3.1 SFT results
The difference between the vertical displacement of the four monitoring points 1#, 2#, 3#, and 4# on the chamber roof is almost nonexistent, so the average value of the vertical displacement Ds is taken to replace the displacement of those four points. The fluctuation of the vertical displacement of each scheme at 10%X is investigated using error bars, and Fig. 5 depicts the results.
Figure 5(a) illustrates a negative connection between Co and Ds. The impact process can be broken down into 3 stages. The shear failure region (Co<5 MPa) is the first stage, which can be produced by low ore strength or external stresses loads, the vertical displacement of the roof is close to or even more than 30 mm, and the possibility of failure is very high (Chen et al. 2016), as shown in Fig. 6(a) (Co=2 MPa), the entire pillar is in shear failure, the roof and both sides of the chamber are subjected to a large shear force, the pillar undergoing compression deformation under the external loads, and the side walls also tend to collapse to the interior of the chamber. Stage Ⅱ is a sensitive area (5 MPa < Co<11 MPa), the vertical displacement decreases significantly with Co increasing. Stage III is the stable area (Co༞11 MPa), in which the vertical displacement does not change dramatically with the increase of Co, the error bars show the variations in displacement.
A declining and nonlinear relation between fr and Ds is displayed in Fig. 5(b), and it can be separated into 3 stages. Stage I is the failure area (fr <35°), which may be caused by the low ore strength and occurs on the pillar and both sides of the chamber, the entire pillar and the chamber roof are all in shear failure, as shown in Fig. 6(b) (fr =20°). As seen by the error bars, Stage II is a sensitive area (35°<fr<55°) that fluctuates with variations in fr. Stage III is the stable area (fr >55°), in which the vertical displacement does not change significantly with the increase of fr.
As illustrated in Fig. 5(c), Ds satisfy the nonlinear declining relation for different T, 3 stages exist: Stage I is the failure area (T < 3 MPa), which the low ore strength may cause. Stage Ⅱ is a sensitive area (3 MPa < T < 5.5 MPa), the error bars show that the change in Ds is noticeable in this location. Stage III is the stable area (T༞5.5 MPa), in which the vertical displacement does not change significantly with the increase of T. Figure 5(d) illustrates a negative connection between Wp and Ds, 3 stages exist: Stage I is the failure area (Wp<3 m), which may be caused by the too narrow pillar and the large load in the stud. Stage Ⅱ is a sensitive area (3 m < Wp<4.5 m). Stage III is the stable area (Wp >4.5 m), in which the vertical displacement does not change substantially with the increase of Wp. Figure 5(e) illustrates a positive connection between Ls and Ds, 3 stages exist: Stage I is the stable area (Ls<35 m), in which the vertical displacement is small, and the stope safety is good. Stage Ⅱ is a sensitive area (35 m < Ls<50 m). Stage III is the failure area (Ls >50 m), which the too-long stope may cause. In this paper, the mathematical function fitting (Table 3) is used to study the nonlinear relationship between Ds and Co, fr, T, Wp, Ls, and it can be seen from the table below that the fitting coefficients are all above 0.9, and the fitting degree is reasonable.
Relationship
|
Polynomial model equations
|
Correlation coefficient, R2
|
Table 3
The fitting results between single-factor and the vertical displacement
Ds - Co
|
Ds=0.0829Co2-1.9495Co + 35.446
|
0.9731
|
Ds - fr
|
Ds=0.0047fr2-0.6083fr + 43.806
|
0.9933
|
Ds - T
|
Ds=0.0499T2-0.6915T + 28.703
|
0.9805
|
Ds – Wp
|
Ds= -0.5783Wp + 28.709
|
0.9948
|
Ds - Ls
|
Ds= -0.0032Ls2 + 0.4382Ls + 14.397
|
0.9275
|
3.2 PBD simulation results
12 groups of specific tests were implemented according to the scheme of PBD, and the vertical displacements of the 1–4# monitoring points Ds were averaged and listed in the following Table 4. The significance of the factors was analyzed.
