Upload
others
View
4
Download
0
Embed Size (px)
Citation preview
AP1000 is a trademark or registered trademark of Westinghouse Electric Company LLC, its affiliates and/or its subsidiaries in the United States of
America and may be registered in other countries throughout the world. All rights reserved. Unauthorized use is strictly prohibited. Other names
may be trademarks of their respective owners.
Westinghouse Non-Proprietary Class 3
3D LINEAR BIFURCATION ANALYSIS OF STEEL CONTAINMENT VESSEL
Jay Schmidt Westinghouse Electric Company
Cranberry Twp, PA, USA
Dr. Bernd Laskewitz Westinghouse Electric Company
Cranberry Twp, PA, USA
ABSTRACT The AP1000
® Containment Vessel (CV) is a freestanding steel
containment designed to protect the public from radiation
release. The CV consists of 2 ellipsoidal heads connected by a
cylindrical shell and is constructed of carbon steel. The
AP1000 plant design has four large penetrations (two airlocks
and two equipment hatches) located in approximately the same
quadrant of the circumference of the shell which imposes
asymmetric effects in the shell structure. The CV is designed
and constructed in accordance with ASME Boiler and Pressure
Vessel Code, Section III, Subsection NE.
Traditionally, the local and global stability of freestanding steel
containments have been designed by use of formulae using
conservative assumptions based on an axisymmetric structure.
ASME Code Case N-284 “Metal Containment Shell Buckling
Design Methods, Class MC Section III, Division 1” outlines
methodology for satisfying the stability of the CV using two
approaches. Section 1710 provides a stress based buckling
approach using detailed formulae that assumes an axisymmetric
structure. The second approach provides guidance and
acceptability based on a linear bifurcation analysis (2D (1720)
or 3D (1730)). Due to the asymmetric structure of the CV, the
3D linear bifurcation method delivers the most accurate results.
The methodology and assumptions implemented by
Westinghouse to qualify stability of the CV via Code Case N-
284 are outlined. Also, the procedure to properly amplify the
stresses as required by N-284 is included as justification of the
methods used. This justification was thoroughly investigated by
the Nuclear Regulatory Commission (NRC) and deemed
acceptable.
INTRODUCTION The primary purpose of a nuclear power plant containment
vessel is to act as the final line of defense for radiation release
to the public. Previous generations of nuclear power plants
utilized concrete containments using steel liner plates on the
inside. The AP1000 plant CV is a free standing steel
containment vessel. A reason for this is the role the CV plays in
the passive cooling technology that is unique to the AP1000
plant design.
The AP1000 plant CV and other freestanding containments or
similarly shaped pressure vessels are susceptible to buckling
concerns. Large portions of unsupported sections of the CV
shell are areas most prone to large compressive stresses and
therefore of particular concern in this analysis.
Criteria for the AP1000 plant CV are taken from the American
Society of Mechanical Engineers (ASME) Boiler Pressure
Vessel Code (BPVC), Section NE, 2001 with 2002 Addenda.
This year of the code is the year used for licensing of the
AP1000 plant CV. The NE-3000 Article of this code details
design and qualification of the CV. Buckling criteria is also
contained in section NE-3000. The buckling rules outlined in
NE-3133 do not cover all geometries of pressure vessels and do
not provide reasonable safety margins. Non-uniform
compressive stresses are also not accounted for in NE-3133.
Because of these reasons, an ASME task force was created to
develop rules for the design of CVs under compressive stress
scenarios. More refined analysis based on testing and detailed
research of pressure vessel buckling led to Code Case N-284
“Metal Containment Shell Buckling Design Methods, Class
MC Section III Division 1”. Revision 1 of this code case is
used in the AP1000 plant licensing basis and the major
supporting criteria for the CV buckling analysis.
Proceedings of the 2016 24th International Conference on Nuclear Engineering ICONE24
June 26-30, 2016, Charlotte, North Carolina
ICONE24-60673
1 Copyright © 2016 by ASME
CODE CASE N-284-1 Scope and Analysis Methods
The following text is taken directly from Section 1110 of N-
284-1 to provide overall scope of the code case: “The purpose
of this case is to provide stability criteria for determining the
structural adequacy against buckling of containment shells with
more complex shell geometries and loading conditions than
those covered by NE-3133. Such effects as symmetrical or
unsymmetrical dynamic loading conditions, circumferential
and/or meridional stiffening for heads as well as cylindrical
shell, combined stress fields, discontinuity stresses and
secondary stresses are considered in the stability evaluation.”
