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Journal of Natural Sciences Research                                                            www.iiste.org
ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online)
Vol.2, No.3, 2012

    Failure Analysis of the Reducer Nipple of a Propylene Gas Tank
                         in a Petrochemicals Complex

                                        Okpala, Alexander Nwachukwu, PhD
                                      Department of Mechanical Engineering,
                                 Faculty of Engineering, Niger Delta University,
                                   Wilberforce Island, Bayelsa State, Nigeria.
                             E-mail: okpalana@gmail.com Phone: +2348030854206


Abstract
Failure Investigation was carried out on a fractured reducer nipple of pipeline connected to a propylene tank in a
         Petrochemical complex. The Investigation was carried out with the aim of determining the root cause of
         the failure. In the course of this investigation, Metallurgical techniques including micrography and
         fractography as well as stress analysis of the piping were carried out on the failed part. The root cause
         of the failure was identified as vibration induced fatigue enhanced by the non-homogeneity of the
         microstructure of the nipple. Remedial measures to prevent a reoccurrence were proffered.


Key Word: Metallography, Fractography, Failure, Analysis, Striation, Fatigue, transgranular.


1.0      Introduction
This article is based on the root cause analysis of a fractured reducer nipple of pipeline connected to a propylene
          tank in a Petrochemical complex. The line operated at a pressure of 32kg/cm2. The fractured end of the
          nipple has an outside diameter of 0.885in and a thickness of 0.167in. Picture of this nipple is presented
          in figures 1. Records showed that the piping have been in service for about thirteen years and failed
          within this period under similar circumstances and was repaired.
2.0      Scope of Report
The scope of the failure analysis includes:
(1)      Complete metallographic analysis of failed pieces with scanning electron microscopy (SEM), and
         spectrometric analysis of material and weldment.
(2)      Mechanical Testing include; hardness testing and Tensile strength determination.
(3)      Combing piping stress analysis at fracture point
(4)      Root cause determination and recommendations to avoid reoccurrence of failure.
3.0      Metallurgical Study of Failure
3.1      Spectrometric Analysis
The Chemical analysis of the nipple was carried out using an optical emission spectrometer which gave the
       composition presented in Table 1.
Table 1: Chemical Composition of Nipple Body
C          Cr         Ni         Si           Mn        S         P         Cu      Mo

0.31       0.28       0.04       0.25         0.8       0.04      0.035     0.035   0.12


This conforms to ASTM A105.
3.2      Metallographic Analysis
The fractured Heat affected zone (HAZ) of the reducer nipple of the pipe linking the propylene gas tank and the
cracked weld joint in the by-pass line were prepared for metallography in accordance with ASTM E3, methods
of preparation of metallographic specimen. The three samples were then observed under metallurgical



                                                       34
Journal of Natural Sciences Research                                                             www.iiste.org
ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online)
Vol.2, No.3, 2012

microscope and the resulting micrographs are presented in figures 3 and 4. The grain sizes of the samples were
also determined in consonance with the requirement of ASTM E 112.


Discussion of Micrographs
The micrograph of the reducer nipple of the propylene gas tank presented in figure 3 revealed that the nipple has
a coarse grained ferrite-pearlite microstructure with ASTM grain size number 4 to 6. The variation in grain size
depicts in homogeneity in the microstructure. The micrograph of the weldment (valve end of nipple) in figure 4
however revealed homogenous structure of pearlite in ferrite matrix with ASTM grain size number between 9
and 10. This micrograph also shows porosities on the weldment.


3.3      SEM Analysis
Samples from, reducer nipple of the propylene gas tank and the valve end of the nipple were subjected to SEM
fractography using JEOL JSM-6390LV scanning electron microscope. In the course         of      the       SEM
fractography, several shots were taken at different points on each of the mounted samples at magnification of
x300, x500 and x700. The resultant fractographs are presented in figures 5 though 10.


Discussion of SEM Fractographs
The fractographs of the nipple revealed the three-dimensional nature of the various grains which is typical of
integranular brittle fracture as opined in Davis(1998). It also revealed fatigue striations characteristic of fatigue
failure. The presence of an isolated tear in figure 8 shows the weldment is tougher than the body of the nipple.