Simulation order
|
Hp (m)
|
Wp (m)
|
Co (MPa)
|
Ls (m)
|
Ws (m)
|
fr (°)
|
α (°)
|
T (MPa)
|
Ds (mm)
|
Table 4
Simulation parameters and results of PBD
1
|
4.2
|
4.5
|
11
|
35
|
22
|
55
|
30
|
5.5
|
25.54
|
2
|
3
|
4.5
|
11
|
35
|
22
|
35
|
30
|
3
|
31.25
|
3
|
3
|
3
|
5
|
35
|
15
|
35
|
30
|
3
|
24.24
|
4
|
3
|
4.5
|
5
|
35
|
15
|
55
|
55
|
5.5
|
18.21
|
5
|
4.2
|
3
|
11
|
35
|
15
|
35
|
55
|
5.5
|
22.49
|
6
|
4.2
|
3
|
5
|
35
|
22
|
55
|
55
|
3
|
34.46
|
7
|
3
|
3
|
5
|
50
|
22
|
55
|
30
|
5.5
|
36.02
|
8
|
3
|
4.5
|
11
|
50
|
15
|
55
|
55
|
3
|
20.51
|
9
|
4.2
|
4.5
|
5
|
50
|
22
|
35
|
55
|
3
|
41.09
|
10
|
3
|
3
|
11
|
50
|
22
|
35
|
55
|
5.5
|
36.58
|
11
|
4.2
|
3
|
11
|
50
|
15
|
55
|
30
|
3
|
21.06
|
12
|
4.2
|
4.5
|
5
|
50
|
15
|
35
|
30
|
5.5
|
23.55
|
The findings in Table 4 showed a broad range of Ds from 18.21 mm to 41.09 mm in the 12 tests, and this variety revealed that optimizing influencing factors were essential for enhancing chamber roof stability. The above test results are analyzed, the estimated effect, regression coefficient, and corresponding t and p values are given in Table 5. The calculated standard deviation of the calculation is 1.16029. The sum of prediction errors squares is 96.9312, pred-R2 is 99.59%, and adj-R2 is 97.56%, which indicates that better prediction results are obtained, t-values and p-values were used to determine the significance of each variable.
Variables
|
Effect
|
Coefficient
|
Standard error
|
t-value
|
p-value
|
Table 5
Estimated effect, regression coefficient and corresponding t and p values for Ds in eight variable PBD
Hp/(m)
|
0.064
|
0.032
|
0.3349
|
0.10
|
0.933x
|
Wp/(m)
|
-2.616
|
-1.308
|
0.3349
|
-3.91
|
0.060x
|
Co/(MPa)
|
-3.189
|
-1.594
|
0.3349
|
-4.76
|
0.041z
|
Ls/(m)
|
3.603
|
1.801
|
0.3349
|
5.38
|
0.033y
|
Ws/(m)
|
12.314
|
6.157
|
0.3349
|
18.38
|
0.003y
|
fr/(°)
|
-3.729
|
-1.864
|
0.3349
|
-5.57
|
0.031z
|
α/(°)
|
1.780
|
0.890
|
0.3349
|
2.66
|
0.117x
|
T/(MPa)
|
-1.539
|
-0.769
|
0.3349
|
-2.30
|
0.148x
|
Table 5 Estimated effect, regression coefficient and corresponding t and p values for Ds in eight variable PBD
The variable with a confidence level above 95% (p-value < 0.05) is considered the significant parameter. Analysis of the regression coefficients and the p-values of eight factors (Table 5) show that Co, Ls, Ws, fr were the significant parameter, at the same time, Hp, Wp, α, T were considered non-significant, they were fixed as 3.6 m, 4.5 m, 55°, 1.2 MPa, respectively in the following path of SAD and BBD tests.
3.3 SAD simulation results
By analyzing the PBD results of Table 5, it is found that Ls and Ws positively affect the Ds. In contrast, Co, fr have a negative effect on the Ds, the path of steepest ascent was moved along the direction in which Co, fr decreased and Ls, Ws increased. Five tests were designed as presented in Table 6.
