阅读说明：本技术 一种玻璃基板溢流成型退火装置设计方法 (Design method of glass substrate overflow forming annealing device ) 是由 李淼 李孟虎 徐莉华 于 2021-01-29 设计创作，主要内容包括：本发明提供了一种玻璃基板溢流成型退火装置设计方法,将玻璃基板退火划分为六个基本流体特征：自由流动的熔体、高粘滞塑性体、弹塑性体、弹性体初态、过渡为完全弹性体和完全弹性体等；玻璃从熔融态冷却至常温,其物理特性连续渐变规律是退火理论的唯一依据,通过产线设计确定基板玻璃在成型退火装置的参数以及依据玻璃基板料方的粘温特性曲线确定的温度参数,分别分为了不同的区段,计算玻璃基板的退火速度h-0、玻璃基板牵引速度PR和成型退火装置中厚度形成区的长度L-δ、预退火区的长度的长度L-1、均热区的长度L-2、退火区的长度L-3和后续退火区的长度L-4及成型退火装置总长度L-W,实现了更精确、更高效、更低成本的溢流成型退火装置设计。(The invention provides a design method of a glass substrate overflow forming annealing device, which divides the annealing of a glass substrate into six basic fluid characteristics: free flowing melts, high viscous plastomers, elastoplastomers, elastomer initial state, transition to full elastomers and full elastomers, and the like; the continuous gradual change rule of the physical characteristics of the glass is the only basis of the annealing theory when the glass is cooled from the molten state to the normal temperature, the parameters of the substrate glass in a forming annealing device are determined through the design of a production line, the temperature parameters are determined according to the viscosity-temperature characteristic curve of the glass substrate material side and are respectively divided into different sections, and the annealing speed h of the glass substrate is calculated 0 Glass substrate pulling speed PR and length L of thickness forming area in forming annealing device δ Length L of the pre-annealing zone 1 Length L of soaking zone 2 Length L of the annealing zone 3 And the length L of the subsequent annealing zone 4 And total length L of the forming and annealing device W And the design of the overflow forming annealing device with higher accuracy, higher efficiency and lower cost is realized.)

1. A design method of a glass substrate overflow forming annealing device is characterized by comprising the following steps:

step 1, determining parameters of substrate glass in a forming annealing device through production line design;

step 2, determining the temperature T of the overflow brick tip according to the viscosity-temperature characteristic curve of the glass substrate material square_iTheoretical annealing starting point temperature T of glass substrate_TExpansion softening point temperature T_dActual annealing starting point temperature T_aStrain point temperature T_stAnnealing furnace exit temperature T_o；

Step 3, dividing the forming annealing device into different functional sections according to the thermodynamic and kinetic characteristics of the glass, wherein the functional sections comprise a thickness forming zone, a pre-annealing zone, a soaking zone, an annealing zone and a subsequent annealing zone;

step 4, calculating the annealing speed h of the glass substrate according to different functional sections₀Glass substrate pulling speed PR and length L of thickness forming area in forming annealing device_δLength L of the pre-annealing zone₁Length L of soaking zone₂Length L of the annealing zone₃And the length L of the subsequent annealing zone₄And total length L of the forming and annealing device_W。

2. The method as claimed in claim 1, wherein the parameters of the substrate glass determined by the production line design in step 1 include the draw-out amount Q of the substrate glass on the production line, the average draw width L of the glass substrate, the product width W of the glass substrate, and the target thickness δ of the glass substrate.

3. The method of claim 1, wherein the temperature T of the overflow brick tip in step 2 is higher than the temperature T of the overflow brick tip_iSetting the corresponding viscosity eta_iTheoretical annealing starting point temperature T of glass substrate_TSetting the corresponding viscosity eta_T＝10⁸Pa.s, expansion softening point temperature T_dSetting the corresponding viscosity eta_d＝10¹¹Pa s, actual annealing starting point temperature T_aSetting the corresponding viscosity eta_a＝10¹²Pa · s, temperature T at which strain point is the lower limit of annealing_stSetting the corresponding viscosity eta_st＝10^13.5Pa.s, annealing furnace exit temperature T_o(ii) a Wherein, the temperature T of the overflow brick tip_iCorresponding viscosity η_i＝10^3.8Pa·s～10^4.2Pa · s; annealing furnace exit temperature T_o＝300℃～500℃。

4. The method according to claim 1, wherein in step 3, the temperature range of the thickness forming region in different functional sections of the forming lehr device is T_i～T_TThe temperature interval of the pre-annealing area is T_T～T_dThe temperature interval of the soaking zone is T_d～T_aThe temperature interval of the annealing zone is T_a～T_stAnd the temperature interval of the subsequent annealing zone is T_st～T_o。

5. The method of claim 4, wherein the difference in temperature delta T between the thickness forming zones in different functional sections of the lehr apparatus is a function of the temperature drop across the thickness forming zones_δ＝T_T-T_iTemperature drop difference Δ T of pre-annealing zone₁＝T_d-T_TTemperature drop difference of soaking zone delta T₂＝T_a-T_dTemperature drop difference Δ T of annealing zone₃＝T_st-T_aTemperature drop difference delta T of subsequent annealing zone₄＝T_o-T_st。

6. The method as claimed in claim 1, wherein in step 4, the annealing speed h of the glass substrate is set to be higher than that of the annealing apparatus₀The calculation method comprises the following steps:

l1 calculating the structural stress σ of the glass substrate_s：

Wherein alpha is_UTemperature at expansion softening point T_dLinear coefficient of thermal expansion of alpha_gTo glass transition point temperature T_gThe coefficient of linear thermal expansion of (a),is the thermal conductivity coefficient, lambda is the thermal conductivity coefficient of the glass substrate, rho is the density of the glass substrate, C_pThe specific heat capacity of the glass substrate is shown, and mu is the Poisson ratio; e is Young's modulus; h is₀Is the annealing speed of the glass substrate, delta is the target thickness of the glass substrate,. phi_sThe stress growth coefficient of the residual structure is considered when the relaxation factor is considered; wherein the physical parameters are lambda, rho and C_pThe temperatures corresponding to μ and E are strain point temperatures T_st；

L2, coefficient of increase of residual structural stress psi when calculating relaxation factors_s；

Wherein h is₀Is the annealing speed of the glass substrate;

l3, calculating the stress σ of the glass substrate due to the reverse temperature difference_T；

Wherein alpha is a glass baseThe coefficient of linear thermal expansion of the plate,is the thermal conductivity coefficient, lambda is the thermal conductivity coefficient of the glass substrate, rho is the density of the glass substrate, C_pThe specific heat capacity of the glass substrate is shown, and mu is the Poisson ratio; e is Young's modulus; h is₀The cooling rate of the glass substrate is determined, delta is the target thickness of the glass substrate, alpha_TThe scale factor of the unrelaxed part in the relaxation factor of the temperature difference stress under the dynamic temperature condition; physical property parameters of lambda, rho and C_pThe temperatures corresponding to μ and E are strain point temperatures T_st(ii) a When overflow forming is directly annealed, alpha_T＝0；

