Critical patent/CN102156184A/en
Application granted granted Critical
Publication of CN102156184B publication Critical patent/CN102156184B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Crystals, And After-Treatments Of Crystals (AREA)
  • Investigating Or Analyzing Materials Using Thermal Means (AREA)

Abstract

The invention relates to a method for predicting space between aluminium-silicon alloy eutectic structure lamellas; the method is characterized in that an experimental period can be greatly shortened by using a numerical simulation method to predict the space between aluminium-silicon alloy eutectic lamellas; the cost is low, and the prediction result is not limited by the experimental conditions; and the influences of a certain single factor to the space between the aluminium-silicon alloy eutectic structure lamellas can be inspected. The shortages that the cost of the existing experimental method for measuring the space between aluminium-silicon alloy eutectic structure lamellas is relatively high, the experimental period is long and the experiment results are influenced obviously by the experimental conditions are overcome; the computation is fast; the error is small; and the quantitative prediction to the space between eutectic lamellas can be realized.

Description

Method for predicting space between aluminium-silicon alloy eutectic structure lamellas
One, technical field:
The invention belongs to metallurgical technology field, relate generally to a kind of Forecasting Methodology of eutectic structure sheet interlayer spacing, particularly for the Forecasting Methodology of Alpax eutectic structure sheet interlayer spacing.
Two, background technology:
Alpax is one of most widely used aluminium alloy, and it is widely used in the fields such as automobile, electric power, aviation.Casting is a main method of Alpax moulding.But in casting process, al-si eutectic tissue is a kind of typical Solidification Microstructure Morphology.The sheet interlayer spacing of al-si eutectic tissue is a principal element that is directly connected to cast product mechanical property, Eutectic spacing for Alpax adopted experimental technique to measure more in the past, but the sheet interlayer spacing cost of determination of experimental method al-si eutectic tissue is higher, experimental period is long, and experimental result is affected significantly by experiment condition.
Three, summary of the invention:
1, goal of the invention:
The present invention is directed to the less present situation of Al-Si eutectic structure sheet interlayer spacing Quantitative study, a kind of method for predicting space between aluminium-silicon alloy eutectic structure lamellas is proposed, solve the existing problem of current determination of experimental method al-si eutectic tissue lamellar spacing, for Alpax eutectic structure performance prediction from now on provides theoretical direction, and can be applied directly to foundry method improvement, realize the sheet interlayer spacing of refinement al-si eutectic tissue.
2, technical scheme:
The present invention is achieved through the following technical solutions:
A method for predicting space between aluminium-silicon alloy eutectic structure lamellas, is characterized in that: the eutectic structure sheet interlayer spacing after doping Alpax under this cooling velocity and thermograde and solidify according to the cooling velocity of actual measurement and local thermograde, and step is as follows:
(1), set up Alpax eutectic structure sheet interlayer spacing forecast model:
First true origin QuαXiang center, determines the coordinate of y and z therefrom.Y axle is positioned in solid-liquid interface, and vertical with lamella.Problem reduction is become to two-dimensional state, and due to the symmetry of diffusion, its solution is in region, 0≤y≤λ/2.Solid-liquid interface is with speed stable growth in z direction of V, and diffusion equation is now:
∂ 2 C ∂ y 2 + ∂ 2 C ∂ z 2 + V D · ∂ C ∂ z = 0 - - - ( 1 )
Wherein, C is silicon solute concentration, and D is the coefficient of diffusion of solute in liquid phase.
Due in process of setting, temperature can have a certain impact to the solute coefficient of diffusion of liquid phase, therefore will predict accurately Eutectic spacing, temperature must be taken into account the impact of solute coefficient of diffusion.
(2), calculate solute coefficient of diffusion:
D = D 0 exp ( - Q R g T ) - - - ( 2 )
D in formula 0---equilibrium state solute coefficient of diffusion;
Q---atom diffusion activation energy;
R g---air constant;
T---temperature.
Due to D here 0, Q and R gbe constant, wherein D 0=8 * 10 -9;
Figure GDA0000413113700000023
these two data substitution formula (2) are obtained to solute coefficient of diffusion is:
Figure GDA0000413113700000024
(3), calculate eutectic structure sheet interlayer spacing λ:
According to the periodic change condition of eutectic composition, can obtain:
C = C e + Aexp ( - V Z D ) + Bexp ( - 2 πZ λ ) cos ( 2 πy λ ) - - - ( 3 )
Wherein, C efor balance eutectic composition, V zfor the eutectic growth speed in z direction, A, B are constants, and it is worth by formula (4), and (5) calculate:
A=fC′-C β (4)
B = f ( 1 - f ) VλC ′ 2 D sin ( πf ) - - - ( 5 )
Wherein C ' is eutectic line length.
(4), the constitutional supercooling degree of α phase and β phase
Figure GDA0000413113700000032
with
Figure GDA0000413113700000033
Δ T c α = | m α | [ A + B sin ( πf ) πf ] - - - ( 6 )
Δ T c β = - | m β | [ A - B sin ( πf ) π ( 1 - f ) ] - - - ( 7 )
Wherein, m αfor the slope of α phase liquidus curve, m βslope for β phase liquidus curve.In process of setting, the speed of growth at interface exerts an influence to solute distribution coefficient, adopts in the method its expression formula of solute redistribution coefficient of continuity model calculating α phase and β phase as follows:
m α = m 0 α ( 1 - k 0 α + ( k 0 α + Y ) ln ( k 0 α + Y k 0 α ( 1 + Y ) ) ) ( 1 - k 0 α ) ( 1 + Y ) - - - ( 8 )
m β = m 0 β ( 1 - k 0 β + ( k 0 β + Y ) ln ( k 0 β + Y k 0 β ( 1 + Y ) ) ) ( 1 - k 0 β ) ( 1 + Y ) - - - ( 9 )
Wherein Y = Rδ D L ,
M 0 α---equilibrium state α phase liquidus curve slope;
M 0 β---equilibrium state β phase liquidus curve slope;
K 0a---nonequilibrium condition solute redistribution coefficient;
K 0 β---nonequilibrium condition solute redistribution coefficient;
D l---non-equilibrium solute coefficient of diffusion.
(5), in eutectic growth process, the curvature of α phase and β phase is excessively cold
Figure GDA0000413113700000039
with
Figure GDA00004131137000000310
for:
ΔT r α = 2 Γ α sin ( θ α ) fλ - - - ( 10 )
ΔT r β = 2 Γ β sin ( θ β ) ( 1 - f ) λ - - - ( 11 )
Wherein, θ αfor the contact angle of α phase solid-liquid phase, θ βfor the contact angle of β phase solid-liquid phase, Γ αfor α phase Gibbs-Thomson free energy coefficient Γ βfor β phase Gibbs-Thomson free energy coefficient.
(6), the degree of supercooling of each phase is:
ΔT α = | m α | [ A + B sin ( πf ) πf ] + 2 Γ α sin ( θ α ) fλ - - - ( 12 )
ΔT β = - | m β | [ A - B sin ( πf ) π ( 1 - f ) ] + 2 Γ α sin ( θ β ) ( 1 - f ) λ - - - ( 13 )
By Δ T α| m β|+Δ T β| m α|, Δ T α=Δ T β=Δ T obtains:
ΔT = | m α | | m β | | m α | + | m β | Vλ C ′ 2 πD + 2 ( 1 - f ) | m β | Γ α sin ( θ α ) + 2 f | m α | Γ β sin ( θ β ) f ( 1 - f ) λ ( | m α | + | m β | ) - - - ( 14 )
