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Refined Globe Valve Thrust Prediction Model to Bound Midstroke ...

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<strong>Refined</strong> <strong>Globe</strong> <strong>Valve</strong> <strong>Thrust</strong> <strong>Prediction</strong><br />

<strong>Model</strong> <strong>to</strong> <strong>Bound</strong> <strong>Midstroke</strong> <strong>Prediction</strong>s of<br />

AOV Margins<br />

Zachary Leutwyler<br />

Dr. M. S. Kalsi<br />

Kalsi Engineering<br />

Tenth NRC/ASME Symposium on<br />

<strong>Valve</strong>s, Pumps and IST<br />

July 15, 2008<br />

Slide #1 #


• Introduction<br />

Objectives<br />

Background<br />

Two-point Two point thrust prediction model<br />

KEI <strong>Bound</strong>ing <strong>Thrust</strong> Zone (BTZ) <strong>Model</strong><br />

• KEI Flow Loop Testing<br />

• KEI Flow Loop Test Results<br />

• Comparison of BTZ prediction with Test Data<br />

• Conclusion<br />

Outline<br />

Slide #2 #


Identify key limitations of Two-point Two point model<br />

Objectives<br />

Identify improvement gained through<br />

implementing the <strong>Bound</strong>ing <strong>Thrust</strong> Zone (BTZ)<br />

Identify Key fac<strong>to</strong>rs governing the “general general”<br />

nature of globe valve thrust w.r.t. w.r.t.<br />

position<br />

Overview of BTZ model and model validation<br />

Slide #3 #


Background<br />

March March 2000 – NRC Issued RIS 2000-03 2000 03 “Resolution Resolution<br />

of Generic Safety Issue 158: Performance of<br />

Safety-Related<br />

Safety Related POVs Under Design Basis<br />

Conditions” Conditions<br />

Prior Prior <strong>to</strong> RIS 2000-03 2000 03:<br />

• NRC and INPO conducted surveys and identified<br />

common cause failures with AOVs that can lead <strong>to</strong><br />

safety concerns, reac<strong>to</strong>r scrams, reduced plant<br />

efficiency<br />

– NUREG/CR-6654 NUREG/CR 6654 & NUREG-1275 NUREG 1275 Vol. 13<br />

– INPO SER 1-99 1 99<br />

Slide #4 #


Background – Continued<br />

• EPRI conducted an AOV AOV pilot pilot program program (1996-1999) (1996 1999) teaming with<br />

four utilities <strong>to</strong> develop AOV evaluation methodologies<br />

– EPRI AOV Evaluation Guide TR-107322 TR 107322, , issued May 1999<br />

– Where applicable, EPRI MOV PPM validated methodologies<br />

where used for AOVs<br />

– Several Industry AOV issues identified, including three issues<br />

related <strong>to</strong> globe valves<br />

1) EPRI MOV PPM models were not applicable for flashing (two-<br />

phase) or compressible flow. flow.<br />

<strong>Valve</strong> fac<strong>to</strong>rs as high as 1.6 - 2.35<br />

were found during in-situ in situ plant tests for steam flow application<br />

(INPO OE-11440) OE 11440)<br />

2) No validated models exist for predicting globe valve disc side<br />

loading/friction force<br />

Mid-position position loads may be greater than fully seated loads under<br />

dynamic conditions due <strong>to</strong> flow-induced flow induced forces<br />

3) Mid<br />

Slide #5 #


Background - Continued<br />

EPRI refined and validated models <strong>to</strong> address issue 2) for balanced disc<br />

globe valves only (NUREG/CP-0152, (NUREG/CP 0152, Vol. 3), July 2000<br />

EDF/KEI addressed side-load side load and cavitating/flashing flow effects for an<br />

unbalanced globe valve through experimentation and CFD (ASME PVP<br />

conference July2008 , PVP2008-61238)<br />

PVP2008 61238)<br />

The methodology <strong>to</strong> address mid-position loads being greater or equal<br />