L4, calculating the allowable stress delta n of the glass substrate with the thickness delta;

Δn＝B×(σ_T+σ_s)；

wherein, Delta n is the allowable stress of the glass substrate with the thickness of Delta, and B is the photoelastic coefficient of the glass substrate; sigma_sStructural stress of the glass substrate; sigma_TIs the reverse temperature differential stress of the glass substrate;

l5, the annealing rate h of the glass substrate was obtained by combining the calculation formulas of L1, L2, L3 and L4₀。

7. The method as claimed in claim 1, wherein in step 4, the drawing speed PR of the glass substrate of the forming and annealing device is calculated;

wherein Q is the extraction amount of the substrate glass in a production line, L is the average extraction width of the glass substrate, rho is the density of the glass substrate, and delta is the target thickness of the glass substrate.

8. The method as claimed in claim 1, wherein in step 4, the forming and annealing device is usedThickness forming region length L_δThe calculation method comprises the following steps:

s1, calculating the traction force F of the traction roller_PR；

Wherein: t is_PFor torque of the pulling rolls, I_PThe polar moment of inertia of the drawing roll, D the diameter of the drawing roll and delta the target thickness of the glass substrate;

s2, calculating the length L of the thickness forming area of the forming annealing device_δ

Wherein eta is_iThe viscosity of the root of the overflow brick tip, Q the extraction amount of the substrate glass in a production line, L the average extraction width of the glass substrate, d the thickness of the glass belt leaving the root of the overflow brick, and F_PRIs the pulling roll pulling force, delta is the target thickness of the glass substrate;

s3, calculating the thickness d of the glass ribbon leaving the root of the overflow brick;

wherein eta is_iThe viscosity of the overflow brick tip (root), Q the glass extraction amount of a design production line, L the average extraction width of a glass substrate, rho the density of the glass substrate, g the gravity acceleration, epsilon the empirical coefficient, and epsilon being 0.5-0.8.

9. The method as claimed in claim 1, wherein in step 4, the length L of the pre-annealing region of the forming and annealing apparatus is calculated₁Length L of soaking zone₂Length L of the annealing zone₃And the length L of the subsequent annealing zone₄；

Calculating the length L of the pre-annealing area of the forming annealing device₁：

Wherein, Delta T₁＝T_d-T_TThe temperature difference is reduced in the pre-annealing region, h₀Is the annealing speed of the glass substrate, PR is the pulling speed of the glass substrate, K₁For correction factors, the pre-annealing zone K₁＝1；

Calculating the length L of the soaking zone of the forming annealing device₂：

Wherein, Delta T₂＝T_a-T_d＝T_g-T_dThe temperature difference is reduced in the soaking zone h₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₁For correction factors, general soaking zone K₂＝1；

Calculating the length L of the soaking zone of the forming annealing device₃：

Wherein, Delta T₃＝T_st-T_aTemperature difference reduction h for annealing zone₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₃For correction factors, the general annealing zone K₃＝1；

Calculating the length L of the soaking zone of the forming annealing device₄：

Wherein，ΔT₄＝T_o-T_stThe temperature difference of the subsequent annealing area is reduced by h₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₄Is a correction factor; since the subsequent annealing zone only increases the temporary stress, the annealing speed can be properly accelerated within the safe stress range to reduce the length of the annealing device, generally the subsequent annealing zone 1<K₄<3.5。

10. The method as claimed in claim 1, wherein in step 4, the total length L of the forming and annealing apparatus is calculated_W：

L_W＝L_δ+L₁+L₂+L₃+L₄；

Wherein L is_δA length of the thickness forming region; l is₁Is the length, L, of the pre-annealing zone₂Length, L, of soaking zone₃The length of the annealing zone; l is₄The length of the subsequent annealing zone.

Technical Field

The invention relates to the field of glass substrate manufacturing, in particular to a design method of an overflow forming annealing device for a glass substrate.

Background

General TFT-LCD (thin film transistor display)) Glass substrates used in the field of flat panel display manufacturing such as PDPs (plasma display panels) and the like are manufactured by overflow down-draw, and in a molding process, molten glass melted in a glass melting furnace is supplied to a fusion overflow down-draw molding apparatus. Control of glass substrate thickness uniformity, residual stress, and warpage is one of the particularly important process technologies, and is related to the design and process control of the overflow forming annealing device. Annealing of glass substrates does not initially result in thermal stress in the article, but rather in a substantial temperature gradient (especially across the sheet glass). The function of the soaking zone is to minimize this temperature gradient. Because the temperature in the soaking zone is higher than the glass transition point temperature T_gThe thermal stress is relaxed quickly, so that the thermal stress caused by the reduction of the temperature gradient in the process of soaking while cooling slowly can be relaxed, and the foundation is laid for further reducing the temperature gradient after the product enters an annealing zone, so that the soaking section in the annealing process does not aim at eliminating the stress, but aims at reducing the temperature gradient to realize soaking.

From alpha-S_iTo P-S_iThe development of (e.g., LTPS) has presented significant challenges to the use of glass substrates. P-S_iCoating requirement ratio alpha-S_iThe process temperature is much higher, about 600-700 ℃. The glass substrate must have good thermal shrinkage (compression) stability at this temperature. Thermal shrinkage (compression) stability is dependent on the intrinsic viscosity temperature characteristics of the glass frit composition (expressed as strain point) and the thermal history of the glass substrate (thermal history). Compression is an important indicator for the end customer. The glass liquid flows through the surface of the overflow brick, and is gathered and bonded into a glass belt at the root parts of the overflow surfaces at the two sides of the overflow brick. The glass ribbon overcomes the internal friction viscous resistance under the action of gravity and traction force, and the thickness is gradually reduced to the thickness of a target product. The pulling rolls are located sufficiently downstream of the apparatus so that the ribbon is cooled and sufficiently rigid as it is drawn. The thickness distribution below the overflow brick tip (root) is strongly related to the cooling speed of the section (about the softening point (lower forming operation limit) to reach the thickness of the target product preliminarily).

The overflow down-drawing method is a comprehensive manufacturing cost reduction method which comprises the steps of improving the productivity and reducing the construction cost of a production line. 1. The drawing speed is increased, and the productivity (extraction amount) is improved; 2. the sheet width is improved, a higher generation overflow forming annealing device is designed, and the production of wide-width, large-capacity and compatible glass substrate products with various thicknesses is realized; 3. shortening the overall length of the production line (e.g., the vertical height of the overflow brick root and the separation of the substrate from the ribbon). Conventional unified scaling up methods can guarantee sufficient time at temperature to achieve the same compression of the final substrate. The drawback is that a longer distance is required between the root of the overflow brick and the location of the separation substrate, which takes up more capital investment.