4.0      Mechanical Test
4.1      Micro hardness Test
The samples of the reducer nipple of A propylene tanks were subjected to micro microhardness test using
Leco microhardness tester LM 700AP, applying a load of 50gf in a dwell time of 15 seconds. The test was
carried out in accordance with ASTM standard E92, standard test method for Vickers hardness of metallic
materials and ASTM E384, standard test for microhardness of materials. The result of the test is presented in
table.
Table 2 : Microhardness Test Result of Reducer Nipple
                VHN           VHN            VHN           Average       Deviation      Range         Converted
                                                           VHN                                        to BHN
Nipple Body     122.3         129.3          117.8         123.1         5.7            11.5          116
Weldment        152.4         168.4          166.5         162.4         8.7            16.0          150


Discussion
The high values of the deviation in the hardness of the three points taken in each of the sample shows in-
homogenity in the microstructure of the flange.


4.2      Tensile Strength of materials
The tensile strength = KxBHN Mpa [Rao (1998)]
Where k = 3.296 for allow steel and 3.342 for plain carbon steel.
For the nipple body, tensile strength = 3.296 x 1.6 = 382.Mpa
For the weldment, Tensile strength = 23.342 x 150 = 501.3Mpa
5.0      Stress Analysis of Failed Reducer Nipple
5.1      Determination of the maximum allowable pressure (Design pressure)
Data:
Nominal outside diameter, D = 0.885in
Nominal inside diameter, d = 0.55in

                                                        35
Journal of Natural Sciences Research                                                           www.iiste.org
ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online)
Vol.2, No.3, 2012

Mean diameter Dm = 0.7175in
Operating Temperature = 75 – 80oC (167 – 176F)
Material of pipe = ASTM A 105
Designation: Similar to API 5L GR B
Operating pressure = 32kg/cm2 = 456.7psi


The maximum allowable pressure is determined in accordance with ANSI/ASME B31.8 standard for Gas
Transmission and Distribution system by the equation.
P = (2 St/D) x F x E x T                                                         5.1
Where, P = Design pressure, (psi)
S = Specified minimum yield strength (psi)
t = Nominal wall thickness (in)
D = Nominal outside diameter (in)
F = Design factor
E = Longitudinal joint factor
T = Temperature de-rating factor.
S = 35,000psi [ANSI/ASME Code B31-8-2003, Appendix D]
t = 0.157IN
D = 2.357in
F = 0.72 [ANSI/ASME Code B 31-8-2003 Table 841.1A]
E = 1.00 [ANSI/ASME Code B 31-8-2003 Table 841.1B]
T = 1.00 [ANSI/ASME Code B 31-8-2003 Table 841.1C]
Therefore Design pressure,
P = (2 x 35,000 x 0.0.167 ÷ 0.885) x 0.72 x 1.00 x 1.00 = 9510.5Psi = 670kg/cm2


5.2      Determination of the collapsing pressure of pipe
The collapsing pipe pressure is determined, taking into consideration the effect of lateral contraction by the DNV
equation.

                                                               5.2

 [Antaki (2005)] Where Pc = minimum net collapsing pipe pressure (psi)
                                    6
Ey = modulus of elasticity = 28 x 10 psi
t = pipe thickness = 0.167in
Dm = Mean diameter of pipe = 0.7175in
λ = Poisson ration = 0.29

Therefore, collapsing pipe pressure,




5.3      Determination of Maximum allowable net external pressure for pipe with eccentricity (1% out-of-
         roundness)




                                                       36
Journal of Natural Sciences Research                                                               www.iiste.org
ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online)
Vol.2, No.3, 2012

[Yong Bai and Qiang Bai (2005)]

Where Pe = maximum allowable net external pressure
Pc = critical value of collapsing pressure
S = yield stress allowable stress value.

