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OBJECTIVES
Develop structural analysis blast load cases for multiple explosion scenarios
that account for directionality of the pressure wave front as well as the near
field/far field variation of overpressure relative to defined ignition points.
INPUT DATA
1. SACS model to be blast loaded
2. A “saclst” file containing the SACS model sections, grups, members, plates
and joints data
3. Design blast overpressure, specified 3D Blast ignition points & selected
overpressure distribution function (2 types available)
4. Module deck elevations and deck covering type (plated or grated)
5. Member & Plate drag/pressure coefficients
OUTPUT
1. Module sacinp file with (up to 5) generated blast load cases for
standalone module blast analysis (including input to progressive collapse
analysis)
2. Overpressure display for each generated blast load case (as illustrated on
Slide 2) that is viewable in SACS/Precede.
LEVEL OF EFFORT – half a day per model after initial input gathered
MCHTM Inc
RAPID BLAST LOAD DEVELOPMENT
for Preliminary Design
(or a Poor Man’s Blast Load generation when
sophisticated programs such as USFOS are not in
the project budget)
SUPPORTING 3rd PARTY SOFTWARE
At present, the system has been implemented to
work with SACS input files but could be adapted
to work with other software.
Result for Blast due to Explosive
Device (unmodified Eq 8)
Result for Blast due to Jet fire passing through
Hydrocarbon Cloud (modified Eq. 8)
660 kPa
222 kPa
15 kPa
22 kPa
52 kPa
20 kPa
In these examples,
1. Assumed basis for overpressure distribution function is
Eq 8 in Report EUR 26456 EN, “Calculation of Blast Loads
for Application to Structural Components”.
2. 70 kPa is the specified global overpressure in both cases
BLAST OVERPRESSURE CALCULATION (Two options)
High near-field & low far-field overpressures (as
expected based on API RP 2FB, Appendix C.6.9. 1
(TNT Equivalent Method)
Lower near-field & higher far-field
overpressures when compared to
“explosive device” case
227 kPa
136 kPa
43 kPa
49 kPa
69 kPa
47 kPa
Deck outline
(typical)
Method:
Assume an overpressure distribution function and
scale the calculated overpressures to average out
to be the module global overpressure provided in
a Probabilistic Explosion Analysis report.
MCHTM Inc
To determine Blast
Loads, these
overpressures are
projected onto
modelled member &
plate local axes and
multiplied by the
appropriate pressure
coefficients
OVERALL CONCLUSION:
1. Assuming explosive device blast load is perhaps
overly conservative for near-field structure in O&G
facilities.
2. Hydrocarbon blast load generated with the method
reported here is more in line with API RP 2FB advice
3. Consider not optimizing supporting structure of
plated deck in cases where specified global
overpressures are high
Blast due to explosive device
vs Blast in hydrocarbon cloud
initiated by a jet fire
Hydrocarbon Blast in a Compression
Module – Single ignition point between
2nd & 3rd Deck Levels
(Average overpressure = 0.7 bar)
Initially “Failed” members (shown in
“Orange”) are at Levels 2 & 3 only
MCHTM Inc
Progressive Collapse Analysis Summary following
Explosion due to Explosive Device in Compression Module
Iter ID OO 8A 8B 8C
Iter Seq ID 1 2 3 4
#off members 367 367 367 367
#off memb failures 58 63 65 65
#off deactiv membs 0 0 0 0
#off new memb failures this iteration 58 63 65 65
Note: No plate element failures
Progressive Collapse Analysis Summary following
Hydrocarbon Cloud Explosion in Compression Modile
Iter ID OO 8A 8B 8C
Iter Seq ID 1 2 3 4
#off members 367 367 367 367
#off memb failures 53 61 65 64
#off deactiv membs 0 0 0 0
#off new memb failures this iteration 53 61 65 64
Note: No plate element failures
Hydrocarbon
Cloud Blast
PROGESSIVE COLLAPSE ANALYSIS COMPARISON
Initially “Failed” members (shown in
“Orange”) include two supports
Explosive
Device
Blast
Progressive Collapse Analysis History
Progressive Collapse Analysis History
Note on the Progressive Collapse Analyses:
1. Structure stabilizes after 3 iterations in both
cases considered here though there are more
initial failures in the “explosive device” case.