According to the result of the updated research on the glass thermal history, the glass undergoes the glass states of viscosity (free flow, high viscous plasticity), viscoelasticity (elastoplasticity, elastomer initial state and sub-rigid body) and elasticity (rigid body) according to the cooling curve. Different proportion rules are applied to each glass state section, the distance of a viscous zone is reduced through quick cooling, the time of a vitrification zone and an annealing zone is prolonged through slower cooling, and the interval of an elastic zone is properly reduced, so that the forming device can basically keep the existing physical shell and improve the quality indexes of stress, compression and the like.

The traditional error zone one: by mistake, stress relaxation is regarded as stress disappearance, and by mistake, 10¹²Determining the annealing region 10 by determining the thermal stress due to the exposed structural difference as the whole of the internal stress¹²～10¹⁶Pa·s。

The conventional error zone two: the three stages of "melt viscous plastomer elastomer" do not fully reveal the mechanism of the annealing stage; the glass annealing mechanism cannot be accurately analyzed by using the temperature difference, stress relaxation and internal stress.

In order to overcome the miszone of the traditional theory, the novel design concept of the glass annealing furnace is annealing, explosion prevention, high-efficiency cooling, environmental interference reduction and high-level transverse temperature control, and the glass cooling speed is carried out by the procedure of slowest, slow, fast and faster. The invention obtains the technical route of the glass annealing furnace design from six physical characteristic stages, two annealing stages and four annealing states, and analyzes the glass annealing mechanism by using a 'temperature difference, structure difference and thermal stress' deduction. The theory of glass annealing can be established based on the assumptions of the six physical property phases and the guidance of the lehr design and annealing operation, in combination with the use of the plane stress concept, the causes of glass ribbon warpage, explosion and cutting obstruction can be analyzed. Discussion the glass annealing furnace must strictly distinguish between the irreversible structural difference and the reversible structural difference, the annealing stage and the subsequent annealing stage, the theoretical value and the actual value of the glass annealing starting point viscosity, the temper proof annealing and the non-deforming annealing, the best, the second annealing state and the subsequent annealing state, the stress relaxation phenomenon in a narrow sense and the stress relaxation phenomenon in a broad sense by taking the viscosity (temperature cannot be used only) as the dimension of the physical characteristics.

Disclosure of Invention

Aiming at the problem that the design of a glass annealing furnace in the prior art has a miszone in the traditional theory, the invention provides a design method of a glass substrate overflow forming annealing device, which overcomes the miszone of the traditional theory, realizes annealing with more accurate, more efficient and lower cost in the overflow method forming, is particularly suitable for the fine design of a large-capacity (output), wide-breadth and thin glass substrate forming annealing device, and is also suitable for the fine design of the LTPS glass substrate forming annealing device on the performance.

The invention is realized by the following technical scheme:

a design method of a glass substrate overflow forming annealing device comprises the following steps:

step 1, determining parameters of substrate glass in a forming annealing device through production line design;

step 2, determining the temperature T of the overflow brick tip according to the viscosity-temperature characteristic curve of the glass substrate material square_iTheoretical annealing starting point temperature T of glass substrate_TExpansion softening point temperature T_dActual annealing starting point temperature T_aStrain point temperature T_stAnnealing furnace exit temperature T_o；

Step 3, dividing the forming annealing device into different functional sections according to the thermodynamic and kinetic characteristics of the glass, wherein the functional sections comprise a thickness forming zone, a pre-annealing zone, a soaking zone, an annealing zone and a subsequent annealing zone;

step 4, calculating the annealing speed h of the glass substrate according to different functional sections₀Glass substratePulling speed PR and length L of thickness forming zone in forming annealing apparatus_δLength L of the pre-annealing zone₁Length L of soaking zone₂Length L of the annealing zone₃And the length L of the subsequent annealing zone₄And total length L of the forming and annealing device_W。

Preferably, the parameters of the substrate glass determined by the production line design in step 1 include the draw-out amount Q of the substrate glass on the production line, the average draw width L of the glass substrate, the product width W of the glass substrate, and the target thickness δ of the glass substrate.

Preferably, the temperature T of the overflow brick tip in the step 2_iSetting the corresponding viscosity eta_iTheoretical annealing starting point temperature T of glass substrate_TSetting the corresponding viscosity eta_T＝10⁸Pa.s, expansion softening point temperature T_dSetting the corresponding viscosity eta_d＝10¹¹Pa s, actual annealing starting point temperature T_aSetting the corresponding viscosity eta_a＝10¹²Pa · s, temperature T at which strain point is the lower limit of annealing_stSetting the corresponding viscosity eta_st＝10^13.5Pa.s, annealing furnace exit temperature T_o(ii) a Wherein, the temperature T of the overflow brick tip_iCorresponding viscosity η_i＝10^3.8Pa·s～10^4.2Pa · s; annealing furnace exit temperature T_o＝300℃～500℃。

Preferably, in step 3, the temperature range of the thickness forming zone in the different functional sections of the profile annealing furnace device is T_i～T_TThe temperature interval of the pre-annealing area is T_T～T_dThe temperature interval of the soaking zone is T_d～T_aThe temperature interval of the annealing zone is T_a～T_stAnd the temperature interval of the subsequent annealing zone is T_st～T_o。

Furthermore, the temperature drop delta T of the thickness forming region in different functional sections of the forming annealing furnace device_δ＝T_T-T_iTemperature drop difference Δ T of pre-annealing zone₁＝T_d-T_TTemperature drop difference of soaking zone delta T₂＝T_a-T_dTemperature drop difference Δ T of annealing zone₃＝T_st-T_aTemperature drop difference delta T of subsequent annealing zone₄＝T_o-T_st。

Preferably, in step 4, the annealing speed h of the glass substrate₀The calculation method comprises the following steps:

l1 calculating the structural stress σ of the glass substrate_s：

Wherein alpha is_UTemperature at expansion softening point T_dLinear coefficient of thermal expansion of alpha_gTo glass transition point temperature T_gThe coefficient of linear thermal expansion of (a),is the thermal conductivity coefficient, lambda is the thermal conductivity coefficient of the glass substrate, rho is the density of the glass substrate, C_pThe specific heat capacity of the glass substrate is shown, and mu is the Poisson ratio; e is Young's modulus; h is₀The annealing speed of the glass substrate is delta, the target thickness of the glass substrate is delta, and psi s is a residual structural stress growth coefficient when relaxation factors are considered; wherein the physical parameters are lambda, rho and C_pThe temperatures corresponding to μ and E are strain point temperatures T_st；