= 30,250 psi [ANSI/ASME code B31-4-2006, Table 402.3.1(a)




         Pe2- 475,510.81Pe +4,819,308,354 = 0

         Pe=10,360.8psi=729.9Kg/cm2

5.4      Hoop Stress (Sh) Analysis
Sh = (Pe – Pi) (D – t)/2t   5.4
= (10,360.8 – 456.7) (0.885 – 0.167)/2 x 0.167
= 21,289psi
Hoop stress criterion of ABS (2000) according to Yong Bai and Qiang Bai (2005) is given by
=        Sh < F x S x T = 0.72 x 35000 x 1 = 25200
The hoop stress for the pipe is therefore appropriate since it is less than the value obtained from the criterion.


6.0      Conclusion / Root Cause of Failure
(1)      The nipple failed by brittle fracture, the cracks being mainly intergranular in nature.
(2)      The fatigue striation in the SEM fractography revealed the fracture mechanism as fatigue.
(3)      The grain size variation of the nipple shows in-homogeneity of the coarse microstructure.
(4)      Failure of the reducer nipple of a propylene gas tank as a result of vibration induced fatigue enhanced
by the non-homogeneity of its microstructure.


7.0      Recommendations
         Irrespective of the accompanying certificate, it is advised that new nipples to be installed be
subjected to in-house normalizing heat treatment at 910oC for 30 minutes as this will go a long way in
improving the homogeneity of its microstructure.


Acknowledgement
The author is grateful to Engineering Materials Development Institute Akure, Nigeria and the University of
Legon, Ghana for providing the equipment used for this work.
REFERENCES
   1) ANSI/ASME B31.8 Standard for Gas Transmission and Distribution, ASTM International., USA, 2003.
   2) ANSI/ASME B31.4 Pipeline Transportation Systems for Hydrocarbon and other liquids, p9, ASTM
      International., USA, 2006.
   3) Antaki, G.A. (2003), Piping and Pipeline Engineering, Marcel Dekker, Inc, New York.
   4) ASTM E3 – 01 Standard Guide for Preparation of Metallographic Specimens, ASTM International,
      West Conshohocken, PA, 2004.
   5) ASTM E112-10 Standard Test Method for Determining Average grain size, ASTM International., USA,
      2010.
   6) Davis, J.R. (1998), Principles and Procedures of Fractography in Metals Handbook, Desk Edition, 2nd
      Edition, ASM International, pp 1238-1247.
   7) Rao, P.N. (1998), Manufacturing Technology, McGraw Hill Publisher.
   8) Yong Bai and Qiang Bai (2005),Subsea Pipelines and Risers, Elsevier Inc, USA.


                                                         37
Journal of Natural Sciences Research                                                     www.iiste.org
ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online)
Vol.2, No.3, 2012




Figure1: Failed Reducer Nipple            Figure 2: Repaired Reducer Nipple




Figure 3: Micrograph of reducer nipple,   Figure 4: Micrograph of valve end of reducer
2% nital etch x800                                nipple, 2% nital etch x400




                                                   38
Journal of Natural Sciences Research                                                         www.iiste.org
ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online)
Vol.2, No.3, 2012




                                                                                    Fatigue Striation


                                                                 3-D appearance of grains
                                                                 (Intergranular attack)




Figure 5: SEM Fractograph of failed reducer                  Figure 6: SEM Fractograph of failed reducer
nipple, x700                                                           nipple , x300




                              Cavity
                                                                                            Tea
                                                                                            r




Figure 7: SEM Fractograph of failed reducer     Figure 8: SEM Fractograph of failed valve end
nipple, x500                                           (weldment) of nipple, x500



    3-D appearance of grain
    (intergranular attack)                                                         3-D appearance of grain
                                  Fatigue                                          (intergranular attack)
                                  Striatio




Figure 9: SEM Fractograph of failed valve end    Figure 10: SEM Fractograph of failed valve end
(weldment) of nipple, x700                              (weldment) of nipple, x300




                                                      39
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Failure analysis of the reducer nipple of a propylene gas tank in a petrochemicals complex