In eutectic growth process, degree of supercooling can be write as:
ΔT = K c Vλ + K r λ - - - ( 15 )
Wherein
K c = | m α | | m β | | m α | + | m β | · C ′ 2 πD - - - ( 16 )
K r = 2 ( 1 - f ) | m β | Γ α sin ( θ α ) + 2 f | m α | Γ β sin ( θ β ) f ( 1 - f ) ( | m α | + | m β | ) - - - ( 17 )
According to equation (15), λ is asked to local derviation, the λ value while obtaining minimum subcooled temperature:
d ( ΔT ) dλ = K c V - K r λ 2 = 0 - - - ( 18 )
(16) and (17) are brought in equation (18) and can be obtained:
λ 2 V = K r K c = 4 πD f ( 1 - f ) f | m α | Γ β sin ( θ β ) + ( 1 - f ) | m β | Γ α sin ( θ α ) | m α | | m β | C ′ - - - ( 19 )
λ 2 V = 2 D p ′ f | m α | Γ β sin ( θ β ) + ( 1 - f ) | m β | Γ α sin ( θ α ) | m α | | m β | C ′ - - - ( 20 )
Wherein
K c = m ‾ C ′ P ′ f ( 1 - f ) D - - - ( 21 )
K r = 2 m ‾ [ Γ α sin ( θ α ) f | m α | + Γ β sin ( θ β ) ( 1 - f ) | m β | ] - - - ( 22 )
Wherein, P '=Σ (1/n 3π 3) sin 2(n π f),
By above-mentioned equation, can draw the al-si eutectic sheet interlayer spacing shown in Fig. 1 and Fig. 2 and degree of supercooling and speed of growth relation.
3, advantage and effect:
A kind of method for predicting space between aluminium-silicon alloy eutectic structure lamellas that the present invention proposes, the method tool has the following advantages:
Adopt method for numerical simulation prediction Alpax Eutectic spacing greatly to shorten experimental period, and cost is low, predicts the outcome and not limited by experiment condition, and can investigates the impact of a certain single technological factor on Alpax eutectic structure sheet interlayer spacing.Calculate fast, error is less, observes by experiment with result of calculation contrast and finds that the relative error of the method is less than 5%, can realize the quantification of Eutectic spacing is predicted.
Four, accompanying drawing explanation:
Fig. 1 is that Al-Si Eutectic spacing and degree of supercooling and speed of growth Δ T-λ-V are related to schematic diagram;
Fig. 2 is that the theoretical λ-V of Al-Si eutectic is related to schematic diagram.
Five, embodiment:
Eutectic structure is a kind of the most common Solidification Microstructure Morphology, and wherein the sheet interlayer spacing of eutectic structure pattern and eutectic structure is the principal element of the final eutectic cast properties of impact.Alpax is the most frequently used casting alloy, and it has good casting character, is therefore widely used in the fields such as automobile, electric power, machinery.According to classical Hall-Pitch formula, the size of crystal grain and the relation of mechanical property are known, and crystal grain is more tiny, and its mechanical property is higher.But in the eutectic structure of solidifying, Eutectic spacing is more tiny, the mechanical property of eutectic structure is better.Therefore refining eutectic sheet interlayer spacing is research and main contents controlling eutectic structure pattern.
Below in conjunction with specific embodiment, the present invention is described further:
A method for predicting space between aluminium-silicon alloy eutectic structure lamellas, is characterized in that: the eutectic structure sheet interlayer spacing after doping Alpax under this cooling velocity and thermograde and solidify according to the cooling velocity of actual measurement and local thermograde, and step is as follows:
(1), set up silicon eutectic structure sheet interlayer spacing forecast model:
First true origin QuαXiang center, determines the coordinate of y and z therefrom.Y axle is positioned in solid-liquid interface, and vertical with lamella.Problem reduction is become to two-dimensional state, and due to the symmetry of diffusion, its solution is in region, 0≤y≤λ/2.Solid-liquid interface is with speed stable growth in z direction of V, and diffusion equation is now:
∂ 2 C ∂ y 2 + ∂ 2 C ∂ z 2 + V D · ∂ C ∂ z = 0 - - - ( 1 )
Wherein, C is silicon solute concentration, and D is the coefficient of diffusion of solute in liquid phase.
Due in process of setting, temperature can have a certain impact to the solute coefficient of diffusion of liquid phase, therefore will predict accurately Eutectic spacing, temperature must be taken into account the impact of solute coefficient of diffusion.
(2), calculate solute coefficient of diffusion:
D = D 0 exp ( - Q R g T ) - - - ( 2 )
D in formula 0---equilibrium state solute coefficient of diffusion;
Q---atom diffusion activation energy;
R g---air constant;
T---temperature.
Due to D here 0, Q and R gbe constant, wherein D 0=8 * 10 -9;
Figure GDA0000413113700000063
these two data substitution formula (2) are obtained to solute coefficient of diffusion is:
Figure GDA0000413113700000071
(3), calculate eutectic structure sheet interlayer spacing λ:
According to the periodic change condition of eutectic composition, can obtain:
C = C e + Aexp ( - V Z D ) + Bexp ( - 2 πZ λ ) cos ( 2 πy λ ) - - - ( 3 )
Wherein, C efor balance eutectic composition, V zfor the eutectic growth speed in z direction, A, B are constants, and it is worth by formula (4), and (5) calculate:
A=fC′-C β (4)
B = f ( 1 - f ) VλC ′ 2 D sin ( πf ) - - - ( 5 )
Wherein C ' is eutectic line length.
(4), the constitutional supercooling degree of α phase and β phase
Figure GDA0000413113700000074
with
Figure GDA0000413113700000075
for:
Δ T c α = | m α | [ A + B sin ( πf ) πf ] - - - ( 6 )
Δ T c β = - | m β | [ A - B sin ( πf ) π ( 1 - f ) ] - - - ( 7 )
Wherein, m αfor the slope of α phase liquidus curve, m βslope for β phase liquidus curve.In process of setting, the speed of growth at interface exerts an influence to solute distribution coefficient, adopts in the method its expression formula of solute redistribution coefficient of continuity model calculating α phase and β phase as follows:
m α = m 0 α ( 1 - k 0 α + ( k 0 α + Y ) ln ( k 0 α + Y k 0 α ( 1 + Y ) ) ) ( 1 - k 0 α ) ( 1 + Y ) - - - ( 8 )
m β = m 0 β ( 1 - k 0 β + ( k 0 β + Y ) ln ( k 0 β + Y k 0 β ( 1 + Y ) ) ) ( 1 - k 0 β ) ( 1 + Y ) - - - ( 9 )
Wherein Y = Rδ D L
M 0 α---equilibrium state α phase liquidus curve slope;
M 0 β---equilibrium state β phase liquidus curve slope;
K 0a---nonequilibrium condition solute redistribution coefficient;
K 0 β---nonequilibrium condition solute redistribution coefficient;
D l---non-equilibrium solute coefficient of diffusion.
(5), in eutectic growth process, the curvature of α phase and β phase is excessively cold
Figure GDA0000413113700000081
with
Figure GDA0000413113700000082
for:
ΔT r α = 2 Γ α sin ( θ α ) fλ - - - ( 10 )
ΔT r β = 2 Γ β sin ( θ β ) ( 1 - f ) λ - - - ( 11 )
Wherein, θ αfor the contact angle of α phase solid-liquid phase, θ βfor the contact angle of β phase solid-liquid phase, Γ αfor α phase Gibbs-Thomson free energy coefficient Γ βfor β phase Gibbs-Thomson free energy coefficient.
(6), the degree of supercooling of each phase is:
ΔT α = | m α | [ A + B sin ( πf ) πf ] + 2 Γ α sin ( θ α ) fλ - - - ( 12 )
ΔT β = - | m β | [ A - B sin ( πf ) π ( 1 - f ) ] + 2 Γ α sin ( θ β ) ( 1 - f ) λ - - - ( 13 )
By Δ T α| m β|+Δ T β| m α|, Δ T α=Δ T β=Δ T obtains:
ΔT = | m α | | m β | | m α | + | m β | Vλ C ′ 2 πD + 2 ( 1 - f ) | m β | Γ α sin ( θ α ) + 2 f | m α | Γ β sin ( θ β ) f ( 1 - f ) λ ( | m α | + | m β | ) - - - ( 14 )