L2, coefficient of increase of residual structural stress psi when calculating relaxation factors_s；

Wherein h is₀Is the annealing speed of the glass substrate;

l3, calculating the stress σ of the glass substrate due to the reverse temperature difference_T；

Wherein alpha is the linear thermal expansion coefficient of the glass substrate,is the thermal conductivity coefficient, lambda is the thermal conductivity coefficient of the glass substrate, rho is the density of the glass substrate, C_pThe specific heat capacity of the glass substrate is shown, and mu is the Poisson ratio; e is Young's modulus; h is₀The cooling rate of the glass substrate is determined, delta is the target thickness of the glass substrate, alpha_TThe scale factor of the unrelaxed part in the relaxation factor of the temperature difference stress under the dynamic temperature condition; physical property parameters of lambda, rho and C_pThe temperatures corresponding to μ and E are strain point temperatures T_st(ii) a When overflow forming is directly annealed, alpha_T＝0；

L4, calculating the allowable stress delta n of the glass substrate with the thickness delta;

Δn＝B×(σ_T+σ_s)；

wherein, Delta n is the allowable stress of the glass substrate with the thickness of Delta, and B is the photoelastic coefficient of the glass substrate; sigma_sStructural stress of the glass substrate; sigma_TIs the reverse temperature differential stress of the glass substrate;

l5, the annealing rate h of the glass substrate was obtained by combining the calculation formulas of L1, L2, L3 and L4₀。

Preferably, in the step 4, calculating the drawing speed PR of the glass substrate of the forming and annealing device;

wherein Q is the extraction amount of the substrate glass in a production line, L is the average extraction width of the glass substrate, rho is the density of the glass substrate, and delta is the target thickness of the glass substrate.

Preferably, in step 4, the forming annealing device thickness forming region length L_δThe calculation method comprises the following steps:

s1, calculating the traction force F of the traction roller_PR；

Wherein: t is_PFor torque of the pulling rolls, I_PThe polar moment of inertia of the drawing roll, D the diameter of the drawing roll and delta the target thickness of the glass substrate;

s2, calculating the length L of the thickness forming area of the forming annealing device_δ

Wherein eta is_iThe viscosity of the root of the overflow brick tip, Q the extraction amount of the substrate glass in a production line, L the average extraction width of the glass substrate, d the thickness of the glass belt leaving the root of the overflow brick, and F_PRIs the pulling roll pulling force, delta is the target thickness of the glass substrate;

s3, calculating the thickness d of the glass ribbon leaving the root of the overflow brick;

wherein, η i is the viscosity of the overflow brick tip (root), Q is the glass extraction amount of the design production line, L is the average extraction width of the glass substrate, ρ is the density of the glass substrate, g is the gravity acceleration, and ε is an empirical coefficient, and ε is 0.5-0.8.

Preferably, in step 4, the length L of the pre-annealing zone of the forming and annealing device is calculated₁Length L of soaking zone₂Length L of the annealing zone₃And the length L of the subsequent annealing zone₄；

Calculating the length L of the pre-annealing area of the forming annealing device₁：

Wherein, Delta T₁＝T_d-T_TThe temperature difference is reduced in the pre-annealing region, h₀Is the annealing speed of the glass substrate, PR is the pulling speed of the glass substrate, K₁For correction factors, the pre-annealing zone K₁＝1；

Calculating the length L of the soaking zone of the forming annealing device₂：

Wherein, Delta T₂＝T_a-T_d＝T_g-T_dThe temperature difference is reduced in the soaking zone h₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₁For correction factors, general soaking zone K₂＝1；

Calculating the length L of the soaking zone of the forming annealing device₃：

Wherein, Delta T₃＝T_st-T_aTemperature difference reduction h for annealing zone₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₃For correction factors, the general annealing zone K₃＝1；

Calculating the length L of the soaking zone of the forming annealing device₄：

Wherein, Delta T₄＝T_o-T_stThe temperature difference of the subsequent annealing area is reduced by h₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₄Is a correction factor; because the subsequent annealing area only increases temporary stress, the annealing speed can be properly accelerated within the safe stress range to reduce the length of the annealing device, and the subsequent annealing area is 1 < K₄＜3.5。

Preferably, in step 4, the total length L of the forming and annealing device is calculated_W：

L_W＝L_δ+L₁+L₂+L₃+L₄；

Wherein L is_δA length of the thickness forming region; l is₁Is the length, L, of the pre-annealing zone₂Length, L, of soaking zone₃The length of the annealing zone; l is₄The length of the subsequent annealing zone.

Compared with the prior art, the invention has the following beneficial technical effects:

the invention provides a design method of a glass substrate overflow forming annealing device, which divides the annealing of a glass substrate into six basic fluid characteristics: free flowing melts, high viscous plastomers, elastoplastomers, elastomer initial state, transition to full elastomers and full elastomers, and the like; the continuous gradual change law of the physical characteristics of the glass is the only basis of the annealing theory when the glass is cooled from a molten state to a normal temperature, the law of the traditional theory 'melt, viscous plastomer and elastomer' is not completely revealed, the annealing mechanism of the glass is more completely analyzed by using the deduction of 'temperature difference, structure difference and thermal stress', the parameters of the substrate glass in a forming and annealing device are determined through the design of a production line, the temperature parameters determined according to the viscosity-temperature characteristic curve of the glass substrate material are respectively divided into different sections, and the annealing speed h of the glass substrate is calculated according to the different sections₀Glass substrate pulling speed PR and length L of thickness forming area in forming annealing device_δLength L of the pre-annealing zone₁Length L of soaking zone₂Length L of the annealing zone₃And the length L of the subsequent annealing zone₄And total length L of the forming and annealing device_WThe design method overcomes the error of the traditional theory and realizes the design of the overflow forming annealing device with more accuracy, higher efficiency and lower cost.

Drawings

FIG. 1 is a schematic diagram of the overflow system of the present invention;

FIG. 2 is a schematic diagram of an overflow downdraw structure of the present invention;

FIG. 3 is a residual structural stress growth factor in accordance with the present invention;

FIG. 4 is a schematic view of the design of the forming lehr of the present invention.

In the figure: 1-overflow brick; 2-an overflow trough; 3-molten glass feeding device; 4-the root of the overflow brick; 5-forming the glass substrate; 6-glass substrate pull-down direction; w-glass substrate width; l-glass substrate tab width.

Detailed Description

The present invention will now be described in further detail with reference to specific examples, which are intended to be illustrative, but not limiting, of the invention.