  • 1. Journal of Natural Sciences Research www.iiste.org ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online) Vol.2, No.3, 2012 Failure Analysis of the Reducer Nipple of a Propylene Gas Tank in a Petrochemicals Complex Okpala, Alexander Nwachukwu, PhD Department of Mechanical Engineering, Faculty of Engineering, Niger Delta University, Wilberforce Island, Bayelsa State, Nigeria. E-mail: okpalana@gmail.com Phone: +2348030854206 Abstract Failure Investigation was carried out on a fractured reducer nipple of pipeline connected to a propylene tank in a Petrochemical complex. The Investigation was carried out with the aim of determining the root cause of the failure. In the course of this investigation, Metallurgical techniques including micrography and fractography as well as stress analysis of the piping were carried out on the failed part. The root cause of the failure was identified as vibration induced fatigue enhanced by the non-homogeneity of the microstructure of the nipple. Remedial measures to prevent a reoccurrence were proffered. Key Word: Metallography, Fractography, Failure, Analysis, Striation, Fatigue, transgranular. 1.0 Introduction This article is based on the root cause analysis of a fractured reducer nipple of pipeline connected to a propylene tank in a Petrochemical complex. The line operated at a pressure of 32kg/cm2. The fractured end of the nipple has an outside diameter of 0.885in and a thickness of 0.167in. Picture of this nipple is presented in figures 1. Records showed that the piping have been in service for about thirteen years and failed within this period under similar circumstances and was repaired. 2.0 Scope of Report The scope of the failure analysis includes: (1) Complete metallographic analysis of failed pieces with scanning electron microscopy (SEM), and spectrometric analysis of material and weldment. (2) Mechanical Testing include; hardness testing and Tensile strength determination. (3) Combing piping stress analysis at fracture point (4) Root cause determination and recommendations to avoid reoccurrence of failure. 3.0 Metallurgical Study of Failure 3.1 Spectrometric Analysis The Chemical analysis of the nipple was carried out using an optical emission spectrometer which gave the composition presented in Table 1. Table 1: Chemical Composition of Nipple Body C Cr Ni Si Mn S P Cu Mo 0.31 0.28 0.04 0.25 0.8 0.04 0.035 0.035 0.12 This conforms to ASTM A105. 3.2 Metallographic Analysis The fractured Heat affected zone (HAZ) of the reducer nipple of the pipe linking the propylene gas tank and the cracked weld joint in the by-pass line were prepared for metallography in accordance with ASTM E3, methods of preparation of metallographic specimen. The three samples were then observed under metallurgical 34
  • 2. Journal of Natural Sciences Research www.iiste.org ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online) Vol.2, No.3, 2012 microscope and the resulting micrographs are presented in figures 3 and 4. The grain sizes of the samples were also determined in consonance with the requirement of ASTM E 112. Discussion of Micrographs The micrograph of the reducer nipple of the propylene gas tank presented in figure 3 revealed that the nipple has a coarse grained ferrite-pearlite microstructure with ASTM grain size number 4 to 6. The variation in grain size depicts in homogeneity in the microstructure. The micrograph of the weldment (valve end of nipple) in figure 4 however revealed homogenous structure of pearlite in ferrite matrix with ASTM grain size number between 9 and 10. This micrograph also shows porosities on the weldment. 3.3 SEM Analysis Samples from, reducer nipple of the propylene gas tank and the valve end of the nipple were subjected to SEM fractography using JEOL JSM-6390LV scanning electron microscope. In the course of the SEM fractography, several shots were taken at different points on each of the mounted samples at magnification of x300, x500 and x700. The resultant fractographs are presented in figures 5 though 10. Discussion of SEM Fractographs The fractographs of the nipple revealed the three-dimensional nature of the various grains which is typical of integranular brittle fracture as opined in Davis(1998). It also revealed fatigue striations characteristic of fatigue failure. The presence of an isolated tear in figure 8 shows the weldment is tougher than the body of the nipple. 