Code Case N-284-1 outlines the qualification guidelines for
three different analysis methodologies and the required
procedure for each. The three methods can be separated into
two sub groups. The first being a stress based analysis using
interaction equations and the second being a finite element
linear bifurcation analysis. The linear bifurcation analysis can
be 2D or 3D. The 3D linear bifurcation analysis was chosen for
qualification of the AP1000 plant CV.
The stress based method and the 2D linear bifurcation analysis
are designed for axisymmetric structures. The 2D analyses do
not have the ability to capture the seismic response of the
AP1000 plant large penetrations (two personnel airlocks, and
two equipment hatches). Large dynamic loadings that are not
symmetric to the overall CV structures could lead to additional
buckling concerns. The 3D linear bifurcation analysis is able to
investigate the impact of the large penetrations to the CV
stability.
ANSYS Finite Element Analysis Models
Two detailed 3D ANSYS Finite Element (FE) models were
created for use in the stability assessment of the CV. The two
models were the same with one exception. The mesh size
varied between the two models. The first model had a mesh
size of 37 inches and the second mesh size was 18.5 inches.
Eight-node structural shell elements (Shell93) were used in the
analysis and the two final models can be seen in Figures 1 and
2 below.
The bottom ellipsoidal head is not explicitly modeled. The
bottom head is encased in concrete on both sides. For
simplicity the bottom of the ANSYS FE models are considered
fixed in all six degrees of freedom (three translations and three
rotations). In reality the CV bottom head would be able to slide
and rotate and would not act as a fixed boundary. For the
purpose of this analysis the assumed boundary condition is
conservative.
FIGURE1. AP1000 CV Model (Coarse Mesh)
FIGURE 2. AP1000 CV Model (Fine Mesh)
2 Copyright © 2016 by ASME
N-284-1 Analysis Procedure
The following steps are provided in Page 26 of N-284-1. This
is a high level procedure. More detailed information required to
complete the tasks outlined are discussed in greater detail in the
following sections.
1) Perform a static analysis of the basic loads and obtain
, , and .
2) Multiply the stresses by the Factor of Safety (FS) for
the corresponding Service Limit.
3) Calculate the capacity reduction factor ij for local and
general buckling.
4) Calculate any applicable plasticity reduction factors
i.
5) Compute amplified stresses for the imperfect is by
dividing the elastic stress by the capacity reduction
factors calculated in Step 3.
6) Divide the elastic stress components by the proper
plasticity reduction factors to obtain the amplified
inelastic stress component ip. If I is equal to 1, then
is = ip.
7) Apply amplified stresses to the FEA model and
perform eigenvalue buckling analysis*
Note*: ANSYS does not have a function that allows the
mapping of stresses onto the FE model, the loadings were
amplified until the average of the resulting stress components
were amplified to the amount specified by the process outlined
above.
Loading Conditions/ Service Levels
Code Case N-284-1 follows the same service level conditions
as NE-3000 because they are both used in the design and
qualification of MC components. Types of loadings (thermal,
seismic, pressure, etc.) were coupled together based on
applicable service loading conditions. Investigations of all
service loading conditions yielded two that would be the most
limiting case for buckling. These two cases consisted of
loadings, when applied simultaneously, would lead to
compressive stresses over unstiffened portions of the shell. The
applicable service levels investigated are shown in Table 1.
TABLE 1: Applicable Service Levels
Service Level Loadings
Design/Level A Dead Load
Pressure Load
(External)
Thermal Load
(Normal Operation
in cold weather)
Level D Dead Load
Pressure Load
(External)
Thermal Load
(Normal Operation
in cold weather)
Vessel Global
Seismic Load
Large Penetration
Seismic Load
Seismic Loadings
Service Level D load condition includes seismic loadings. The
CV is conservatively analyzed using equivalent static
acceleration data to represent the global seismic loading of the
vessel. The accelerations are provided via North-South and
East-West lateral directions as well as a Vertical component.