According to the figure 1, the overflow system is composed of an overflow brick 1 and a molten glass feeding device 3 which are connected. An overflow groove 2 is formed in the overflow brick 1, and the bottom of the overflow brick 1 is an overflow brick root 4; in the case where a glass substrate is produced by a fusion overflow method, in a molding step, molten glass melted in a glass melting furnace is supplied to a molten glass supply device 3 in a fusion overflow molding device, and overflows along an overflow groove 2 through both sides of an overflow brick 1, thereby forming a glass substrate from a position below an overflow brick root 4.

According to fig. 2, the tab serves as a basis for forming a glass substrate, and during the glass substrate downdraw forming process, a formed glass substrate 5 travels downward in a glass substrate downdraw direction 6. In the figure, W is the width of the glass substrate, and L is the lead width of the glass substrate.

As shown in fig. 3, the increase coefficient psi of the residual structural stress is taken into account_sThe cooling rate. In general case psi_sCan be expressed as follows:

wherein, T_g≈T_aIs approximate to the actual annealing starting point T for the glass transition point temperature_aAnnealing upper limit temperature versus viscosity η_a＝10¹²Pa · s. In the usual continuous cooling, the temperature differential stress and the structural stress anneal to the lower limit temperature T towards the strain point_stCorresponding viscosity eta_st＝10^13.5Pa · s is no longer changed, at which point psi_sA maximum is reached, i.e.:

ψ_shas the following characteristics: (1) psi_sIs a function of temperature; (2) psi_sDecreases with decreasing cooling speed h, when h → 0_s→ 0. When h is approximately equal to 0.1 ℃/min, psi_sAlready close to 0; (3) psi_sIncreasing with h and approaching 1. When h is more than 100 ℃/min,. psi_sAlready close to 1.

The invention provides a design method of a glass substrate overflow forming annealing device, which comprises the following steps:

step 1, determining parameters of substrate glass in a forming annealing device through production line design;

step 2, determining the temperature T of the overflow brick tip according to the viscosity-temperature characteristic curve of the glass substrate material square_iTheoretical annealing starting point temperature T of glass substrate_TExpansion softening point temperature T_dActual annealing starting point temperature T_aStrain point temperature T_stAnnealing furnace exit temperature T_o；

Step 3, dividing the forming annealing device into different functional sections according to the thermodynamic and kinetic characteristics of the glass, wherein the functional sections comprise a thickness forming zone, a pre-annealing zone, a soaking zone, an annealing zone and a subsequent annealing zone;

step 4, calculating the annealing speed h of the glass substrate according to different functional sections₀Glass substrate pulling speed PR and length L of thickness forming area in forming annealing device_δLength L of the pre-annealing zone₁Length L of soaking zone₂Length L of the annealing zone₃And the length L of the subsequent annealing zone₄And total length L of the forming and annealing device_W。

In the step 1, the parameters of the substrate glass determined by the production line design comprise the extraction amount Q of the substrate glass on the production line, the average extraction width L of the glass substrate, the product width W of the glass substrate and the target thickness delta of the glass substrate.

Temperature T of overflow brick tip in step 2_iSetting the corresponding viscosity eta_iTheoretical annealing starting point temperature T of glass substrate_TSetting the corresponding viscosity eta_T＝10⁸Pa.s, expansion softening point temperature T_dSetting the corresponding viscosity eta_d＝10¹¹Pa s, actual annealing starting point temperature T_aSetting the corresponding viscosity eta_a＝10¹²Pa · s, temperature T at which strain point is the lower limit of annealing_stSetting the corresponding viscosity eta_st＝10^13.5Pa.s, annealing furnace exit temperature T_o(ii) a Wherein, the temperature T of the overflow brick tip_iCorresponding viscosity η_i＝10^3.8Pa·s～10^4.2Pa · s; temperature T of overflow brick tip_iThe corresponding viscosity is preferably η_i＝10⁴Pa · s; annealing furnace exit temperature T_o300-500 deg.c; annealing furnace outlet temperature optimization T of the invention_o＝400℃。

In step 3, the temperature interval of the thickness forming area in different functional sections of the forming annealing furnace device is T_i～T_TThe temperature interval of the pre-annealing area is T_T～T_dThe temperature interval of the soaking zone is T_d～T_aThe temperature interval of the annealing zone is T_a～T_stAnd the temperature interval of the subsequent annealing zone is T_st～T_oWherein the difference in temperature of the thickness-forming zone Δ T in the different functional sections of the profile annealing furnace device_δ＝T_T-T_iTemperature drop difference Δ T of pre-annealing zone₁＝T_d-T_TTemperature drop difference of soaking zone delta T₂＝T_a-T_dTemperature drop difference Δ T of annealing zone₃＝T_st-T_aTemperature drop difference delta T of subsequent annealing zone₄＝T_o-T_stAs shown in fig. 4.

In step 4, the annealing speed h of the glass substrate₀The calculation method comprises the following steps:

l1 calculating the structural stress σ of the glass substrate_s：

Wherein alpha is_UTemperature at expansion softening point T_dLinear coefficient of thermal expansion of alpha_gTo the glass transition pointTemperature T_gThe coefficient of linear thermal expansion of (a),is the thermal conductivity coefficient, lambda is the thermal conductivity coefficient of the glass substrate, rho is the density of the glass substrate, C_pThe specific heat capacity of the glass substrate is shown, and mu is the Poisson ratio; e is Young's modulus; h is₀Is the annealing speed of the glass substrate, delta is the target thickness of the glass substrate,. phi_sThe stress growth coefficient of the residual structure is considered when the relaxation factor is considered; wherein the physical parameters are lambda, rho and C_pThe temperatures corresponding to μ and E are strain point temperatures T_st；

L2, coefficient of increase of residual structural stress psi when calculating relaxation factors_s；

Wherein h is₀Is the annealing speed of the glass substrate;

l3, calculating the stress σ of the glass substrate due to the reverse temperature difference_T；

Wherein alpha is the linear thermal expansion coefficient of the glass substrate,is the thermal conductivity coefficient, lambda is the thermal conductivity coefficient of the glass substrate, rho is the density of the glass substrate, C_pThe specific heat capacity of the glass substrate is shown, and mu is the Poisson ratio; e is Young's modulus; h is₀The cooling rate of the glass substrate is determined, delta is the target thickness of the glass substrate, alpha_TThe scale factor of the unrelaxed part in the relaxation factor of the temperature difference stress under the dynamic temperature condition; physical property parameters of lambda, rho and C_pThe temperatures corresponding to μ and E are strain point temperatures T_st(ii) a When overflow forming is directly annealed, alpha_T＝0；

L4, calculating the allowable stress delta n of the glass substrate with the thickness delta;

Δn＝B×(σ_T+σ_s)；

wherein, Delta n is the allowable stress of the glass substrate with the thickness of Delta, and B is the photoelastic coefficient of the glass substrate; sigma_sStructural stress of the glass substrate; sigma_TIs the reverse temperature differential stress of the glass substrate;

l5, the annealing rate h of the glass substrate was obtained by combining the calculation formulas of L1, L2, L3 and L4₀。

In the step 4, calculating the drawing speed PR of the glass substrate of the forming annealing device;

wherein Q is the extraction amount of the substrate glass in a production line, L is the average extraction width of the glass substrate, rho is the density of the glass substrate, and delta is the target thickness of the glass substrate.