4.0 Mechanical Test 4.1 Micro hardness Test The samples of the reducer nipple of A propylene tanks were subjected to micro microhardness test using Leco microhardness tester LM 700AP, applying a load of 50gf in a dwell time of 15 seconds. The test was carried out in accordance with ASTM standard E92, standard test method for Vickers hardness of metallic materials and ASTM E384, standard test for microhardness of materials. The result of the test is presented in table. Table 2 : Microhardness Test Result of Reducer Nipple VHN VHN VHN Average Deviation Range Converted VHN to BHN Nipple Body 122.3 129.3 117.8 123.1 5.7 11.5 116 Weldment 152.4 168.4 166.5 162.4 8.7 16.0 150 Discussion The high values of the deviation in the hardness of the three points taken in each of the sample shows in- homogenity in the microstructure of the flange. 4.2 Tensile Strength of materials The tensile strength = KxBHN Mpa [Rao (1998)] Where k = 3.296 for allow steel and 3.342 for plain carbon steel. For the nipple body, tensile strength = 3.296 x 1.6 = 382.Mpa For the weldment, Tensile strength = 23.342 x 150 = 501.3Mpa 5.0 Stress Analysis of Failed Reducer Nipple 5.1 Determination of the maximum allowable pressure (Design pressure) Data: Nominal outside diameter, D = 0.885in Nominal inside diameter, d = 0.55in 35
  • 3. Journal of Natural Sciences Research www.iiste.org ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online) Vol.2, No.3, 2012 Mean diameter Dm = 0.7175in Operating Temperature = 75 – 80oC (167 – 176F) Material of pipe = ASTM A 105 Designation: Similar to API 5L GR B Operating pressure = 32kg/cm2 = 456.7psi The maximum allowable pressure is determined in accordance with ANSI/ASME B31.8 standard for Gas Transmission and Distribution system by the equation. P = (2 St/D) x F x E x T 5.1 Where, P = Design pressure, (psi) S = Specified minimum yield strength (psi) t = Nominal wall thickness (in) D = Nominal outside diameter (in) F = Design factor E = Longitudinal joint factor T = Temperature de-rating factor. S = 35,000psi [ANSI/ASME Code B31-8-2003, Appendix D] t = 0.157IN D = 2.357in F = 0.72 [ANSI/ASME Code B 31-8-2003 Table 841.1A] E = 1.00 [ANSI/ASME Code B 31-8-2003 Table 841.1B] T = 1.00 [ANSI/ASME Code B 31-8-2003 Table 841.1C] Therefore Design pressure, P = (2 x 35,000 x 0.0.167 ÷ 0.885) x 0.72 x 1.00 x 1.00 = 9510.5Psi = 670kg/cm2 5.2 Determination of the collapsing pressure of pipe The collapsing pipe pressure is determined, taking into consideration the effect of lateral contraction by the DNV equation. 5.2 [Antaki (2005)] Where Pc = minimum net collapsing pipe pressure (psi) 6 Ey = modulus of elasticity = 28 x 10 psi t = pipe thickness = 0.167in Dm = Mean diameter of pipe = 0.7175in λ = Poisson ration = 0.29 Therefore, collapsing pipe pressure, 5.3 Determination of Maximum allowable net external pressure for pipe with eccentricity (1% out-of- roundness) 36
  • 4. Journal of Natural Sciences Research www.iiste.org ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online) Vol.2, No.3, 2012 [Yong Bai and Qiang Bai (2005)] Where Pe = maximum allowable net external pressure Pc = critical value of collapsing pressure S = yield stress allowable stress value. = 30,250 psi [ANSI/ASME code B31-4-2006, Table 402.3.1(a) Pe2- 475,510.81Pe +4,819,308,354 = 0 Pe=10,360.8psi=729.9Kg/cm2 5.4 Hoop Stress (Sh) Analysis Sh = (Pe – Pi) (D – t)/2t 5.4 = (10,360.8 – 456.7) (0.885 – 0.167)/2 x 0.167 = 21,289psi Hoop stress criterion of ABS (2000) according to Yong Bai and Qiang Bai (2005) is given by = Sh < F x S x T = 0.72 x 35000 x 1 = 25200 The hoop stress for the pipe is therefore appropriate since it is less than the value obtained from the criterion. 