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IGCAR : Annual Report - Indira Gandhi Centre for Atomic Research

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IGC<br />

<strong>Annual</strong> <strong>Report</strong> 2007<br />

of core top and absorber rods<br />

and vertical accelerations of<br />

core subassemblies which are<br />

of concern to reactor safety<br />

(Table 1), (2) primary<br />

membrane stress intensities <strong>for</strong><br />

the main vessel and inner<br />

vessel (Table 2) and (3)<br />

generation of high strain<br />

energies at the critical portions<br />

which can enhance the<br />

buckling risks of main<br />

vessel and inner vessel<br />

(Table 3).<br />

In view of increased<br />

displacements, stresses and<br />

strain energies at critical<br />

locations when the reactor vault<br />

is connected with the<br />

remaining structures of NICB,<br />

it is preferable to isolate the<br />

reactor vault, by directly<br />

constructing it from the base<br />

raft without inter-connecting it<br />

with the adjacent buildings of<br />

NICB, from the seismic loading<br />

considerations. This also<br />

provides some flexibility to<br />

design and analyse the reactor<br />

assembly components<br />

independently without linking to<br />

the finalisation of design of rest<br />

of the civil structures. This can<br />

be adopted <strong>for</strong> future FBRs.<br />

III.A.2. Modal Analysis of PFBR Fuel Subassembly<br />

PFBR Fuel subassembly (FSA)<br />

consists of 217 fuel pins held<br />

vertically in the <strong>for</strong>m of a<br />

bundle within a hexagonal<br />

wrapper tube. Flow induced<br />

vibrations (FIV) in FSA is a<br />

potential cause <strong>for</strong> fatigue,<br />

wear and vibration induced<br />

fretting in the subassembly<br />

parts which can lead to<br />

reactivity noise and premature<br />

failure of fuel pins and other SA<br />

parts. The coolant flow in SA is<br />

in highly turbulent regime and<br />

it can cause flow-induced<br />

vibration of fuel pins and FSA<br />

as a whole. The overall<br />

subassembly vibration will be in<br />

its cantilever mode. The SA<br />

vibration will also depends<br />

upon the sodium exit velocity,<br />

restraints at the supports in the<br />

grid plate and the buttons and<br />

the interaction of the discharge<br />

coolant jets with control plug<br />

parts positioned above the<br />

subassembly as well as with<br />

surrounding subassembly jets.<br />

As part of the FIV<br />

experimental program on FSA,<br />

modal measurements were<br />

carried out on SA in water to<br />

estimate the modal parameters.<br />

Theoretical modelling of FSA<br />

was also done using ANSYS<br />

FEM software to extract the<br />

natural frequencies and mode<br />

Table 1 : Modal frequencies in water<br />

Mode<br />

Case-1<br />

(Hz)<br />

shapes. Beam element was<br />

assigned to discretize the<br />

model and the full SA is divided<br />

in into six sections. In the<br />

analytical modelling, two cases<br />

were taken as support<br />

boundary conditions <strong>for</strong> FSA.<br />

Case 1. Hinged support at<br />

the location where FSA rests on<br />

the sleeve top and simply<br />

supported at the discriminator<br />

location.<br />

Case-2<br />

(Hz)<br />

1 3.7 3.9<br />

2 22.2 24.0<br />

3 64.6 66.2<br />

4 126.0 128.1<br />

5 147.9 149.0<br />

R&D FOR FBRs 27

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