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Plastic Collapse Behaviors of Perforating Guns with ScallopsHaifeng Zhao, David Iblings, Aleksey Barykin, and Mohamed MehdiSchlumbergerMay 9-11, 2016, Galveston, TX
2016 International Perforating Symposium (IPS) IPS-16-39
22
Outline
I. Introduction to Perforating Gun and Conveyance Systems
II. Ultimate Collapse Strength for Recessed Tubulars
III. Finite Element Analysis (FEA) and Test Validation
IV. Conclusions and Future Work
2
33
I. Introduction to Perforating Gun and Conveyance Systems
3
44
Slickline Coiled Tubing
Wireline Tubing-Conveyed Perforating (TCP): Completions and Drillstem testing
Open-string TCP system
Perforating Gun and Conveyance Systems
4
55
Density and Phasing
Distance (in degrees) between charges
PhasingDensity
Number of shots per foot (spf)
360°/ 6 =60° phasing
1 ft
5
66
II. Ultimate Collapse Strength for Recessed Tubulars
6
77
Review: Collapse Strength of a Slick Pipe§ Lamé Thick Wall Yield Collapse Formula (Yield at Pipe ID)
§ API Bulletin 5C3
§ Tamano Ultimate Collapse Equation (SPE 48331)
𝑃"# = 𝜎&𝐷() − 𝐷+
)
2𝐷()Open Ends
Closed Ends 𝑃"# = 𝜎&𝐷() − 𝐷+
)
3𝐷()
𝐷( = 𝐷
𝑡 =12𝐷( − 𝐷+
𝑘 = 𝐷 𝑡⁄
𝑃"# = 2𝜎& 2𝑘 − 1𝑘)
𝑃"# = 2.31 2 𝜎& 2𝑘 − 1𝑘)
𝑃45 = 2𝜎& 2𝑘 − 1𝑘)
Yield Collapse
𝑃6 = 𝜎&𝐴𝑘 −𝐵 −𝐶
Plastic Collapse
𝑃: = 𝜎&𝐹𝑘 −𝐺
Transition Collapse
𝑃:= =2𝐸
1− 𝑣) 21
𝑘 𝑘 − 1 )
Elastic Collapse
𝑃: =12 𝑃= +𝑃4 −
14 𝑃= −𝑃4 )+ 𝑃=𝑃4𝐻
𝑃= = 1.08×2𝐸
1 − 𝑣)2
1𝑘 𝑘 −1 )
𝑃4 = 2𝜎& 2𝑘 − 1𝑘)
1 +1.5𝑘 −1
𝐻 = 0.071 2 𝑢 % + 0.0022 2 𝑒 % − 0.18 2𝜎K𝜎&
7
88
Ultimate Collapse Strength of Scalloped Gun Carriers
𝑃# = 𝜇 2 𝑃:𝜇 – Collapse strength reduction factor due to scallops𝑃: – Tamano ultimate collapse strength equation
𝝁𝑃:𝑃#
Definition
Slick PipeRecessed PipeCollapse strength reduction factor
8
99
Reference: Collapse Strength of Perforated Casing
𝜇N = 1 −𝑑𝑆
Reference: SPE 51188
𝑑 𝑆⁄ – (1D) spacing fraction of recess3D representation
d
s
Cross-section view
9
1010
𝜇 for Scalloped Gun Carriers
𝜇Q = 1−𝑑𝑆 2ℎ𝑡
𝜇) = 1 − 𝑓K
𝜇T = 1 −𝛼𝑓K
𝑓K – (3D) volume fraction of recess𝛼 – fitting factor
h
td
Cross-section view 3D representation
sV×WX×Y
– (2D) area fraction of recess
10
1111
III. FEA and Test Validation
11
1212
Modeling ApproachDescriptionØ Nonlinear post-buckling analysis using Riks method based on
arc length scheme in ABAQUSØ Material model: isotropic hardening plasticity with bilinear,
power law or measured stress-strain curveØ Boundary conditions: external pressure prescribed on the
exterior surface with end connection supported
Collapse CriteriaØ When the collapse pressure is reached, the structure will deform dramatically and lose pressure-bearing
capacity.