In step 4, the forming annealing device thickness forming region length L_δThe calculation method comprises the following steps:

s1, calculating the traction force F of the traction roller_PR；

Wherein: t is_PFor torque of the pulling rolls, I_PThe polar moment of inertia of the drawing roll, D the diameter of the drawing roll and delta the target thickness of the glass substrate;

s2, calculating the length L of the thickness forming area of the forming annealing device_δ

Wherein eta is_iThe viscosity of the root of the overflow brick tip, Q the extraction amount of the substrate glass in a production line, L the average extraction width of the glass substrate, d the thickness of the glass belt leaving the root of the overflow brick, and F_PRFor pulling by a pull rollAn attractive force, δ being a target thickness of the glass substrate;

s3, calculating the thickness d of the glass ribbon leaving the root of the overflow brick;

wherein eta is_iThe viscosity of the overflow brick tip (root), Q the glass extraction amount of a design production line, L the average extraction width of a glass substrate, rho the density of the glass substrate, g the gravity acceleration, epsilon the empirical coefficient, and epsilon 0.5-0.8, wherein epsilon is 0.65.

In step 4, calculating the length L of the pre-annealing area of the forming annealing device₁A soaking zone L₂Annealing region L₃And a subsequent annealing zone L₄；

Calculating the length L of the pre-annealing area of the forming annealing device₁：

Wherein, Delta T₁＝T_d-T_TThe temperature difference is reduced in the pre-annealing region, h₀Is the annealing speed of the glass substrate, PR is the pulling speed of the glass substrate, K₁For correction factors, the pre-annealing zone K₁＝1；

Calculating the length L of the soaking zone of the forming annealing device₂：

Wherein, Delta T₂＝T_a-T_d＝T_g-T_dTemperature drop difference of soaking zone (glass transition zone), h₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₁For correction factors, general soaking zone K₂＝1；

Calculating the length L of the soaking zone of the forming annealing device₃：

Wherein, Delta T₃＝T_st-T_aTemperature difference reduction h for annealing zone₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₃For correction factors, the general annealing zone K₃＝1；

Calculating the length L of the soaking zone of the forming annealing device₄：

Wherein, Delta T₄＝T_o-T_stThe temperature difference of the subsequent annealing area is reduced by h₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₄Is a correction factor; because the subsequent annealing area only increases temporary stress, the annealing speed can be properly accelerated within the safe stress range to reduce the length of the annealing device, and the subsequent annealing area is 1 < K₄< 3.5, K in the present invention₄＝2.5。

In step 4, calculating the total length L of the forming annealing device_W：

L_W＝L_δ+L₁+L₂+L₃+L₄；

Wherein L is_δA length of the thickness forming region; l is₁Is the length, L, of the pre-annealing zone₂Length, L, of soaking zone₃The length of the annealing zone; l is₄The length of the subsequent annealing zone.

Annealing stage (10)⁸～10^13.5Pa · s) irreversible structural differences caused by temperature differences (a) are dependent on the viscosity, the time elapsed and the magnitude of the temperature difference; the structural difference (b) reduced by the structural adjustment of the positive displacement is related to the viscosity and the elapsed time, and is not related to the size of the temperature difference; the remaining structural difference (c) is dependent only on the viscosity and on the time elapsed, the magnitude of the temperature difference and whether it is a "positive displacement" or a "disorientation"(non-uniform temperature field) is irrelevant, and viscosity determines whether the remaining structural differences are partly or wholly implied.

Revealing (measurable) structural differences (residual structural differences) (a-b-c), the corresponding stresses including differential temperature stress (due to the temperature difference) and differential expansion stress (due to the differential expansion). The viscosity difference, the expansion difference and the density difference are generated by the temperature difference, and the stress corresponding to the irreversible structural difference (a) generated by reflecting the structural adjustment comprises temperature difference stress (caused by the temperature difference) and expansion difference stress (caused by the expansion difference). Along with the sharp increase of viscosity, the heat conductivity coefficient is slightly reduced along with the temperature drop, so that the temperature difference stress is correspondingly increased, and even if the cooling speed is unchanged, the irreversible structure difference is not reduced or increased. The structural difference of the reduction of the structural adjustment by the displacement of the structural groups or molecules (b) sharply decreases the displacement activity with a sharp increase in viscosity, so that the structural difference is markedly reduced. The structural differences (residual structural differences) (c) implied (not detectable) by differential deformation, unlike structural adjustments, cannot be reduced at all, but are only temporarily implied. The differential deformation activity decreases sharply with a sharp increase in viscosity, so that the structural difference decreases markedly.

According to a new theoretical research result, glass substrate annealing is divided into six basic fluid characteristics:

1. free-flowing melt phase, viscosity range: 10^0.8829～10⁴Pa · s. Melting overflow area corresponding to melting overflow down-draw method: from melting, clarification, homogenization to the overflow brick tip (root). Thermodynamic and kinetic characteristics: free flowing, 10^0.8829Pa · s is the melt viscosity of the glass; 10⁴Pas is the viscosity of the glass melt near the overflow brick tip.

2. High viscosity plastomer stage, viscosity range: 10⁴～10⁸Pa · s. Thickness forming region corresponding to the melt overflow down-draw method: from the overflow brick tip (root) through the thickness zone to the theoretical annealing point. Thermodynamic and kinetic characteristics: the displacement activity is very big, and the structure adjustment is fast going on. 10⁴Pa · s is the viscosity of the glass melt near the overflow brick tip; 10⁸Pas is the viscosity at the starting point of theoretical annealing of the glass, the relaxation time τ₀Starting from 0 to τ₀> 0 (approximate number)Seconds). No structural difference is generated although the temperature difference exists, and no stress field exists in the glass.

3. Elastoplastomer stage, viscosity range: 10⁸～10¹¹Pa · s (annealing against deformation, optimal annealing regime). Corresponding to a pre-annealing area of a fusion overflow downdraw method: from the theoretical annealing point to the expansion softening point (deformation point). Thermodynamic and kinetic characteristics: structural group displacement and molecular displacement. The narrowly defined stress relaxation phenomenon is a typical feature of this stage, the structural difference b with reduced structural adjustment plus the implicit structural difference c is equal to the structural difference a caused by the temperature difference, and the revealed structural difference is 0, i.e. the complete stress dissipation effect.

