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VALIDATION OF SPECTRAL FATIGUE ANALYSIS OF

STRUCTURES IN MUMBAI HIGH FIELD

BY

S.Nallayarasu, S.Goswami, J.S.Manral, R.M.Kotresh

Presenter: S.K. Bhattacharyya

Dept. of Ocean Engineering

IIT Madras

Mumbai high field location

 Historically, Bombay High Field of ONGC has several offshore platforms in the shallow water region of 50 to 80m water depth.

 Most of these platforms are fixed template type structures with either main or skirt piles.

 Many of these structures are as old as 20 to 30 years & have been designed as per API

RP 2A guidelines.

 These structures mostly produce oil & Gas and have both process & well head platforms.

 These platforms have been designed against fatigue from cyclic wave loads.

DIRECTIONAL DISTRIBUTION OF WAVES

1.

2.

The field is located on the west coast of India and the wave approach is from south to northwest directions and the other directions are shielded from land.

Generally waves are approaching the platforms only from

South, South-West,

West and North-West.

The directional distribution of waves used in the deterministic and spectral methods is shown in Figure

FATIGUE RESPONSE ANALYSIS

Deterministic method of analysis

Seastate is discretised in discrete (deterministic) waves the scatter data based sea state specific information is used.

Structural response to these discrete waves is then calculated either with or without dynamic effects depending on natural period.

Spectral method of analysis

Seastate is characterised by the spectral energy.

Further, the scatter data for different directions and wave heights are used to simulate the seastate.

The structural response is then calculated using stochastic method of structural analysis.

Dynamic analysis is performed to generate the dynamic characteristics such as mode shapes and mass characteristics.

WAVE SCATTER DATA

 Wave scatter data and exceedance information used for the deterministic fatigue analysis is shown in Table 1 and 2.

 The exceedance data has been converted to occurrence cyclic data with intermediate data range by interpolation

 It has been summarised in Table 3.

WAVE SCATTER DATA – Deterministic Table - 1

WAVE HEIGHT

(M)

0.0-1.524

1.524 - 3.047

3.048 – 4.571

4.572 – 6.095

6.096 – 7.619

7.620 - 9.143

9.144 – 10.667

10.668 – 12.192

S

8.7

9.2

9.5

9.7

9.9

10.5

10.6

10.8

11.0

PERIOD (SEC)

SW W

9.6

8.3

10.1

10.3

10.4

8.7

9.2

9.6

10.0

10.3

10.6

10.9

8.9

--

--

--

NW

6.6

7.4

7.9

8.4

WAVE SCATTER DATA – Deterministic Table - 2

0

1.524

3.048

4.572

6.096

7.620

9.144

10.668

12.192

Wave

Height (m)

S DIR

-

-

11

0

-

1276045

61704

3132

167

Number of Waves Exceeding Specified Height

In One Year

SW DIR W DIR NW DIR

770535 1015713 1220511

CUMULATIV

E

4282804

219347 220985 69788 571824

37929

5878

31902

4073

3764

177

76727

10295

2

0

869

126

18

493

59

7

1

0

8

0

-

-

-

1381

185

25

3

0

WAVE SCATTER DATA – Deterministic Table - 3

Wave Height

(m)

0.381

1.143

1.905

2.667

3.429

4.191

4.953

5.715

6.447

7.239

8.001

8.763

924

322

112

39

13

541944

252784

137022

52061

20503

7326

2656

W SW

1391

538

205

78

30

359421

191767

128135

53283

22998

9053

3618

0

0

32

11

0

995444

218897

47802

10770

2409

556

124

S NW

0

0

30

8

0

928660

222063

53581

12443

2948

639

139

WAVE SCATTER DATA – Spectral

The wave scatter data for spectral analysis obtained from National

Institute of Oceanography is summarized in Tables 4 to 8 for south, south-west, west and north-west directions respectively.

The percentage distribution for each combination of wave period and height will be used for the spectral representation of the seastate using JONSWAP spectra.