6.0 Conclusion / Root Cause of Failure (1) The nipple failed by brittle fracture, the cracks being mainly intergranular in nature. (2) The fatigue striation in the SEM fractography revealed the fracture mechanism as fatigue. (3) The grain size variation of the nipple shows in-homogeneity of the coarse microstructure. (4) Failure of the reducer nipple of a propylene gas tank as a result of vibration induced fatigue enhanced by the non-homogeneity of its microstructure. 7.0 Recommendations Irrespective of the accompanying certificate, it is advised that new nipples to be installed be subjected to in-house normalizing heat treatment at 910oC for 30 minutes as this will go a long way in improving the homogeneity of its microstructure. Acknowledgement The author is grateful to Engineering Materials Development Institute Akure, Nigeria and the University of Legon, Ghana for providing the equipment used for this work. REFERENCES 1) ANSI/ASME B31.8 Standard for Gas Transmission and Distribution, ASTM International., USA, 2003. 2) ANSI/ASME B31.4 Pipeline Transportation Systems for Hydrocarbon and other liquids, p9, ASTM International., USA, 2006. 3) Antaki, G.A. (2003), Piping and Pipeline Engineering, Marcel Dekker, Inc, New York. 4) ASTM E3 – 01 Standard Guide for Preparation of Metallographic Specimens, ASTM International, West Conshohocken, PA, 2004. 5) ASTM E112-10 Standard Test Method for Determining Average grain size, ASTM International., USA, 2010. 6) Davis, J.R. (1998), Principles and Procedures of Fractography in Metals Handbook, Desk Edition, 2nd Edition, ASM International, pp 1238-1247. 7) Rao, P.N. (1998), Manufacturing Technology, McGraw Hill Publisher. 8) Yong Bai and Qiang Bai (2005),Subsea Pipelines and Risers, Elsevier Inc, USA. 37
  • 5. Journal of Natural Sciences Research www.iiste.org ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online) Vol.2, No.3, 2012 Figure1: Failed Reducer Nipple Figure 2: Repaired Reducer Nipple Figure 3: Micrograph of reducer nipple, Figure 4: Micrograph of valve end of reducer 2% nital etch x800 nipple, 2% nital etch x400 38
  • 6. Journal of Natural Sciences Research www.iiste.org ISSN 2224-3186 (Paper) ISSN 2225-0921 (Online) Vol.2, No.3, 2012 Fatigue Striation 3-D appearance of grains (Intergranular attack) Figure 5: SEM Fractograph of failed reducer Figure 6: SEM Fractograph of failed reducer nipple, x700 nipple , x300 Cavity Tea r Figure 7: SEM Fractograph of failed reducer Figure 8: SEM Fractograph of failed valve end nipple, x500 (weldment) of nipple, x500 3-D appearance of grain (intergranular attack) 3-D appearance of grain Fatigue (intergranular attack) Striatio Figure 9: SEM Fractograph of failed valve end Figure 10: SEM Fractograph of failed valve end (weldment) of nipple, x700 (weldment) of nipple, x300 39
  • 7. This academic article was published by The International Institute for Science, Technology and Education (IISTE). The IISTE is a pioneer in the Open Access Publishing service based in the U.S. and Europe. The aim of the institute is Accelerating Global Knowledge Sharing. More information about the publisher can be found in the IISTE’s homepage: http://www.iiste.org The IISTE is currently hosting more than 30 peer-reviewed academic journals and collaborating with academic institutions around the world. Prospective authors of IISTE journals can find the submission instruction on the following page: http://www.iiste.org/Journals/ The IISTE editorial team promises to the review and publish all the qualified submissions in a fast manner. All the journals articles are available online to the readers all over the world without financial, legal, or technical barriers other than those inseparable from gaining access to the internet itself. Printed version of the journals is also available upon request of readers and authors. IISTE Knowledge Sharing Partners EBSCO, Index Copernicus, Ulrich's Periodicals Directory, JournalTOCS, PKP Open Archives Harvester, Bielefeld Academic Search Engine, Elektronische Zeitschriftenbibliothek EZB, Open J-Gate, OCLC WorldCat, Universe Digtial Library , NewJour, Google Scholar