In eutectic growth process, degree of supercooling can be write as:
ΔT = K c Vλ + K r λ - - - ( 15 )
Wherein
K c = | m α | | m β | | m α | + | m β | · C ′ 2 πD - - - ( 16 )
K r = 2 ( 1 - f ) | m β | Γ α sin ( θ α ) + 2 f | m α | Γ β sin ( θ β ) f ( 1 - f ) ( | m α | + | m β | ) - - - ( 17 )
According to equation (15), λ is asked to local derviation, the λ value while obtaining minimum subcooled temperature:
d ( ΔT ) dλ = K c V - K r λ 2 = 0 - - - ( 18 )
(16) and (17) are brought in equation (18) and can be obtained:
λ 2 V = K r K c = 4 πD f ( 1 - f ) f | m α | Γ β sin ( θ β ) + ( 1 - f ) | m β | Γ α sin ( θ α ) | m α | | m β | C ′ - - - ( 19 )
λ 2 V = 2 D p ′ f | m α | Γ β sin ( θ β ) + ( 1 - f ) | m β | Γ α sin ( θ α ) | m α | | m β | C ′ - - - ( 20 )
Wherein
K c = m ‾ C ′ P ′ f ( 1 - f ) D - - - ( 21 )
K r = 2 m ‾ [ Γ α sin ( θ α ) f | m α | + Γ β sin ( θ β ) ( 1 - f ) | m β | ] - - - ( 22 )
Wherein, P '=Σ (1/n 3π 3) sin 2(n π f),
Figure GDA0000413113700000096
By above-mentioned equation, calculate the al-si eutectic sheet interlayer spacing shown in Fig. 1 and Fig. 2 and degree of supercooling and speed of growth relation.
Embodiment:
Said method material therefor parameter is as follows: Al-12.6mass%Si, and liquidus curve is 577 ℃, eutectic composition is 12.6%, m 0 α=-7.5, m 0 β=17.5, k 0a=0.13, k 0 β=2 * 10 -4, P '=8.9 * 10 -3, Γ α=1.96 * 10 -7, Γ β=1.7 * 10 -7, θ α=30 °, θ β=65 °,
Figure GDA0000413113700000097
the pouring temperature of alloy is 700 ℃, and mold temperature is 300 ℃.
To test β phase size and Eutectic spacing on the metallographic structure photo obtaining according to above-mentioned steps, measure.
That adopt is λ || metering system, λ || be that line is measured in the vertical direction of lamella, repeated measurement is averaged for 10 times.
Table 1 analog result and Comparison of experiment results
Figure GDA0000413113700000101
The sheet interlayer spacing of analog computation is 13.9 μ m as can be seen from Table 1, and the sheet interlayer spacing of the al-si eutectic tissue of practical measurement is 14.6 μ m, and error is 0.7 μ m, and relative error is only 5%, illustrates that model calculates reliable.
Eutectic structure sheet interlayer spacing after can doping Alpax under this cooling velocity and thermograde and solidify according to the cooling velocity of actual measurement and local thermograde; And temperature and the impact of cooling velocity on material thermal physical property parameter have been added in prediction al-si eutectic tissue lamellar spacing model, be mainly the impact of temperature and the cooling velocity liquidus curve slope of the coefficient of diffusion in aluminium liquid, aluminium silicon phasor on silicon, thereby guaranteed that model can realize the accuracy that realizes prediction in wider temperature range and larger cooling velocity interval.
The inventive method is equally applicable to the sheet interlayer spacing prediction of the eutectic freezing tissue of other alloys, the thermograde that can obtain by actual monitoring and cooling velocity, the sheet interlayer spacing of prediction eutectic.
This method for predicting space between aluminium-silicon alloy eutectic structure lamellas provided by the invention, adopt method for numerical simulation prediction Alpax Eutectic spacing greatly to shorten experimental period, and cost is low, predict the outcome and not limited by experiment condition, and can investigate the impact of a certain single factors on Alpax eutectic structure sheet interlayer spacing.Calculate fast, error is less, is suitable for commercial Application.