Table-4 ( South)

Hs

(m)

3-4

0.0 -

0.5

0.5 -

1.0

1.0 -

1.5

1.5 -

2.0

0.38

0.00

0.00

0.00

Total 0.38

4-5

0.77

5.00

2.69

5-6

0.00

17.31

10.77

Mean wave period (s)

6-7

0.00

18.85

15.00

7-8

0.00

11.54

1.92

0.00

2.31

2.31

2.31

8.46 30.38 36.15 15.77

8-9

0.00

1.15

2.31

3.85

7.31

9-10

0.00

0.00

0.00

0.77

0.77

10-11

0.00

0.00

0.00

0.77

0.77

Total

1.15

53.85

32.69

12.31

100.00

WAVE SCATTER DATA – Spectral

Hs

(m)

3-4 4-5 5-6

0.0 - 0.5

0.5 - 1.0

0.00

0.21

0.00

2.92

0.00

5.22

6-7

Mean wave period (s)

7-8 8-9

0.00

1.67

0.00

0.84

0.00

0.00

1.0 - 1.5

1.5 - 2.0

2.0 - 2.5

2.5 - 3.0

3.0 - 3.5

3.5 - 4.0

4.0 - 4.5

4.5 - 5.0

5.0 - 5.5

5.5 - 6.0

Total

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.21

0.00

0.00

0.00

0.00

0.84

0.00

0.00

0.00

0.00

0.00

3.76

11.90

4.59

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

21.71

9.81

16.08

3.97

3.55

1.88

0.63

0.00

0.00

0.00

0.00

37.58

2.51

3.34

0.42

1.25

2.71

9.60

5.22

2.51

0.63

0.00

29.02

0.00

0.00

0.00

0.84

0.21

2.09

2.30

0.42

1.67

0.21

7.72

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

9-10

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

10-11

0.00

0.00

0.00

3.97

0.42

2.09

2.30

0.21

100.00

Total

0.00

10.86

25.47

32.36

11.48

6.47

4.38

WAVE SCATTER DATA – Spectral

Hs

(m)

3-4 4-5 5-6 6-7

Mean wave period (s)

7-8 8-9

0.0 - 0.5 0.00

0.00

0.00

0.00

0.00

0.00

0.5 - 1.0

1.0 - 1.5

1.5 - 2.0

2.0 - 2.5

2.5 - 3.0

3.0 - 3.5

3.5 - 4.0

4.0 - 4.5

4.5 - 5.0

5.0 - 5.5

5.5 - 6.0

6.0 - 6.5

Total

9.85

6.61

2.53

0.14

0.00

30.52

0.00

0.00

0.00

0.56

0.84

3.66

6.33

0.14

0.00

0.00

0.00

0.00

34.60

0.00

0.70

2.81

5.63

12.80

9.00

3.52

0.00

0.00

0.00

0.00

0.00

23.63

1.83

4.22

9.00

6.05

2.39

0.14

0.00

0.00

0.00

0.00

0.00

0.00

3.94

1.83

1.69

0.42

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.28

0.28

0.00

0.00

0.00

0.00

0.00

0.00

0.00

1.69

3.38

1.27

0.42

7.03

0.00

0.00

0.00

0.00

0.14

0.00

0.14

0.00

0.00

0.00

0.00

0.00

0.00

10-11

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

9-10

0.00

0.00

0.00

0.00

0.00

0.00

0.00

0.00

Total

0.00

3.94

6.61

12.24

12.24

16.17

12.80

9.99

9.99

8.30

5.91

1.41

0.42

100.00

WAVE SCATTER DATA – Spectral

Hs

(m)

0.0 - 0.5

0.5 - 1.0

1.0 - 1.5

Total

3-4

0.00

4.35

0.00

4.35

4-5

0.00

34.78

17.39

52.17

5-6

0.00

19.57

19.57

39.13

6-7

Mean wave period (s)

7-8 8-9

0.00

0.00

0.00

0.00

0.00

0.00

2.17

2.17

0.00

0.00

0.00

0.00

9-10

0.00

0.00

0.00

0.00

10-11

0.00

0.00

2.17

2.17

Total

0.00

58.70

41.30

100.00

SELECTED STRUCTURES

RS-14 WELLHEAD PLATFORM

4 LEGGED PRODUCTION CUM DRILLING PLATFORM

WATER DEPTH- 76.2 M

0 MAIN & 8 SKIRT PILES

16 WELL SLOTS & CONDUCTORS

MODULAR DRILLING RIG HAVING RIG MAST, RIG

SUPPORT & LQ MODULE

TOPSIDE WEIGHT- 6000 MT

JACKET WEIGHT-3300 MT (GROSS)