All components are provided at several elevations from the
bottom to the top of the CV. The values were interpolated
linearly if necessary to get more realistic loadings on
components between datum points. Additionally accidental and
added torque loadings were also applied to areas of the vessel
at the large penetrations. These components consisted of
acceleration in the radial direction (axial direction of the
penetration) and two rotational accelerations. One is about the
horizontal axis and the second is around the vertical axis. The
100-40-40 rule was used to create 21 load combinations to
analyze all permutations of seismic loading. The local
accelerations could act in-phase and out-of-phase with the CV
global seismic loading. To capture this loading possibility and
bound the analysis, four additional cases were created to
encompass all possible deviations of loading. This leads to a
total of 96 load combinations for the Level D evaluation.
Factors of Safety and Capacity Reduction Factors
Section 1400 of N-284-1 provides Factors of Safety (FS) per
service level. They are as follows:
a) For Design Conditions and Level A and B Service
Limits, FS = 2.0
3 Copyright © 2016 by ASME
b) For Level C Service Limits the allowable values are
120% of the values of (a). Use FS = 1.67.
c) For Level D Service Limits the allowable stress values
are 150% of the values of (a) Use FS = 1.34.
Section 1500 of N-284-1 provides guidelines for the Capacity
Reduction Factors per service level and is dependent upon what
type of geometry, loading direction, local/general buckling, etc.
Local buckling is defined as the buckling of the vessel shell
between stiffeners. The general buckling refers to an overall
collapse of the system. The capacity reduction factors used in
the evaluation are given below. Equations (1) and (2) correlate
to local buckling for axial and hoop loads respectively.
Equations (3) and (4) are the axial and hoop capacity reduction
factors for general instability, respectively. In order to solve
Equation (3), Equation 5 is needed.
t
RL 10: log473.052.1 (1)
80.0L (2)
LLG A
__
0.56.3 (3)
LG (4)
084.0
__
tl
AA
s
(5)
Where: L = Axial capacity reduction factor for local
buckling
L = Hoop capacity reduction factor for
local buckling
G = Axial capacity reduction factor for
general instability
G = Hoop capacity reduction factor for
general instability
R = the radius of the CV
t = the thickness of the CV shell
A = Cross sectional area of internal stiffener
ls = Length between stiffeners
Based on the mid-surface radius and thickness of the SCV, the
axial knockdown factor was calculated to be 0.267 and 0.457
for local buckling and general instability, respectively. The
hoop capacity reduction factor is defines as 0.8 for both local
and buckling and general instability.
For both Service Level A and D conditions, the external
pressure is a governing load. This loading also acts differently
on the structure, than dead weight, seismic, or thermal loadings.
The amplification of these loadings is accomplished via the
factors calculated in Equations (6) and (7) for hoop and axial
effects, respectively. The remaining load types are
conservatively amplified using the axial capacity reduction
factors shown in Equation (8).
L
extextshell
FSPP
_ (6)
L
extextTP
FSPP
_ (7)
L
iamplified
FSLL
(8)
Where: Pshell_ext = Amplified external pressure on the
side of the CV
PTP_ext = Amplified external pressure on the
top head of the CV
Pext = External pressure
Lamplified = Amplified load
Li = PC and CV acceleration loads
FS = Safety factor (2.0 for service Level
A/Design, 1.34 for service level D)
Two cases were created in ANSYS and compared. The first
with loadings as provided by the design specification
(unamplified) and the second with load amplification factors
calculated using Equations (6) - (8) applied to the FE model
(amplified). The resultants stress components were compared to
assure that the correct amplification occurred.
Thermal loading amplification is accomplished by increasing
the rate of thermal expansion. The axial amplification factor
calculated is multiplied to the original or base expansion
coefficient creating a higher rate of expansion which yields
higher stresses. These stresses were also checked for proper
amplification levels and were found to be correct.
ANALYSIS RESULTS
Table 4 shows the resulting Eigenvalues calculated for each
load combination. One combination exists for Design/Service
Level A and 96 combination results for Service Level D.