Simulation order
|
Co (MPa)
|
Ls (m)
|
Ws (m)
|
fr (°)
|
Ds (mm)
|
Table 6
Simulation parameters and results of SAD
1
|
5
|
50
|
22
|
35
|
42.91
|
2
|
6.5
|
46
|
20
|
40
|
34.18
|
3
|
8
|
43
|
19
|
45
|
29.31
|
4
|
9.5
|
39
|
17
|
50
|
24.63
|
5
|
11
|
35
|
15
|
55
|
20.98
|
It is noted that the Ds of the 5 SAD tests has been decreasing from Table 6 above. The analysis shows that increasing the Co, fr, and decreasing the Ls, Ws of the stope will lead to smaller Ds and better chamber safety. However, mining efficiency will be significantly reduced when the stope length and stope width are reduced to a certain extent. The rock drilling, charging, mining, and other works will also be significantly hindered. So the goal of optimization is to increase the stope structure parameters as much as possible under the premise of safety. Therefore, the displacement failure criterion of 30mm (Chen et al. 2016) is taken as the “top of the ascent” in SAD. The highest response was 29.31 mm with Co (8 MPa), Ls (43 m), Ws (19 m), fr (45°) at test 3, and it was decided that this position was close to the ideal point, therefore it was picked for further optimization.
3.4 BBD results
A 3-level, 4-factor BBD model that requires 29 simulations was employed to assess the individual or combined effects between the four significant factors and the response variable Ds. The four factors, namely Co, Ls, Ws, and fr, were considered independent input variables. We can predict the Ds using comprehensive factors of the sensitive areas (Co (5–11 MPa), Ls (35–50 m), Ws (15–22 m), fr (35°-55°)) and center point (Co (8 MPa), Ls (43 m), Ws (19 m), fr (45°)). As shown in Table 7, the simulation order 1 to 24 are factorial points, the order 25 to 29 correspond to the zero factor points, the design matrix of tested variables, and the results are represented, where Ds is the average displacement of the monitoring points (1#, 2#, 3#, 4#) obtained by using Flac3D, and the predictive values of average displacement Dp are calculated by the BBD analysis.
Simulation order
|
Co (MPa)
|
Ls (m)
|
Ws (m)
|
fr (°)
|
Ds (mm)
|
Dp (mm)
|
Prediction error ε
|
Table 7
Experimental design and results of BBD
1
|
5(-1)
|
35(-1)
|
19(0)
|
45(0)
|
27.98
|
28.05
|
0.26%
|
2
|
11(+ 1)
|
35(-1)
|
19(0)
|
45(0)
|
26.46
|
26.50
|
0.17%
|
3
|
5(-1)
|
50(+ 1)
|
19(0)
|
45(0)
|
32.27
|
32.03
|
0.74%
|
4
|
11(+ 1)
|
50(+ 1)
|
19(0)
|
45(0)
|
30.52
|
30.25
|
0.88%
|
5
|
8(0)
|
43(0)
|
15(-1)
|
35(-1)
|
24.41
|
24.50
|
0.39%
|
6
|
8(0)
|
43(0)
|
22(+ 1)
|
35(-1)
|
36.95
|
36.84
|
0.29%
|
7
|
8(0)
|
43(0)
|
15(-1)
|
55(+ 1)
|
22.77
|
22.71
|
0.24%
|
8
|
8(0)
|
43(0)
|
22(+ 1)
|
55(+ 1)
|
34.63
|
34.32
|
0.89%
|
9
|
5(-1)
|
43(0)
|
19(0)
|
35(-1)
|
33.06
|
33.02
|
0.13%
|
10
|
11(+ 1)
|
43(0)
|
19(0)
|
35(-1)
|
29.87
|
30.03
|
0.55%
|
11
|
5(-1)
|
43(0)
|
19(0)
|
55(+ 1)
|
29.28
|
29.49
|
0.71%
|
12
|
11(+ 1)
|
43(0)
|
19(0)
|
55(+ 1)
|
28.71
|
29.13
|
1.45%
|
13
|
8(0)
|
35(-1)
|
15(-1)
|
45(0)
|
21.48
|
21.21
|
1.27%
|
14
|
8(0)
|
50(+ 1)
|
15(-1)
|
45(0)
|
23.41
|
23.67
|
1.13%
|
15
|
8(0)
|
35(-1)
|
22(+ 1)
|
45(0)
|
31.88
|
31.87
|
0.02%
|
16
|
8(0)
|
50(+ 1)
|
22(+ 1)
|
45(0)
|
36.04
|
36.80
|
2.12%
|
17
|
5(-1)
|
43(0)
|
15(-1)
|
45(0)
|
24.16
|
24.21
|
0.23%
|
18
|
11(+ 1)
|
43(0)
|
15(-1)
|
45(0)
|
22.81
|
22.72
|
0.39%