Local Yielding
12
1313
Physical Understanding of Collapse (Post-buckling)
0 0.05 0.1 0.15 0.2 0.25 0.30
0.2
0.4
0.6
0.8
1
1.2
U/D
P/P m
ax
Collapse
P3
P1
P2
-3 -2 -1 0 1 2 30
0.05
0.1
0.15
0.2
0.25
0.3
x/S
U/D
CollapseP1P2P3
Collapse pressure definition
13
1414
Example: Collapse Animation of 15SPF 5 FT
Deformation Scale Factor = 1
14
1515
Test Validation of FEA
Description Test Temp [Deg F]
D/t Tested Collapse Pressure
[psi]
FEA𝑷𝒄𝒐𝒍𝒍𝒂𝒑𝒔𝒆
[psi]
Differencewith Tests [%]
Test 1 368 9.4 32,250 30,660 -4.9%Test 2 318 10.7 22,500 22,831 +1.5%Test 3 250 10.7 24,263 23,651 -2.5%Test 4 250 14.0 18,329 18,633 +1.7%Test 5 400 11.6 22,745 23,311 +2.4%
Note: • Detailed geometric, product name and material parameters are confidential.• Stress/strain data utilized in the FEA analyses is full measured data from a test
15
1616
Case Study: 𝜇) Expression
𝜇) = 1 − 𝑓K = 1 − 90 2𝑑)
𝑆𝐷𝜃 2ℎ𝑡
𝑓K = 𝑉5 𝑉e⁄𝑉e = 𝑆×
𝜋180𝜃𝐷×𝑡
𝑉5 = 2×14𝜋𝑑
)ℎ
16
17
Case Study: Parametric Study of 7-in OD, 5-ft Length Carrier
17
D [in] t [in] θ [deg] S [in] w [in] d [in]
70.50.71.0
60 4.0 0.2 1.0
D [in] t [in] θ [deg] S [in] h [in] d [in]
7 0.7
25.736456090
4.0 0.5 1.0
D [in] t [in] θ [deg] S [in] h [in] d [in]
7 0.7 60
4.06.08.012.016.0
0.5 1.0
D [in] t [in] θ [deg] S [in] h [in] d [in]
7 0.7 60 4.0
0.30.40.50.6
1.0
D [in] t [in] θ [deg] S [in] h [in] d [in]
7 0.7 60 4.0 0.50.71.01.3
D [in] t [in]
70.50.71.0
Dimension of slick pipes
Wall Thickness, t
Angular Phasing, θ
Longitudinal Spacing, S
Scallop Depth,h
Scallop Diameter, d
𝜇ghi = 𝑃jklmmnoghi 𝑃opoqghir
Definition of “true” 𝝁
1818
Sensitivity Study of Collapse Strength Reduction Factor
𝜇Q = 1 −𝑑𝑆 2
ℎ𝑡
𝜇) = 1 − 90 2𝑑)
𝑆𝐷𝜃 2ℎ𝑡
[1] 𝐷 𝑡⁄ vs. 𝜇
𝜇T = 1 − 3 2 90 2𝑑)
𝑆𝐷𝜃 2ℎ𝑡
𝜇ghi = 𝑃jklmmnoghi 𝑃opoqghir
6 7 8 9 10 11 12 13 14 150.5
0.6
0.7
0.8
0.9
1
D/t
Col
laps
e St
reng
th R
educ
tion
Fact
or µ
µFEA
µ1
µ2
6 7 8 9 10 11 12 13 14 150.5
0.6
0.7
0.8
0.9
1
D/t
Colla
pse S
treng
th Re
ducti
on F
actor
µ
µFEA
µ1
µ3
Collapse strength reduction factor 𝜇 is linearly proportional to D/t ratio.
18
1919
Sensitivity Study of Collapse Strength Reduction Factor
𝜇Q = 1 −𝑑𝑆 2
ℎ𝑡
𝜇) = 1 − 90 2𝑑)
𝑆𝐷𝜃 2ℎ𝑡
[2] 𝜃 vs. 𝜇
𝜇T = 1 − 3 2 90 2𝑑)
𝑆𝐷𝜃 2ℎ𝑡
𝜇ghi = 𝑃jklmmnoghi 𝑃opoqghir
0 30 60 90 120 150 1800.5
0.6
0.7
0.8
0.9
1
θ [deg]
Col
laps
e St
reng
th R
educ
tion
Fact
or µ
µFEA
µ1
µ2
0 30 60 90 120 150 1800.5
0.6
0.7
0.8
0.9
1
θ [deg]
Colla
pse S
treng
th Re
ducti
on F
actor
µ
µFEA
µ1
µ3
Collapse strength reduction factor 𝜇 is inversely proportional to 𝜃.