SELECTED STRUCTURE

MNP PROCESS PLATFORM

EIGHT LEGGED 4 LEVEL TOPSIDES

WATER DEPTH-72 M

16 SKIRT PILES

20 PRE-INSTALLED RISERS

LAUNCH JACKET WEIGHT-7200 MT

PROCESS HUB-

TOTAL TOPSIDE WEIGHT-20000 MT

3 PROCESS GAS COMPRESSORS, 1

BOOSTER GAS COMPRESSOR.

SUBSTRUCTURE SUPPORTS FOR 3

BRIDGES

DETERMINISTIC ANALYSIS

The calculation of cyclic stresses on the tubular joints shall include dynamic amplification. The effects of dynamic amplification can be ignored when the natural period of the structure is below 3 seconds as stated in API RP 2 A. This is due to the fact that most of the wave period inducing cyclic loads will be in range of 4 to 12 seconds.

The dynamic amplification factor (DAF) can be calculated using the following formula assuming a single degree of freedom system for the fixed type jacket structures.

DAF

1

T

T

N

2

2

 

T

(1 ) (2 )

T n

2 where T n is the natural period of the structure, T is the wave period and  is the damping ratio( 2%). It can be shown that the the response and cyclic stress ranges can be linearly multiplied by the DAF and hence the total response can be calculated without going into the full fledged dynamic response of the structure against waves.

However, the accuracy of the analysis depends highly on the descretization of the seastate and any simplification will lead to erroneous estimation of response and fatigue damage.

}

Where [K] is the stiffness matrix, {X} and {F} are the displacement and force vectors respectively. The above approach indicates a simplified method and is very easy to implement for practice. This method has been in use for several years for the prediction response of offshore structures.

SPECTRAL ANALYSIS

Alternatively, the response and the cyclic stresses can be calculated using dynamic wave response including dynamic effects due to the above. This method of calculation involves procedures involving dynamic characteristics of the structure and performing the analysis in close intervals of frequency / wave period. However, the method of calculation involved several approximations and the discussion on these issues is outside the scope of this paper and can be found elsewhere.

M

(3)

Solution to the following equation will lead to Eigen modes and vectors. The dynamic analysis is performed to obtain the dynamic characteristics such as mode shapes and frequencies.

Where X” is the Eigen frequencies and X is the displacements. The mode shapes and frequencies are then used in the subsequent wave response calculation in which the following equation is solved including the dynamic response of the system.

X

M

F

( 4)

The response is calculated as a transfer function to facilitate the computation of the fatigue damage for various waves in different directions. Typical wave response stress transfer function for base shear and overturning moment is shown in Figure 1 and 2 respectively

SPECTRAL ANALYSIS FIG-1

TRANSFER FUNCTION FOR BASE SHEAR

SPECTRAL ANALYSIS FIG-2

TRANSFER FUNCTION FOR OVERTUNING MOMENT

SPECTRAL ANALYSIS

 Selection of frequencies for the generation of transfer function is an important task such that the peaks and valleys of the response is not missed. Following the guidelines given API RP 2A, the frequencies near the natural period of the structure and its multiples shall be selected. The transfer function has been generated for various frequencies from 0.1 Hz to 0.5Hz (Typically from wave periods in the range of 2 to 10 seconds). The frequency interval is selected such that more number of points is generated near the natural period,

 The transfer function and the response are generated for both maximum base shear and maximum overturning moment cases and the worst case is used for the calculation of fatigue damage.

 A wave steepness of 1/20 is used for the all the waves as recommended by API RP

2A for the calculation of wave height for each frequency. This has been used for the generation of the transfer function.

 It can be observed from Figure 1 and 2 that the maximum values of transfer function occurs near the frequency of 0.4 which corresponds to a period of 2.5 sec.

The natural period of the structures for MNP and RS14 is noted to be between 2.5 sec and 3 sec.

ESTIMATION OF FATIGUE DAMAGE

Fatigue damage has been calculated for all the tubular connections using Miner’s rule using cumulative fatigue damage model stated as below.

