Ejemplo de Diseño de Pilotes

Pilote Colado Analisis de Suelos Gruesos por el fuste (fs=sigmaz*b capa 1

a 9.5

9.5 a

3

10

5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21

SM

9

2 4 ML

Profundidad

22 23 24 25 26 27 28 29 30 31 32 33 34

a 10.5

10.5 a 11

24

a 24.5

24.5 a 25

23

a 23.5

23.5 a 24

22

a 22.5

22.5 a 23

21

a 21.5

21.5 a 22

20

a 20.5

20.5 a 21

19

a 19.5

19.5 a 20

18

a 18.5

18.5 a 19

17

a 17.5

17.5 a 18

16

a 16.5

16.5 a 17

15

a 15.5

15.5 a 16

14

a 14.5

14.5 a 15

13

a 13.5

13.5 a 14

12

a 12.5

12.5 a 13

11

a 11.5

11.5 a 12

10

25

a 25.5

25.5 a

26

H

N60

z

beta

sigmaz

fs

0.5

18

9.25

0.754862

99 99.385

75 75.02192

0.5

17

9.75

0.734988

104.235

76.61145

0.5

19

10.25

0.715617

109.085

78.06311

0.5

20

10.75

0.696714

113.935

79.38008

0.5

21

11.25

0.678245

118.785

80.56533

0.5

22

11.75

0.660182

123.635

81.62164

0.5

22

12.25

0.6425

128.485

82.55161

0.5

23

12.75

0.625175

133.335

83.35771

0.5

24

13.25

0.608187

138.185

84.04226

0.5

31

13.75

0.591516

143.535

84.9032

0.5

30

14.25

0.575145

149.385

85.91808

0.5

31

14.75

0.55906

155.235

86.78562

0.5

33

15.25

0.543244

161.085

87.50853

0.5

37

15.75

0.527686

166.935

88.08933

0.5

34

16.25

0.512373

172.785

88.53044

0.5

35

16.75

0.497294

178.635

88.83416

0.5

38

17.25

0.482439

184.485

89.00268

0.5

32

17.75

0.467797

190.335

89.03808

0.5

34

18.25

0.45336

196.185

88.94234

0.5

33

18.75

0.439119

202.035

88.71738

0.5

36

19.25

0.425067

207.885

88.36502

0.5

35

19.75

0.411196

213.735

87.88702

0.5

38

20.25

0.3975

219.585

87.28504

0.5

41

20.75

0.383972

225.435

86.5607

0.5

39

21.25

0.370606

231.285

85.71556

0.5

44

21.75

0.357396

237.135

84.75112

0.5

42

22.25

0.344337

242.985

83.6688

0.5

43

22.75

0.331424

248.835

82.47001

0.5

42

23.25

0.318653

254.685

81.15608

0.5

44

23.75

0.306018

260.535

79.72832

0.5

43

24.25

0.293515

266.385

78.18797

0.5

45

24.75

0.28114

272.235

76.53625

0.5

44

25.25

0.26889

278.085

74.77434

0.5

46 25.75 TOTAL

0.256761

283.935

72.90337

Suelos Finos por el fuste (fs=alfa*Su) capa

profundida

H

Su

al a lfa

fs

A

Ps

1

1.5 a 5.5

4

45

0.55

24.75

4.39823

108.8562

2

5.5 a

3.5

65

0.55

35.75

3.848451 137.5821

9

246.4383

b

0.35

2b 0.7 Resistencia por la Punta

ta) As

Ps

Ps Acumulado

q't

0.549779 41.24545

41.245

1035

0.096211 99.57867

0.549779 42.11934

83.365

977.5

0.096211 94.04652

0.549779 42.91744

126.282

1092.5

0.096211 105.1108

0.549779 43.64148

169.924

1150

0.549779 44.29311

214.217

1207.5

0.096211 116.1751

0.549779 44.87384

259.091

1265

0.096211 121.7073

0.549779 45.38512

304.476

1265

0.096211 121.7073

0.549779

45.8283

350.304

1322.5

0.096211 127.2394

0.549779 46.20464

396.509

1380

0.096211 132.7716

0.549779 46.67797

443.187

1782.5

0.096211 171.4966

0.549779 47.23593

490.423

1725

0.096211 165.9644

0.549779 47.71289

538.136

1782.5

0.096211 171.4966

0.549779 48.11033

586.246

1897.5

0.096211 182.5609

0.549779 48.42964

634.675

2127.5

0.096211 204.6895

0.549779 48.67215

683.348

1955

0.549779 48.83913

732.187

2012.5

0.096211 193.6252

0.549779 48.93178

781.119

2185

0.096211 210.2216

0.549779 48.95124

830.070

1840

0.096211 177.0287

0.549779 48.89861

878.968

1955

0.096211

0.549779 48.77493