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Inp toblastloadlinkedinpost 2feb18

  • 1. OBJECTIVES Develop structural analysis blast load cases for multiple explosion scenarios that account for directionality of the pressure wave front as well as the near field/far field variation of overpressure relative to defined ignition points. INPUT DATA 1. SACS model to be blast loaded 2. A “saclst” file containing the SACS model sections, grups, members, plates and joints data 3. Design blast overpressure, specified 3D Blast ignition points & selected overpressure distribution function (2 types available) 4. Module deck elevations and deck covering type (plated or grated) 5. Member & Plate drag/pressure coefficients OUTPUT 1. Module sacinp file with (up to 5) generated blast load cases for standalone module blast analysis (including input to progressive collapse analysis) 2. Overpressure display for each generated blast load case (as illustrated on Slide 2) that is viewable in SACS/Precede. LEVEL OF EFFORT – half a day per model after initial input gathered MCHTM Inc RAPID BLAST LOAD DEVELOPMENT for Preliminary Design (or a Poor Man’s Blast Load generation when sophisticated programs such as USFOS are not in the project budget) SUPPORTING 3rd PARTY SOFTWARE At present, the system has been implemented to work with SACS input files but could be adapted to work with other software.
  • 2. Result for Blast due to Explosive Device (unmodified Eq 8) Result for Blast due to Jet fire passing through Hydrocarbon Cloud (modified Eq. 8) 660 kPa 222 kPa 15 kPa 22 kPa 52 kPa 20 kPa In these examples, 1. Assumed basis for overpressure distribution function is Eq 8 in Report EUR 26456 EN, “Calculation of Blast Loads for Application to Structural Components”. 2. 70 kPa is the specified global overpressure in both cases BLAST OVERPRESSURE CALCULATION (Two options) High near-field & low far-field overpressures (as expected based on API RP 2FB, Appendix C.6.9. 1 (TNT Equivalent Method) Lower near-field & higher far-field overpressures when compared to “explosive device” case 227 kPa 136 kPa 43 kPa 49 kPa 69 kPa 47 kPa Deck outline (typical) Method: Assume an overpressure distribution function and scale the calculated overpressures to average out to be the module global overpressure provided in a Probabilistic Explosion Analysis report. MCHTM Inc To determine Blast Loads, these overpressures are projected onto modelled member & plate local axes and multiplied by the appropriate pressure coefficients
  • 3. OVERALL CONCLUSION: 1. Assuming explosive device blast load is perhaps overly conservative for near-field structure in O&G facilities. 2. Hydrocarbon blast load generated with the method reported here is more in line with API RP 2FB advice 3. Consider not optimizing supporting structure of plated deck in cases where specified global overpressures are high Blast due to explosive device vs Blast in hydrocarbon cloud initiated by a jet fire Hydrocarbon Blast in a Compression Module – Single ignition point between 2nd & 3rd Deck Levels (Average overpressure = 0.7 bar) Initially “Failed” members (shown in “Orange”) are at Levels 2 & 3 only MCHTM Inc Progressive Collapse Analysis Summary following Explosion due to Explosive Device in Compression Module Iter ID OO 8A 8B 8C Iter Seq ID 1 2 3 4 #off members 367 367 367 367 #off memb failures 58 63 65 65 #off deactiv membs 0 0 0 0 #off new memb failures this iteration 58 63 65 65 Note: No plate element failures Progressive Collapse Analysis Summary following Hydrocarbon Cloud Explosion in Compression Modile Iter ID OO 8A 8B 8C Iter Seq ID 1 2 3 4 #off members 367 367 367 367 #off memb failures 53 61 65 64 #off deactiv membs 0 0 0 0 #off new memb failures this iteration 53 61 65 64 Note: No plate element failures Hydrocarbon Cloud Blast PROGESSIVE COLLAPSE ANALYSIS COMPARISON Initially “Failed” members (shown in “Orange”) include two supports Explosive Device Blast Progressive Collapse Analysis History Progressive Collapse Analysis History Note on the Progressive Collapse Analyses: 1. Structure stabilizes after 3 iterations in both cases considered here though there are more initial failures in the “explosive device” case.