RMS i   

0

H i

2

( ) h

( )

(5)

T z

 

0

RMS i

2 2 f H ( ) h

( )

(6)

ESTIMATION OF FATIGUE DAMAGE – (Contd.) where σ is the RMS (Root mean square value) of the stress calculated from the transfer function for a given Seastate, H is the transfer function and S is the spectral density of the seastate.

(7) n ( s )

 mL

T z where n(s) is the number of applied cycles, L is the design life and Tz is the spectral mean period calculated above.

Fatigue damage

D

 n ( s )

2

RMS i

 

0

N s

( s ) exp(

 s

2

2

RMS i

) ds (8) where N(s) is the allowable cycles from the S-N curve and S is the stress range.

Stress concentration factor (SCF) for the tubular joints has been calculated as per

Effthimiou formulas as recommended by API RP 2A for tubular joints and the S-N curve has been adopted as per API RP 2A for tubular joints.

FACTOR OF SAFETY

FAILURE

CRITICAL

NO

YES

API RP 2A

INSPECTABLE

2

5

NON-INSPECTABLE

5

10

ONGC

2

4

ONGC USE A FOS OF 4.0 FOR JOINTS BELOW TOW LEVELS OF JACKET FRAMING TO COVER FOR

FATIGUE DUE TO WAVE LOADS

RESULTS AND DISCUSSIONS

 MHN (Mumbai High North) field has been presented in

Table 8 and 9 respectively. The fatigue life of major tubular joints along the jacket legs and X braces is presented. Fatigue life greater than 1000 years is marked as * since it is very high compared to the required design fatigue life of 50 years.

The fatigue life predicted by deterministic analysis for RS

14 well platforms seems to be on a higher side compared to the spectral fatigue analysis. In the case of MNP

Process platform deterministic results are lower than spectral for lower three levels and reverse is the case for

4 th and 5 th level.

This is due to the fact that the Seastate has been condensed to discrete waves and the DAF has been treated approximately.

Table 8. RS-14 Well platform

Comparison of results of deterministic & spectral fatigue on selected joints

JOINT NO.

FATIGUE LIFE

DETERMINISTIC SPECTRAL

397L

301X

302X

303X

303

304

305

403L

203L

217L

283L

297L

201X

303L

317L

383L

417L

483L

497L

401X

402X

74.71

31.17

968.58

*

*

224.9

1039.15

*

456.34

*

287.44

416.70

*

*

*

307.89

1287.7

369.62

118.87

23.18

4.11

17.84

31.79

473.76

627.151

*

83.01

215.84

245.01

187.75

*

172.09

241.13

*

*

*

844.62

*

90.76

32.14

5.32

0.87

DIFFERENCE

(D-S)

0

-

0

0

269

0

115

175

56.87

0

494

400

0

142

824

750

0

278.86

86.73

17.86

3.24

503X

504X

603L

617L

683L

697L

601X

602X

403X

404X

503L

517L

583L

597L

501X

502X

603X

604X

703L

717L

783L

797L

Table 8. Continued

JOINT NO.

FATIGUE LIFE

DETERMINISTIC SPECTRAL

*

*

255.38

541.82

78.56

67.82

49.13

18.42

*

*

145.32

273.35

160.99

28.88

*

*

*

*

1344.463

*

*

*

*

*

252.72

432.30

14.58

25.80

3.86

1.91

655.58

*

141.13

12.08

19.34

7.21

399.95

398.85

23.92

24.27

6.60

6.055

6.099

5.54

DIFFERENCE

(D-S)

0

0

2.66

109.52

63.98

42.02

45.27

16.51

345

0

131.19

261.27

141.65

21.67

600

600

976

976

994

994

994

994

JOINT

NO.

504X

603L

617L

683L

697L

601X

602X

603X

404X

503L

517L

583L

597L

501X

502X

503X

604X

703L

717L

783L

797L

Table 8. Continued

FATIGUE LIFE

DETERMINISTIC SPECTRAL

*

255.38

541.82

78.56

67.82

49.13

18.42

*

*

145.32

273.35

160.99

28.88

*

*

*

*

1344.463

*

*

*

*

252.72

432.30

14.58

25.80

3.86

1.91

655.58

*

141.13

12.08

19.34

7.21

399.95

398.85

23.92

24.27

6.60

6.055

6.099

5.54

DIFFERENCE

(D-S)

0

2.66

109.52

63.98

42.02

45.27

16.51

345

0

131.19

261.27

141.65

21.67

600

600

976

976

994

994

994

994

Table 9. MNP Process platform

Comparison of results of deterministic & spectral fatigue on selected joints

JOINT NO.