4. Elastomer initial stage, viscosity range: 10¹¹～10¹²Pa · s (temper proof annealing, sub-optimal annealing state). Soaking (GTTR: glass transition) zone for the down-draw of the melt overflow: from the expansion softening point (deformation point) to the actual annealing point. Thermodynamic and kinetic characteristics: the displacement of the structural groups tends towards molecular displacement. The sharp increase in viscosity sharply reduces the displacement activity and the differential deformation activity. Because the heat conductivity coefficient is slightly reduced along with the temperature drop, the temperature difference is correspondingly increased, and even if the cooling speed is not changed, a is not reduced or increased. About 10¹²Pa · s, the proportion of exposed thermal stress can already be measured for the remaining structure, except partially hidden. The narrow stress relaxation phenomenon is finally replaced by the generalized stress relaxation phenomenon, and the internal stress is semi-implicit and semi-obvious, namely, the incomplete stress dissipation effect.

5. Transition to a fully elastomeric (sub-rigid) stage, viscosity range: 10¹²～10^13.5Pa · s (non-deformation annealed, most annealed state). The stress control area corresponding to the fusion overflow downdraw method: the actual anneal upper limit is to the theoretical anneal lower limit. Thermodynamic and kinetic characteristics: and (4) molecular displacement. The displacement and differential deformation tend to collapse as the viscosity further steepens, with b ≈ 0 and c ≈ 0. Although the degree to which stress is proportional to strain and follows Hooke's Law has not been reached, it has exhibited the characteristics of a hyporigid body.

6. Fully elastomeric (rigid) stage, viscosity range: 10^13.5Pa · s (subsequent annealing). Corresponding to a subsequent annealing area of a melting overflow down-drawing method: theoretical annealingLower limit via actual annealing lower limit 10^17.5Pa-s to below room temperature. Thermodynamic and kinetic characteristics: the mass point vibrates. Viscosity of 10^13.5Pa.s, b is 0 and c is 0, i.e. the generalized stress relaxation phenomenon annihilates, with stress proportional to strain and following hooke's law. The structural differences are all exposed until the temperature is uniform, and the structural differences are not changed and are permanent stress. Viscosity greater than 10^13.5Pa.s, the temperature difference only produces reversible structural differences, which are completely exposed because no differential deformation has occurred, and the resulting thermal stress, which disappears with temperature uniformity, is called temporary stress. Before the temporary stress disappears, it is superimposed on the permanent stress at the vector coincidence. Spalling occurs when the individual or additive stresses exceed the tensile strength of the glass.

The continuous gradual change rule of the physical characteristics of the glass is the only basis of the annealing theory when the glass is cooled from a molten state to a normal temperature. The conventional theory "melt (viscosity) · viscous plastomer (viscoelasticity) · elastomer" does not fully reveal its rule. The updated research shows that the glass undergoes the glass states of viscosity (free flow, high viscous plasticity), viscoelasticity (elastoplasticity, elastomer initial state, sub-rigid body) and elasticity (rigid body) according to the cooling curve, and the glass annealing mechanism is analyzed by the deduction of 'temperature difference, structure difference and thermal stress'.

According to the most recent theoretical research results, the annealing phase consists of a deformation-proof annealing (. eta.)_T～η_PPa · s) and non-deforming annealing (. eta.)_P～10^13.5Pa · s) in two small stages. According to the annealing efficiency, 3 annealing states are distinguished, which correspond to 3 physical characteristic stages respectively. Eta_T＝10⁸Pa · s is the theoretical annealing onset viscosity, η_P≈10¹²Pa · s is the actual annealing initiation viscosity.

The following examples illustrate the design method of the glass substrate overflow forming annealing device of the present invention, including the following steps:

firstly, the average lead width L of the glass substrate is calculated by the formula (3), that is:

L＝a×W；

wherein a is a lead plate coefficient, a is more than or equal to 1.20 and less than or equal to 1.25, and W is the width of the glass substrate product. The upper limit value is generally the best value in production design, namely alpha is 1.25.

Secondly, calculating the annealing rate h of the forming annealing device₀

Annealing speed h of glass substrate₀The calculation method comprises the following steps:

l1 calculating the structural stress σ of the glass substrate_s：

Wherein alpha is_UTemperature at expansion softening point T_dLinear coefficient of thermal expansion of alpha_gTo glass transition point temperature T_gThe coefficient of linear thermal expansion of (a),is the thermal conductivity coefficient, lambda is the thermal conductivity coefficient of the glass substrate, rho is the density of the glass substrate, C_pThe specific heat capacity of the glass substrate is shown, and mu is the Poisson ratio; e is Young's modulus; h is₀Is the annealing speed of the glass substrate, delta is the target thickness of the glass substrate,. phi_sThe stress growth coefficient of the residual structure is considered when the relaxation factor is considered; wherein the physical parameters are lambda, rho and C_pThe temperatures corresponding to μ and E are strain point temperatures T_st；

L2, coefficient of increase of residual structural stress psi when calculating relaxation factors_s；

Wherein h is₀Is the annealing speed of the glass substrate;

l3, calculating the stress σ of the glass substrate due to the reverse temperature difference_T；

Wherein alpha is the linear thermal expansion coefficient of the glass substrate,is the thermal conductivity coefficient, lambda is the thermal conductivity coefficient of the glass substrate, rho is the density of the glass substrate, C_pThe specific heat capacity of the glass substrate is shown, and mu is the Poisson ratio; e is Young's modulus; h is₀The cooling rate of the glass substrate is determined, delta is the target thickness of the glass substrate, alpha_TThe scale factor of the unrelaxed part in the relaxation factor of the temperature difference stress under the dynamic temperature condition; physical property parameters of lambda, rho and C_pThe temperatures corresponding to μ and E are strain point temperatures T_st(ii) a When overflow forming is directly annealed, alpha_T＝0；

L4, calculating the allowable stress delta n of the glass substrate with the thickness delta;

Δn＝B×(σ_T+σ_s)；

wherein, Delta n is the allowable stress of the glass substrate with the thickness of Delta, and B is the photoelastic coefficient of the glass substrate; sigma_sStructural stress of the glass substrate; sigma_TIs the reverse temperature differential stress of the glass substrate;

l5, the annealing rate h of the glass substrate was obtained by combining the calculation formulas of L1, L2, L3 and L4₀。

Thirdly, calculating the traction speed PR of the glass substrate of the forming annealing device;

wherein Q is the extraction amount of the substrate glass in a production line, L is the average extraction width of the glass substrate, rho is the density of the glass substrate, and delta is the target thickness of the glass substrate.