Claims (2)

1. a method for predicting space between aluminium-silicon alloy eutectic structure lamellas, it is characterized in that: the eutectic structure sheet interlayer spacing after doping Alpax under this cooling velocity and thermograde and solidify according to the cooling velocity of actual measurement and local thermograde, step is as follows:
(1), set up Alpax eutectic structure sheet interlayer spacing forecast model:
First true origin QuαXiang center, determines the coordinate of y and z thus; Y axle is positioned in solid-liquid interface, and vertical with lamella; Problem reduction is become to two-dimensional state; Due to the symmetry of diffusion, its solution is in region, 0≤y≤λ/2; Solid-liquid interface is with speed V stable growth in z direction, and diffusion equation is now:
∂ 2 C ∂ y 2 + ∂ 2 C ∂ z 2 + V D · ∂ C ∂ z = 0 - - - ( 1 )
In formula (1), C is silicon solute concentration, and D is the coefficient of diffusion of solute in liquid phase;
(2), calculate solute coefficient of diffusion:
D = D 0 exp ( - Q R g T ) - - - ( 2 )
In formula (2): D 0---equilibrium state solute coefficient of diffusion;
Q---atom diffusion activation energy;
R g---air constant;
T---temperature;
Due to D 0, Q and R gbe constant, wherein D 0=8 * 10 -9;
Figure FDA0000413113690000013
these two data substitution formula (2) are obtained to solute coefficient of diffusion is:
Figure FDA0000413113690000014
(3), calculate eutectic structure sheet interlayer spacing λ:
According to the periodic change condition of eutectic composition, obtain:
C = C e + Aexp ( - V Z D ) + Bexp ( - 2 πZ λ ) cos ( 2 πy λ ) - - - ( 3 )
Wherein, C efor balance eutectic composition, V zfor the eutectic growth speed in z direction, A, B are constants, and its value is calculated by formula (4), (5):
A=fC′-C β (4)
B = f ( 1 - f ) VλC ′ 2 D sin ( πf ) - - - ( 5 )
Wherein C ' is eutectic line length;
(4), the constitutional supercooling degree of α phase and β phase with
Figure FDA0000413113690000023
for:
Δ T c α = | m α | [ A + B sin ( πf ) πf ] - - - ( 6 )
Δ T c β = - | m β | [ A - B sin ( πf ) π ( 1 - f ) ] - - - ( 7 )
Wherein, m αfor the slope of α phase liquidus curve, m βslope for β phase liquidus curve;
(5), in eutectic growth process, the curvature of α phase and β phase is excessively cold
Figure FDA0000413113690000026
with
Figure FDA0000413113690000027
for:
ΔT r α = 2 Γ α sin ( θ α ) fλ - - - ( 10 )
ΔT r β = 2 Γ β sin ( θ β ) ( 1 - f ) λ - - - ( 11 )
Wherein, θ αfor the contact angle of α phase solid-liquid phase, θ βfor the contact angle of β phase solid-liquid phase, Γ αfor α phase Gibbs-Thomson free energy coefficient Γ βfor β phase Gibbs-Thomson free energy coefficient;
(6), the degree of supercooling of each phase is:
ΔT α = | m α | [ A + B sin ( πf ) πf ] + 2 Γ α sin ( θ α ) fλ - - - ( 12 )
ΔT β = - | m β | [ A - B sin ( πf ) π ( 1 - f ) ] + 2 Γ α sin ( θ β ) ( 1 - f ) λ - - - ( 13 )
By Δ T α| m β|+Δ T β| m α|, Δ T α=Δ T β=Δ T obtains:
ΔT = | m α | | m β | | m α | + | m β | Vλ C ′ 2 πD + 2 ( 1 - f ) | m β | Γ α sin ( θ α ) + 2 f | m α | Γ β sin ( θ β ) f ( 1 - f ) λ ( | m α | + | m β | ) - - - ( 14 )
In eutectic growth process, degree of supercooling is:
ΔT = K c Vλ + K r λ - - - ( 15 )
Wherein
K c = | m α | | m β | | m α | + | m β | · C ′ 2 πD - - - ( 16 )
K r = 2 ( 1 - f ) | m β | Γ α sin ( θ α ) + 2 f | m α | Γ β sin ( θ β ) f ( 1 - f ) ( | m α | + | m β | ) - - - ( 17 )
According to equation (15), λ is asked to local derviation, the λ value while drawing minimum subcooled temperature:
d ( ΔT ) dλ = K c V - K r λ 2 = 0 - - - ( 18 )
Formula (16) and formula (17) are brought in equation (18) and are obtained:
λ 2 V = K r K c = 4 πD f ( 1 - f ) f | m α | Γ β sin ( θ β ) + ( 1 - f ) | m β | Γ α sin ( θ α ) | m α | | m β | C ′ - - - ( 19 )
λ 2 V = 2 D p ′ f | m α | Γ β sin ( θ β ) + ( 1 - f ) | m β | Γ α sin ( θ α ) | m α | | m β | C ′ - - - ( 20 )
Wherein
K c = m ‾ C ′ P ′ f ( 1 - f ) D - - - ( 21 )
K r = 2 m ‾ [ Γ α sin ( θ α ) f | m α | + Γ β sin ( θ β ) ( 1 - f ) | m β | ] - - - ( 22 )
Wherein, P '=Σ (1/n 3π 3) sin 2(n π f),
By above-mentioned equation, can calculate al-si eutectic sheet interlayer spacing and degree of supercooling and speed of growth relation.
2. method for predicting space between aluminium-silicon alloy eutectic structure lamellas according to claim 1, it is characterized in that: in process of setting, the speed of growth at interface exerts an influence to solute distribution coefficient, adopts continuity model to calculate the solute redistribution coefficient of α phase and β phase, and its expression formula is as follows:
m α = m 0 α ( 1 - k 0 α + ( k 0 α + Y ) ln ( k 0 α + Y k 0 α ( 1 + Y ) ) ) ( 1 - k 0 α ) ( 1 + Y ) - - - ( 8 )
m β = m 0 β ( 1 - k 0 β + ( k 0 β + Y ) ln ( k 0 β + Y k 0 β ( 1 + Y ) ) ) ( 1 - k 0 β ) ( 1 + Y ) - - - ( 9 )
Wherein Y = Rδ D L ,
M 0 α---equilibrium state α phase liquidus curve slope;
M 0 β---equilibrium state β phase liquidus curve slope;
K 0a---nonequilibrium condition solute redistribution coefficient;
K 0 β---nonequilibrium condition solute redistribution coefficient;
D l---non-equilibrium solute coefficient of diffusion.
CN201010566116.3A 2010-11-30 2010-11-30 Method for predicting space between aluminium-silicon alloy eutectic structure lamellas Expired - Fee Related CN102156184B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201010566116.3A CN102156184B (en) 2010-11-30 2010-11-30 Method for predicting space between aluminium-silicon alloy eutectic structure lamellas