927.743

1897.5

0.096211 182.5609

0.549779 48.58121

976.325

2070

0.096211 199.1573

0.549779 48.31841

1024.643

2012.5

0.096211 193.6252

0.549779 47.98746

1072.630

2185

0.096211 210.2216

0.549779 47.58923

1120.220

2357.5

0.096211 226.8181

0.549779 47.12459

1167.344

2242.5

0.096211 215.7538

0.549779 46.59436

1213.939

2530

0.096211 243.4145

0.549779 45.99933

1259.938

2415

0.096211 232.3502

0.549779 45.34026

1305.278

2472.5

0.096211 237.8824

0.549779 44.61789

1349.896

2415

0.096211 232.3502

0.549779 43.83293

1393.729

2530

0.096211 243.4145

0.549779 42.98608

1436.715

2472.5

0.096211 237.8824

0.549779

1478.793

2587.5

0.096211 248.9467

0.549779 41.10934

1519.902

2530

0.096211 243.4145

0.549779 40.08072

1559.983

2645

0.096211 254.4788

42.078

1559.983

At

0.096211

0.096211

Pt

110.643

188.093

188.093

COMP fuste arcillas Pnec

536.1 246.4383087 Analisis Punta hasta siguiente estrato

Resistencia de Fuste+punta estrato siguiente 135.292 188.476 236.925 286.099 335.924 380.798 431.715 483.076 568.005 609.151 661.919 720.696 790.935 822.769 876.973 942.408 958.147 1018.163 1061.529 1126.901 1169.950 1234.865 1299.448 1335.973 1410.759 1446.289 1497.820 1537.628 1593.311 1631.611 1685.662 1722.208 1774.381 1559.983

289.6617

An

P Necesaria

Cumple

Sobra

Fuste+punta estrato

289.6616913

NO

0.000

0

289.6616913

NO

0.000

0

289.6616913

NO

0.000

0

289.6616913

NO

0.000

0

289.6616913

SI

46.262

330.3919358

289.6616913

SI

91.136

380.7979244

289.6616913

SI

142.054

426.1830438

289.6616913

SI

193.414

477.5434873

289.6616913

SI

278.344

529.2802795

289.6616913

SI

319.489

614.683292

289.6616913

SI

372.258

656.3870741

289.6616913

SI

431.035

709.6321113

289.6616913

SI

501.274

768.8067331

289.6616913

SI

533.107

839.3649639

289.6616913

SI

587.311

871.4406717

289.6616913

SI

652.747

925.8119529

289.6616913

SI

668.486

991.3401773

289.6616913

SI

728.501

1007.098526

289.6616913

SI

771.868

1067.061429

289.6616913

SI

837.239

1110.30421

289.6616913

SI

880.288

1175.481864

289.6616913

SI

945.203

1218.268127

289.6616913

SI

1009.787

1282.852027

289.6616913

SI

1046.312

1347.037704

289.6616913

SI

1121.097

1383.098

289.6616913

SI

1156.627

1457.353101

289.6616913

SI

1208.159

1492.28813

289.6616913

SI

1247.967

1543.160535

289.6616913

SI

1303.649

1582.246274

289.6616913

SI

1341.950

1637.143503

289.6616913

SI

1396.000

1674.597438

289.6616913

SI

1432.546

1727.739738

289.6616913

SI

1484.720

1763.316931

289.6616913

SI

1270.321

1814.46195

RESION

lisis Punta a mitad de estrato CUMPLE

Sobra

NO

0

NO

0

NO

0

NO

0

SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI

40.73024 91.13623 136.5214 187.8818 239.6186 325.0216 366.7254 419.9704 479.145 549.7033 581.779 636.1503 701.6785 717.4368 777.3997 820.6425 885.8202 928.6064 993.1903 1057.376 1093.436 1167.691 1202.626 1253.499 1292.585 1347.482 1384.936 1438.078 1473.655 1524.8

sobra con correccion a mitad de capa 0 0 0 0 18.58369146 68.69931296 113.8287928 164.9676484 216.5162663 301.6826136 343.1074176 396.1139755 455.0898792 525.4884538 557.4429041 611.7306952 677.2125963 692.9612156 752.9504348 796.2550539 861.5295681 904.4472301 969.1966083 1033.581397 1069.874012 1144.39423 1179.626776 1230.828715 1270.275639 1325.565346 1363.442705 1417.039045 1453.100569 1504.759897