19
2020
Sensitivity Study of Collapse Strength Reduction Factor
𝜇Q = 1 −𝑑𝑆 2
ℎ𝑡
𝜇) = 1 − 90 2𝑑)
𝑆𝐷𝜃 2ℎ𝑡
3 𝑆 vs. 𝜇
𝜇T = 1 − 3 2 90 2𝑑)
𝑆𝐷𝜃 2ℎ𝑡
𝜇ghi = 𝑃jklmmnoghi 𝑃opoqghir
2 4 6 8 10 12 14 16 18 20 22 240.5
0.6
0.7
0.8
0.9
1
S [in]
Col
laps
e St
reng
th R
educ
tion
Fact
or µ
µFEA
µ1
µ2
2 4 6 8 10 12 14 16 18 20 22 240.5
0.6
0.7
0.8
0.9
1
S [in]
Colla
pse S
treng
th Re
ducti
on F
actor
µ
µFEA
µ1
µ3
Collapse strength reduction factor 𝜇 is inversely proportional to S.
20
2121
Sensitivity Study of Collapse Strength Reduction Factor
𝜇Q = 1 −𝑑𝑆 2
ℎ𝑡
𝜇) = 1 − 90 2𝑑)
𝑆𝐷𝜃 2ℎ𝑡
[4] ℎ vs. 𝜇
𝜇T = 1 − 3 2 90 2𝑑)
𝑆𝐷𝜃 2ℎ𝑡
𝜇ghi = 𝑃jklmmnoghi 𝑃opoqghir
0 0.1 0.2 0.3 0.4 0.5 0.6 0.70.5
0.6
0.7
0.8
0.9
1
h [in]
Col
laps
e St
reng
th R
educ
tion
Fact
or µ
µFEA
µ1
µ2
0 0.1 0.2 0.3 0.4 0.5 0.6 0.70.5
0.6
0.7
0.8
0.9
1
h [in]
Colla
pse S
treng
th Re
ducti
on F
actor
µ
µFEA
µ1
µ3
Collapse strength reduction factor 𝜇 is “linearly” proportional to h.
21
2222
Sensitivity Study of Collapse Strength Reduction Factor
𝜇Q = 1 −𝑑𝑆 2
ℎ𝑡
𝜇) = 1 − 90 2𝑑)
𝑆𝐷𝜃 2ℎ𝑡
[5] 𝑑 vs. 𝜇
𝜇T = 1 − 3 2 90 2𝑑)
𝑆𝐷𝜃 2ℎ𝑡
𝜇ghi = 𝑃jklmmnoghi 𝑃opoqghir
0 0.3 0.6 0.9 1.2 1.50.5
0.6
0.7
0.8
0.9
1
d [in]
Col
laps
e St
reng
th R
educ
tion
Fact
or µ
µFEA
µ1
µ2
0 0.3 0.6 0.9 1.2 1.50.5
0.6
0.7
0.8
0.9
1
d [in]
Colla
pse S
treng
th Re
ducti
on F
actor
µ
µFEA
µ1
µ3
Collapse strength reduction factor 𝜇 is a quadratic function of d.
22
2323
IV. Conclusions and Future Work
23
2424
Conclusions and Future Work§ An analytical collapse strength equation based on Tamano formula was proposed for scalloped
perforating guns.
§ The proposed equation was thoroughly validated with the aid of FEA in a multivariable parametric space – an analysis hardly affordable with the use of physical tests.
§ An FEA method used to validate the proposed equation showed strong agreement with the test data giving collapse predictions for scalloped tubulars within 5% of the test results.
§ The method applied to scalloped perforating guns can also be used for any tubulars with patterned cutouts or recesses, such as prepacked sand screens, perforated or slotted liners, etc.
24
2525
Questions?
25
Publications
• Zhao, H., Iblings, D., Barykin, A., and Mehdi, M., 2015, Plastic Collapse Behaviors of Tubulars with Recess Patterns, Proceedings of ASME International Mechanical Engineering Congress & Exposition, IMECE2015-‐50204, Houston, TX.
• Zhao, H., Iblings, D., Barykin, A., and Mehdi, M., 2016, Plastic Collapse Behaviors of Tubulars with Recess Patterns, ASCE-‐ASME Journal of Risk and Uncertainty in Engineering Systems, Part B: Mechanical Engineering , Accepted.
IPS-16-39