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201010566116.3A CN102156184B (en) 2010-11-30 2010-11-30 Method for predicting space between aluminium-silicon alloy eutectic structure lamellas

Publications (2)

Publication Number Publication Date
CN102156184A CN102156184A (en) 2011-08-17
CN102156184B true CN102156184B (en) 2014-04-02

Family

ID=44437754

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201010566116.3A Expired - Fee Related CN102156184B (en) 2010-11-30 2010-11-30 Method for predicting space between aluminium-silicon alloy eutectic structure lamellas

Country Status (1)

Country Link
CN (1) CN102156184B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106052543B (en) * 2016-07-19 2018-08-28 武汉钢铁有限公司 The method for measuring the true spacing of pearlite lamella
CN115852137A (en) * 2022-12-27 2023-03-28 太原科技大学 Method for eliminating low-alloy high-strength Q345E steel strip-shaped structure defects

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6188079B1 (en) * 1999-01-12 2001-02-13 Owens-Brockway Glass Container Inc. Measurement of hot container wall thickness
CN1542155A (en) * 2003-11-04 2004-11-03 上海大学 Fe-Ni-B alloy wire and production method thereof
CN1873401A (en) * 2006-06-28 2006-12-06 中国船舶重工集团公司第十二研究所 Method for forecasting defects of shrinkage cavity of ductile iron castings based on finite elements
CN101169386A (en) * 2007-11-30 2008-04-30 江苏大学 Calculation method for predicating directional solidification first dendrite distance

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6188079B1 (en) * 1999-01-12 2001-02-13 Owens-Brockway Glass Container Inc. Measurement of hot container wall thickness
CN1542155A (en) * 2003-11-04 2004-11-03 上海大学 Fe-Ni-B alloy wire and production method thereof
CN1873401A (en) * 2006-06-28 2006-12-06 中国船舶重工集团公司第十二研究所 Method for forecasting defects of shrinkage cavity of ductile iron castings based on finite elements
CN101169386A (en) * 2007-11-30 2008-04-30 江苏大学 Calculation method for predicating directional solidification first dendrite distance

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
Al-CuAl2共晶层片间距的数值模拟;张伟强等;《金属学报》;19980131;第34卷(第1期);1-6 *
张伟强等.Al-CuAl2共晶层片间距的数值模拟.《金属学报》.1998,第34卷(第1期),1-6.

Also Published As

Publication number Publication date
CN102156184A (en) 2011-08-17

Similar Documents

Publication Publication Date Title
CN103729511B (en) Method for predicating ingredient segregation degrees in casting process of complex-structure casting
Wang et al. Hot tearing susceptibility of binary Mg–Y alloy castings
Rosa et al. Cellular/dendritic transition and microstructure evolution during transient directional solidification of Pb-Sb alloys
Spinelli et al. Design of mechanical properties of Al-alloys chill castings based on the metal/mold interfacial heat transfer coefficient
CN102998324B (en) Thermal analysis and detection method for solidification grain size of magnesium alloy melt
CN109785907B (en) Method for predicting precipitation condition of TiN inclusion in molten steel solidification process
CN110851997B (en) System and method for measuring and predicting thickness of real initial solidified blank shell in crystallizer
Ares et al. Corrosion and wear resistance of hypoeutectic Zn–Al alloys as a function of structural features
Fu et al. Microstructure and mechanical properties of Al–1Mn and Al–10Si alloy circular clad ingot prepared by direct chill casting
CN102156184B (en) Method for predicting space between aluminium-silicon alloy eutectic structure lamellas
Hua et al. Influence of alloy elements and pouring temperature on the fluidity of cast magnesium alloy
CN103235001B (en) Steel solidus-liquidus temperature measurement method
CN102680326B (en) Device and method for testing hot crack of aluminum alloy under condition of active applied load
CN103521731A (en) Method for determining tundish outlet concentration through steel ingot multi-tundish concentration-changing continuous pouring
Liu et al. Effect of cooling rate on microstructure and inclusion in non-quenched and tempered steel during horizontal directional solidification
Mizukami et al. Prediction of density of carbon steels
Rosa et al. Cellular growth during transient directional solidification of Pb–Sb alloys
CN102430750B (en) Method and device for carrying out online component detection and solidification structure control on magnesium alloy
CN102416454A (en) Method for controlling dynamic soft reduction of continuous casting slab
Cao et al. Quantitative Characterization of Solidification Structure in Different Sections for Calculating the Permeability in Actual High-Carbon Steel Billet
CN101169386A (en) Calculation method for predicating directional solidification first dendrite distance
OKAMOTO et al. Solidification structure and segregation in iron-chromium-nickel alloys
Mizukami et al. Prediction of solid-liquid interfacial energy of steel during solidification and control of dendrite arm spacing
Kaya et al. Directional cellular growth of Al-2 wt% Li bulk samples
Guan et al. Calorimetric analysis of AZ91D magnesium alloy

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140402

Termination date: 20141130

EXPY Termination of patent right or utility model