FATIGUE LIFE

DETERMINISTIC SPECTRAL

DIFFERENCE

(D-S)

204X

205X

206X

207X

208X

209X

210X

211X

203L

207L

213L

217L

283L

287L

293L

297L

212X

213X

203L

207L

213L

217L

*

*

*

*

*

*

*

*

52.41

9.47

9.26

78.80

52.93

11.55

11.14

43.65

*

*

52.41

9.47

9.26

78.80

*

*

*

*

*

*

*

*

108.38

34.14

21.43

127.34

129.05

81.14

69.06

88.38

*

*

108.38

34.14

21.43

127.34

0

0

0

0

0

0

0

0

-77

-70

-58

-45

-56

-24

-12

-49

0

0

-56

-24

-12

-49

JOINT

NO.

303L

307L

305X

306X

307X

308X

309X

310X

311X

312X

313X

313L

317L

383L

387L

393L

397L

304X

403L

407L

Table 9. Continued

FATIGUE LIFE

DETERMINISTIC SPECTRAL

20.89

70.45

*

*

*

*

*

*

*

*

*

69.36

18.49

19.56

197.60

253.92

18.97

*

149.07

20.62

202.21

508.03

*

*

*

*

*

*

*

*

*

806.51

302.99

267.49

485.68

783.73

358.24

*

*

200.44

DIFFERENCE

(D-S)

-182

-438

-737

-284

-248

-288

-530

-339

-851

-180

JOINT

NO.

406X

407X

408X

409X

410X

411X

412X

413X

417L

483L

487L

493L

497L

404X

405X

503L

507L

513L

517L

583L

Table 9. Continued

DETERMINISTIC SPECTRAL

156.09

185.24

168.31

140.70

135.05

*

*

*

*

*

*

*

*

*

429.95

104.71

24.17

23.69

153.88

301.03

72.32

163.23

147.37

132.46

118.97

*

*

*

*

*

*

96.67

513.86

125.03

21.49

0.88

0.06

1.07

0.85

0.87

DIFFERENCE

(D-S)

84

22

21

8

16

903

486

875

409

104

24

22

153

300

JOINT

NO.

505X

506X

507X

508X

509X

510X

603L

607L

587L

593L

597L

501X

502X

503X

504X

613L

617L

683L

687L

693L

Table 9. Continued

DETERMINISTIC SPECTRAL

73.39

156.72

181.49

*

*

*

*

*

*

*

*

*

*

151.58

99.52

184.74

370.08

206.42

105.74

180.44

0.89

1.01

0.69

127.26

136.83

234.38

115.94

108.49

233.61

1.42

1.57

1.42

0.21

0.57

1.18

1.21

0.56

0.70

1.20

1.13

DIFFERENCE

(D-S)

892

767

999

999

999

999

151

98

183

369

205

104

179

72

155

180

873

864

760

884

CONCLUSIONS

 Based on the results obtained from the fatigue analysis of platforms in

Mumbai High North and South platforms, following observations are made.

 Generally both methods predict fatigue life reasonably well for most of the joints except for some joints at the bottom of the jacket, the deterministic method predicts the fatigue life lower than the spectral methods. This is due to the fact that the dynamic response of the structure over-predicted by deterministic method by approximate calculations of DAF due to course discretisation of wave periods.

 However, the joints near the top of the jacket, the predicted fatigue life using deterministic methods seems to be higher than the spectral methods. This is due to the fact that the wave load and associated cyclic stresses are only due to the local wave loads rather than the dynamic response.

 It is recommended that spectral fatigue analysis be used for large platforms to assess the fatigue life since the inaccuracy introduced due to the treatment of dynamic amplification factor.

References

 API RP 2A Recommended Practice for the Design and

Construction of fixed offshore platforms, working stress design.

 Fatigue User Manual, SACS Software, EDI

 Identification of wave spectra for Mumbai offshore region,

National Institute of Oceanography, December 2007.

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