Analisis por Compresion Longitud Pilote

h rest

Pn Sobrante

10.24

0.01

17.69782934

10.23

0.02

16.81196722

10.22

0.03

15.9261051

10.21

0.04

15.04024298

10.2

0.05

14.15438086

10.19

0.06

13.26851874

10.18

0.07

12.38265662

10.17

0.08

11.4967945

10.16

0.09

10.61093238

10.15

0.1

9.725070256

10.14

0.11

8.839208135

10.13

0.12

7.953346015

10.12

0.13

7.067483894

10.11

0.14

6.181621774

10.1

0.15

5.295759653

10.09

0.16

4.409897533

10.08

0.17

3.524035412

10.07

0.18

2.638173292

10.06

0.19

1.752311172

10.05 10.04 10.03

0.2 0.21 0.22

0.866449051 -0.01941307 -0.90527519

TENSION Fuste Arcillas Corregido

184.8287

P Necesaria

244.1713

Rest. Fuste al 75% 30.934 31.590 32.188 32.731 33.220 33.655 34.039 34.371 34.653 35.008 35.427 35.785 36.083 36.322 36.504 36.629 36.699 36.713 36.674 36.581 36.436 36.239 35.991 35.692 35.343 34.946 34.499 34.005 33.463 32.875 32.240 31.559 30.832 30.061

Rest. Fuste al 75% Acumulado 30.934 62.524 94.712 127.443 160.663 194.318 228.357 262.728 297.382 332.390 367.817 403.602 439.684 476.007 512.511 549.140 585.839 622.552 659.226 695.807 732.243 768.482 804.473 840.165 875.508 910.454 944.953 978.959 1012.422 1045.297 1077.536 1109.095 1139.927 1169.987

Wf

Sumatoria P necesaria

Cumple

15.63048

15.304

244.171268

NO

16.29434

46.229

244.171268

NO

16.9582

77.753

244.171268

NO

17.62206

109.821

244.171268

NO

18.28591

142.377

244.171268

NO

18.94977

175.368

244.171268

NO

19.61363

208.743

244.171268

NO

20.27749

242.451

244.171268

NO

20.94135

276.440

244.171268

21.6052

310.785

244.171268

22.26906

345.548

244.171268

22.93292

380.669

244.171268

23.59678

416.088

244.171268

24.26064

451.746

244.171268

24.92449

487.586

244.171268

25.58835

523.552

244.171268

26.25221

559.587

244.171268

26.91607

595.636

244.171268

27.57992

631.646

244.171268

28.24378

667.564

244.171268

28.90764

703.336

244.171268

29.5715

738.911

244.171268

30.23536

774.237

244.171268

30.89921

809.266

244.171268

31.56307

843.945

244.171268

32.22693

878.227

244.171268

32.89079

912.063

244.171268

33.55464

945.404

244.171268

34.2185

978.204

244.171268

34.88236

1010.414

244.171268

35.54622

1041.990

244.171268

36.21008

1072.885

244.171268

36.87393

1103.053

244.171268

37.53779

1132.450

244.171268

SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI SI

Analisis por Tension Sobra

Longitud Pilote

h res

Pn Sobrante

0

13.49

0.01

31.57585575

0

13.48

0.02

30.88278609

0

13.47

0.03

30.18971643

0

13.46

0.04

29.49664677

0

13.45

0.05

28.80357711

0

13.44

0.06

28.11050746

0

13.43

0.07

27.4174378

0

13.42

0.08

26.72436814

32.26893 66.61355 101.3766 136.4974 171.9163 207.5747 243.415 279.3805 315.4154 351.465 387.4751 423.3924 459.1645 494.7394 530.0662 565.0942 599.7738 634.0557 667.8914 701.2327 734.0323 766.2431 797.8188 828.7135 858.8816 888.2783

13.41

0.09

26.03129848

13.4

0.1

25.33822882

13.39

0.11

24.64515916

13.38

0.12

23.9520895

13.37

0.13

23.25901984

13.36

0.14

22.56595019

13.35

0.15

21.87288053

13.34

0.16

21.17981087

13.33

0.17

20.48674121

13.32

0.18

19.79367155

13.31

0.19

19.10060189

13.3

0.2

18.40753223

13.29

0.21

17.71446258

13.28

0.22

17.02139292

13.27

0.23

16.32832326

13.26

0.24

15.6352536

13.25

0.25

14.94218394

13.24

0.26

14.24911428

13.23

0.27

13.55604462

13.22

0.28

12.86297496

13.21

0.29

12.16990531

13.2

0.3

11.47683565

13.19

0.31

10.78376599

13.18

0.32

10.09069633

13.17

0.33

9.397626671

13.16

0.34

8.704557012

13.15

0.35

8.011487353

13.14

0.36

7.318417695

13.13

0.37

6.625348036

13.12

0.38

5.932278377

13.11

0.39

5.239208718

13.1

0.4

4.54613906

13.09

0.41

3.853069401

13.08

0.42

3.159999742

13.07

0.43

2.466930084

13.06

0.44

1.773860425

13.05

0.45

1.080790766

13.04 13.03 13.02 13.01 13

0.46 0.47 0.48 0.49 0.5

0.387721107 -0.30534855 -0.99841821 -1.69148787 -2.38455753