4 Copyright © 2016 by ASME
TABLE 4: Eigenvalues for Local and Global Instability
x
y z
Lev
el A
1/D
es2
Lev
el D
1 L
oca
l N
eg N
eg
Lev
el D
1 G
lob
al
Neg
Neg
Lev
el D
1 L
oca
l N
eg P
os
Lev
el D
1 G
lob
al
Neg
Po
s
Lev
el D
1 L
oca
l P
os
Neg
*
Lev
el D
1 L
oca
l P
os
Po
s*
1.44
0.4 0.4 1 1.75 2.21 1.70 2.18 1.65 1.61
-0.4 0.4 1 1.64 2.14 1.69 2.18 1.69 1.71
0.4 0.4 -1 1.62 2.13 1.61 2.10 1.78 1.78
-0.4 0.4 -1 1.63 2.16 1.57 2.14 1.79 1.80
0.4 1 0.4 1.17 1.73 1.18 1.70 1.33 1.29
-0.4 1 0.4 1.17 1.71 1.15 1.70 1.31 1.37
0.4 1 -0.4 1.15 1.71 1.16 1.68 1.39 1.39
0.4 -0.4 1 1.72 2.20 1.71 2.22 1.62 1.66
0.4 -0.4 -1 1.60 2.12 1.56 2.11 1.79 1.80
-0.4 1 -0.4 1.14 1.71 1.12 1.68 1.38 1.42
-0.4 -0.4 1 1.66 2.15 1.61 2.11 1.71 1.67
-0.4 -0.4 -1 1.61 2.15 1.65 2.13 1.81 1.80
0.4 -1 0.4 1.17 1.72 1.14 1.69 1.29 1.33
-0.4 -1 0.4 1.17 1.70 1.16 1.67 1.34 1.31
0.4 -1 -0.4 1.15 1.69 1.12 1.67 1.39 1.40
-0.4 -1 -0.4 1.14 1.71 1.16 1.68 1.42 1.40
1 0.4 0.4 1.20 1.80 1.22 1.77 1.45 1.41
-1 0.4 0.4 1.23 1.78 1.17 1.78 1.45 1.45
1 0.4 -0.4 1.16 1.77 1.18 1.75 1.54 1.51
-1 0.4 -0.4 1.19 1.78 1.14 1.74 1.54 1.52
1 -0.4 0.4 1.18 1.78 1.16 1.75 1.39 1.42
-1 -0.4 0.4 1.18 1.78 1.20 1.76 1.41 1.38
1 -0.4 -0.4 1.14 1.73 1.12 1.70 1.49 1.53
-1 -0.4 -0.4 1.14 1.74 1.17 1.77 1.51 1.47
5 Copyright © 2016 by ASME
* Global buckling analyses were not performed for load cases
in which the Eigenvalue exceeds 1.2 in the local buckling
analyses.
Note: The 1st “Negative” or “Positive” in the load cases
description refers to the applied global seismic acceleration
direction compared to the global coordinate system. The 2nd
“Negative” or “Positive” refers to the applied equivalent static
forces due to seismic acceleration of the large penetrations
according to their local coordinate systems. This approach is
extremely conservative since it combines in-phase and out-of-
phase movements of the shell and other seismic loadings.
Figures 3 and 4 below show the deformed shape of the critical
case of this analysis. Figure 3 shows the CV model from an
elevation view and Figure 4 shows the CV from the top as a
plan view. The buckling waves can be seen in the vicinity of
the shell away from the large penetrations but at similar
elevations.
FIGURE 3. Critical Eigenmode (Elevation View)
FIGURE 4. Critical Eigenmode (Plan View)
CONCLUSION
The stability of the Containment Vessel for all appropriate load
combinations per ASME NE-3000 are found to be within the
allowable values of ASME Code Case N-284-1. The lowest
Eigenvalue for local buckling is 1.12 (allowable > 1.0). For
global buckling, the lowest Eigenvalue is 1.67 (allowable
>1.2). Considering loading conditions that would add yield
compressive stresses in the vessel cylindrical wall, the overall
stability and the local buckling capacities are met with
conservative loading conditions applied.
REFERENCES
Laskewitz, B.R. and Schmidt J.E., (2011). APP-GW-GLR-
005, Rev 5. “Containment Vessel Design Adjacent to
Large Penetrations.
CASES OF ASME BOILER AND PRESSURE VESSEL
CODE: Case N-284-1 “Metal Containment Shell
Buckling Design Methods, Class MC Section III,
Division 1. March 14, 1995.
ASME Section III “Rules for Construction of Nuclear Power
Plant Components, Division 1 Subsection NE, Class MC
Components”, 2001 Edition with 2002 Addenda.
6 Copyright © 2016 by ASME