Fourthly, forming the thickness forming area length L of the annealing device_δThe calculation method comprises the following steps:

s1, calculating the traction force F of the traction roller_PR；

Wherein: t is_PFor torque of the pulling rolls, I_PThe polar moment of inertia of the drawing roll, D the diameter of the drawing roll and delta the target thickness of the glass substrate;

s2, calculating the length L of the thickness forming area of the forming annealing device_δ

Wherein eta is_iThe viscosity of the root of the overflow brick tip, Q the extraction amount of the substrate glass in a production line, L the average extraction width of the glass substrate, d the thickness of the glass belt leaving the root of the overflow brick, and F_PRIs the pulling roll pulling force, delta is the target thickness of the glass substrate;

s3, calculating the thickness d of the glass ribbon leaving the root of the overflow brick;

wherein eta is_iThe viscosity of the overflow brick tip (root), Q the glass extraction amount of a design production line, L the average extraction width of a glass substrate, rho the density of the glass substrate, g the gravity acceleration, epsilon the empirical coefficient, and epsilon being 0.5-0.8.

Fifthly, calculating the length of each section of the annealing area

Determining the temperature T of the overflow brick tip according to the viscosity-temperature characteristic curve of the glass substrate material_i(corresponding viscosity. eta.)_i) Theoretical annealing starting point temperature T of glass substrate_T(corresponding viscosity. eta.)_T＝10⁸Pa · s), expansion softening point temperature T_d(corresponding viscosity. eta.)_d＝10¹¹Pa · s), actual annealing start point temperature T_a(corresponding viscosity. eta.)_a＝10¹²Pas), strain point (annealing lower limit) temperature T_st(corresponding viscosity. eta.)_st1013.5Pa · s), the annealing furnace exit temperature To;

temperature zones of the thickness forming zone in different functional sections of the forming lehr arrangement depending on the thermodynamic and kinetic characteristics of the glassIs at interval of T_i～T_TThe temperature interval of the pre-annealing area is T_T～T_dThe temperature interval of the soaking zone is T_d～T_aThe temperature interval of the annealing zone is T_a～T_stAnd the temperature interval of the subsequent annealing zone is T_st～T_o；

Temperature T of overflow brick tip in design_iCorresponding viscosity η_i＝10^3.8Pa·s～10^4.2Pa · s; annealing furnace exit temperature T_o300 ℃ to 500 ℃. Temperature drop difference Δ T of thickness forming region_δ＝T_T-T_iTemperature drop difference Δ T of pre-annealing zone₁＝T_d-T_TTemperature drop difference of soaking zone delta T₂＝T_a-T_dTemperature drop difference Δ T of annealing zone₃＝T_st-T_aTemperature drop difference delta T of subsequent annealing zone₄＝T_o-T_st。

Calculating the length L of the pre-annealing area of the forming annealing device₁Length L of soaking zone₂Length L of the annealing zone₃And the length L of the subsequent annealing zone₄；

Calculating the length L of the pre-annealing area of the forming annealing device₁：

Wherein, Delta T₁＝T_d-T_TThe temperature difference is reduced in the pre-annealing region, h₀Is the annealing speed of the glass substrate, PR is the pulling speed of the glass substrate, K₁For correction factors, the pre-annealing zone K₁＝1～2.5；

Calculating the length L of the soaking zone of the forming annealing device₂：

Wherein, Delta T₂＝T_a-T_d＝T_g-T_dIs a uniform heating zone (vitrification conversion)Variable area) of temperature drop, h₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₁For correction factors, general soaking zone K₂＝1；

Calculating the length L of the soaking zone of the forming annealing device₃：

Wherein, Delta T₃＝T_st-T_aTemperature difference reduction h for annealing zone₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₃For correction factors, the general annealing zone K₃＝1；

Calculating the length L of the soaking zone of the forming annealing device₄：

Wherein, Delta T₄＝T_o-T_stThe temperature difference of the subsequent annealing area is reduced by h₀The cooling rate of the glass substrate, PR is the pulling speed of the glass substrate, K₄Is a correction factor; because the subsequent annealing area only increases temporary stress, the annealing speed can be properly accelerated within the safe stress range to reduce the length of the annealing device, and the subsequent annealing area is 1 < K₄＜3.5。

Moving glass ribbon from temperature T_iCooling to T_TRate of thermal energy loss Q_H(unit: J/S ═ W) is:

Q_H＝Q×C_p×(T_i-T_T)＝Q×C_p×ΔT；

wherein Q is the lead-out quantity of the substrate glass on a production line; c_pIs the specific heat capacity of the glass; t is_iThe temperature of the overflow brick tip; t is_TIs the theoretical annealing starting point temperature of the glass substrate; delta T_δ＝T_T-T_iThickness forming region L_δThe temperature drop difference is small;

average heat fluxComprises the following steps:

wherein W is the width of the glass substrate; l is_δIs the length of the glass ribbon thickness forming region; q is the leading-out quantity of the substrate glass on a production line; c_pIs the specific heat capacity of the glass; t is_iThe temperature of the overflow brick tip; t is_TIs the theoretical annealing starting point temperature of the glass substrate; delta T_δ＝T_T-T_iThickness forming region L_δThe temperature drop of (2).

Rate of heat loss Q of cooling of glass ribbon in other functional zones_HAnd average heat fluxCalculation method and the above-mentioned heat energy loss rate Q_HAnd average heat fluxThe calculation method of (2) is similar.

The invention provides a design method of a glass substrate overflow forming annealing device, which divides the annealing of a glass substrate into six basic fluid characteristics: free flowing melts, high viscosity plastomers, elastoplastomers, elastomer precursors, transitions to full elastomers (sub-rigid) and full elastomers (rigid), and the like. The continuous gradual change rule of the physical characteristics of the glass is the only basis of the annealing theory when the glass is cooled from a molten state to a normal temperature. The traditional theory of 'melt (viscosity) & viscous plastomer (viscoelasticity) & elastomer' does not completely reveal the rule, and the theory of 'temperature difference, structure difference and thermal stress' is used for analyzing the glass annealing mechanism to be more complete. According to the most recent theoretical research results, the annealing phase consists of a deformation-proof annealing (. eta.)_T～η_PPa · s) and non-deforming annealing (. eta.)_P～10^13.5Pa · s) in two small stages. According to the annealing efficiency, 3 annealing states are distinguished, respectively corresponding to 3The physical property phases correspond. Eta_T＝10⁸Pa · s is the theoretical annealing onset viscosity, η_P≈10¹²Pa · s is the actual annealing initiation viscosity. Based on the theoretical basis, the invention applies the latest research result, overcomes the error zone of the traditional theory, and realizes the design of the overflow forming annealing device with more accuracy, higher efficiency and lower cost.