|
19
|
5(-1)
|
43(0)
|
22(+ 1)
|
45(0)
|
36.42
|
36.35
|
0.19%
|
20
|
11(+ 1)
|
43(0)
|
22(+ 1)
|
45(0)
|
34.80
|
34.53
|
0.78%
|
21
|
8(0)
|
35(-1)
|
19(0)
|
35(-1)
|
28.30
|
28.42
|
0.42%
|
22
|
8(0)
|
50(+ 1)
|
19(0)
|
35(-1)
|
32.69
|
32.47
|
0.67%
|
23
|
8(0)
|
35(-1)
|
19(0)
|
55(+ 1)
|
26.36
|
26.41
|
0.18%
|
24
|
8(0)
|
50(+ 1)
|
19(0)
|
55(+ 1)
|
30.39
|
30.08
|
1.01%
|
25
|
8(0)
|
43(0)
|
19(0)
|
45(0)
|
29.53
|
29.33
|
0.69%
|
26
|
8(0)
|
43(0)
|
19(0)
|
45(0)
|
29.36
|
29.33
|
0.09%
|
27
|
8(0)
|
43(0)
|
19(0)
|
45(0)
|
29.49
|
29.33
|
0.54%
|
28
|
8(0)
|
43(0)
|
19(0)
|
45(0)
|
29.11
|
29.33
|
0.77%
|
29
|
8(0)
|
43(0)
|
19(0)
|
45(0)
|
29.18
|
29.33
|
0.51%
|
The adequacy and the significance level for the regression model were checked using ANOVA. The regression relationship between Ds and the independent variables A(Co), B(Ls), C(Ws), D(fr) is significant if p-Value ≤ 0.05 of the model item, and when p-Value ≤ 0.01, it means that the regression relationship is highly significant. A more minor “Lack of fit” represent a more significant p-value, which means the model is more significant with linear and quadratic model terms. The closer the coefficient of determination (R2) is to 1, the better the correlation of the model. When R2 is greater than 80%, the correlation of the regression equation is thought to be good.
Table 8 shows the results, the “F-value” of the model was 316.28 and the “p-value”< 0.0001, indicating that the model was highly significant, the value of 1.46 showed that the “Lack of fit” was not the significant compared to the pure error, so the model was suitable for making a prediction. Linear terms of A(Co), B(Ls), C(Ws), D(fr), quadratic terms of A2、B2、C2、D2 and interactive terms of AD、BC were significant for DS, and the other terms are insignificant. A larger F-value indicates that the factor is more critical in the model. From this, the sensitivity of the four factors is Ws >Ls >fr > Co.
Source
|
Sum of
squares
|
Degree of freedom
|
Mean
square
|
F-Value
|
p-Value
|
Significant level
|
Table 8
ANOVA for quadratic Model
model
|
506.51
|
14
|
36.18
|
316.28
|
< 0.0001
|
significant
|
A(Co)
|
7.88
|
1
|
7.88
|
68.85
|
< 0.0001
|
significant
|
B(Ls)
|
39.80
|
1
|
39.80
|
347.95
|
< 0.0001
|
significant
|
C(Ws)
|
421.85
|
1
|
421.85
|
3687.81
|
< 0.0001
|
significant
|
D(fr)
|
13.37
|
1
|
13.37
|
116.90
|
< 0.0001
|
significant
|
AB
|
0.0135
|
1
|
0.0135
|
0.1179
|
0.7364
|
—
|
AC
|
0.0263
|
1
|
0.0263
|
0.2296
|
0.6392
|
—
|
AD
|
1.73
|
1
|
1.73
|
15.09
|
0.0017
|
significant
|
BC
|
1.55
|
1
|
1.55
|
13.52
|
0.0025
|
significant
|
BD
|
0.0353
|
1
|
0.0353
|
0.3089
|
0.5872
|
—
|
CD
|
0.1354
|
1
|
0.1354
|
1.18
|
0.2950
|
—
|
A²
|
1.46
|
1
|
1.46
|
12.75
|
0.0031
|
significant
|
B²
|
1.43
|
1
|
1.43
|
12.51
|
0.0033
|
significant
|
C²
|
1.62
|
1
|
1.62
|
14.16
|
0.0021
|
significant
|
D²
|
2.41
|
1
|
2.41
|
21.08
|
0.0004
|
significant
|
Residual
|
1.60
|
14
|
0.1144
|
—
|
—
|
—
|
Lack of fit
|
1.46
|
10
|
0.1462
|
4.19
|
0.0901
|
not significant
|
Pure error
|
0.1397
|
4
|
0.0349
|
—
|
—
|
—
|
Total
|
508.11
|
28
|
—
|
—
|
—
|
—
|
Based on the data acquired from the Flac3D, a statistical analysis via RSM was used to construct the best-fit regression model for Ds as follows:
For the programming regression equation:
Ds=28.35-0.8233A + 1.85B + 5.95C-1.07D-0.058AB-0.0805AC + 0.6569AD + 0.6166BC-0.0938BD-0.1827CD + 0.4741A²-0.4723B²+0.5129C²+0.6097D²
|
(6)
|
At the same time, the actual regression equation obtained from the programming regression equation according to the actual testing data is as follows:
Ds=25.96701-1.85129Co + 0.602135Ls-0.552446Ws-0.681461fr-0.002577CoLs-0.007666CoWs + 0.021896Cofr + 0.023491LsWs-0.001251Lsfr-0.005221Wsfr + 0.052681 Co2-0.008397 Ls2 +0.041873 Ws2+0.006097 fr2
|
(7)
|
The coefficient of determination R2 and the adj-R2 were calculated as 0.9968, 0.9937, respectively, indicating that the testing and the predicted values are in perfect accordance and that RSM may be represented by a quadratic function. Table 7 lists the predicted value Dp of the chamber roof displacement obtained by using Eq. (7), and the prediction error is also counted in Table 7 to validate the prediction model, the prediction error ε can be calculated by Eq. (8) as follows:
ε=\(\frac{\left|{\text{D}}_{\text{p}}\text{-}{\text{D}}_{\text{s}}\right|}{{\text{D}}_{\text{s}}}\text{×100%}\)
|
(8)
|
The model has favorable reliability because the statistics in Table 7 shows that the ε of the 16th group is 2.12%, and the rest errors are less than 2%, the prediction error is tiny, and the model prediction accuracy is satisfactory.
3.5 Comprehensive study of BBD
It can be seen from the above analysis that Ds is not only related to the single factor of A(Co), B(Ls), C(Ws), D(fr), but also to the interaction between the four factors. The order of influence of each factor on stope displacement Ds can be determined: Ws >Ls >fr > Co> interaction between Co and fr > interaction between Ls and Ws.
The three-dimensional response surface (Fig. 7) can be plotted using the regression equation by selecting any two parameters from the four factors above, and the correlation of each variable on Ds can be reflected by the horizontal plane of the three-dimensional surface.
Figure 7 Response surface figures for Ds by showing variable interactions of (a) Co and Ls, (b) Co and Ws, (c) fr and Co, (d) Ws and Ls, (e) Ls and fr, (f) Ws and fr
The effect of Co and Ls on Ds is given in Fig. 7(a). Ds increases when Co decrease and Ls increases; the growing trend indicates that Ls has a more significant effect on Ds than Co. As shown in Fig. 7(b), Ds increases when Co decrease and Ws increases, the curvature of the graph indicates that Ws has a more significant effect on Ds than Co. The adverse effects of fr and Co on Ds are depicted in Fig. 7(c), which shows that Ds increases when fr, and Co decrease and the effect of fr is almost equivalent Co, there is a zero factor point (when Co(0) = 8 MPa, LS(0) = 43 m, WS(0) = 19 m, fr(0) = 45°), which has a mutation phenomenon, that is, the Ds increases significantly after the zero factor point. As indicated in Fig. 7(d), Ws and Ls positively affect Ds, and the influence of Ws on Ds is more significant from the response surface increasing trend. The adverse effects of fr and positive effects of Ls on Ds are depicted in Fig. 7(e), the effect of Ls and fr on Ds is similar to the growing trend of the response surface. Figure 7(f) shows the influence of Ws and fr on Ds, displacement rises with an increase in Ws and a decrease in fr, Ws has a more significant effect on Ds than fr.