than fully seated load developed and incorporated in AOV evaluation<br />

software by KEI in 2000.<br />

The methodology is addressed in this paper<br />

Slide #6 #


The two-point two point model is the common<br />

industry approach<br />

- Suitable for MOVs, MOVs,<br />

but not for AOVs<br />

Limitations<br />

Established by predicting the thrust at<br />

the closed and open position.<br />

<strong>Thrust</strong> at closed position is predicted<br />

by imposing the peak thrust at the<br />

closed position – peak thrust may be<br />

as far away 30% from the seating<br />

position<br />

Two--point Two point model model may not bound all<br />

thrust profiles and may result in non-- non<br />

conservative conservative margin margin predictions predictions for<br />

AOVs<br />

Two-point Two point <strong>Model</strong><br />

Slide #7 #


BTZ - Enhanced <strong>Model</strong><br />

Peak thrust magnitude is predicted<br />

the same as Two-point Two point model, but<br />

“knee knee” position is defined by the<br />

user <strong>to</strong> bound the thrust curve.<br />

BTZ bounds F DP throughout the<br />

stroke, thus eliminating non-<br />

conservative margin predictions for<br />

AOVs<br />

<strong>Bound</strong>ing <strong>Thrust</strong> Zone<br />

Slide #8 #


<strong>Bound</strong>ing <strong>Thrust</strong> Zone - Applicability<br />

When is BTZ necessary?<br />

<strong>Valve</strong> Parameters<br />

• Flow Over the Disc<br />

• Opening Stroke<br />

Actua<strong>to</strong>r Parameters<br />

• Spring return (i. e., not<br />

applicable <strong>to</strong> double acting<br />

without spring actua<strong>to</strong>rs)<br />

Notes:<br />

Potential non-conservatism<br />

non conservatism<br />

can exist regardless of<br />

actua<strong>to</strong>r action (i. e., reverse<br />

or direct).<br />

• Actua<strong>to</strong>r action only<br />

determines if the air stroke<br />

or spring stroke corresponds<br />

<strong>to</strong> the opening stroke<br />

Slide #9 #


Notes (Continued):<br />

<strong>Bound</strong>ing <strong>Thrust</strong> Zone - Applicability<br />

Closing stroke generally not a<br />

problem since actua<strong>to</strong>r<br />

capability decreases in the<br />

closing direction – minimum<br />

margin at seating position<br />

Slide #10 # 10


<strong>Thrust</strong> Components<br />

Disc DP Force, F DP<br />

Stem Rejection Force, F P<br />

Side-load Force, F US<br />

Static Forces, F P<br />

Packing<br />

Bellows<br />

Static Pis<strong>to</strong>n Seal<br />

Friction<br />

Sealing Load, F SL<br />

Closing Stroke<br />

Opening Stroke<br />

Introduction<br />

<strong>Thrust</strong> Components<br />

FC = FDS + FP + FUS + FSR + FDF + FDP + FSL<br />

FO = FDS + FP + FUS + FSR + FDF + FDP<br />

Slide #11 # 11


Key Fac<strong>to</strong>rs<br />

Key Fac<strong>to</strong>rs Influencing FDP DP vs. Position<br />

Balanced/Unbalanced Trim affects<br />

magnitude<br />

Maximum Disc Head Diameter vs.<br />

Seating Diameter<br />

Disc Head-<strong>to</strong> Head <strong>to</strong>-Body/Cage Body/Cage Wall<br />

Clearance<br />

Trim Trim Flow Flow Characteristics<br />

Characteristics<br />

(focus (focus of of testing) testing)<br />

Fluid Media<br />

Operating Conditions (e.g. DP, Q,<br />

T, & Cavitation/flashing)<br />

Slide #12 # 12


Example of Geometric<br />

Dependency<br />

(e.g., Seat Based vs. Guide Based)<br />

Unbalanced Unbalanced Disc<br />

Clearance Clearance between Disc<br />

Head and body/cage wall<br />

is small ( (lower lower Figure) Figure)<br />

Key Fac<strong>to</strong>rs - Continued<br />

Wide<br />

Clearance<br />

Narrow<br />

Clearance<br />

Slide #13 # 13


Key Fac<strong>to</strong>rs - Continued<br />

Area Based on D seat<br />

Example of Geometric Dependency<br />

(e.g., Seat Based vs. Guide Based)<br />

Narrow clearance restricts flow and<br />

causes high static pressure <strong>to</strong> act on the<br />

disc face<br />

Once disc opens, area on which pressure<br />

acts increases from Dseat seat <strong>to</strong> Ddisc disc diam.<br />

The increase in Area and preservation of<br />

DP Close causes an increase in F DP<br />

As such, F DP initially increases as the disc<br />

moves from the seat untill ~ +25%<br />

open, then decreases as DP drops below<br />

DP<br />

DPclose close<br />

Area Based on D disc diam.<br />

Slide #14 # 14


Test Specimen<br />

4” <strong>Globe</strong> <strong>Valve</strong><br />

Unbalanced Trim<br />

4 3/8 inch Port<br />

Flow Under<br />

Equal Percent or Quick Open Trim<br />

(established by the Cage)<br />

Quick Open Equal Percent<br />

KEI Flow Loop Testing<br />

Slide #15 # 15


Measurements/Instrumentation<br />

<strong>Thrust</strong> (using a Crane ForceLink<br />

and a traditional load cell)<br />

Upstream and Downstream<br />

Pressure<br />

Upper Body Cavity Pressure<br />

Flow Rate<br />

Actua<strong>to</strong>r Diaphragm Pressure<br />

Key Parameters<br />

Three DP/Flow rates<br />

Equal Percent and quick open<br />

trim flow characteristics<br />

KEI Flow Loop Testing<br />

Slide #16 # 16


KEI Flow Loop Testing<br />

4-inch 150# unbalanced cage guided globe valve<br />

Slide #17 # 17


Flow Coefficient, Cv<br />

250<br />

200<br />

150<br />

100<br />

50<br />

0<br />

Quick Open - Test Data<br />

Quick Open - Fisher Data<br />

Equal Percent - Test Data<br />

Equal Percent - Fisher Data<br />

Test Results<br />

0% 10% 20% 30% 40% 50% 60% 70% 80% 90% 100%<br />

Disc Position, % Open<br />

Comparison of Experimental versus Published C v Data<br />

Slide #18 # 18


Disc Differential Pressure Force (F DP ), lbs<br />

1600<br />

1400<br />

1200<br />

1000<br />

800<br />

600<br />

400<br />

200<br />

Test Results-Equal Results Equal Percent Trim<br />

Equal Percent Trim<br />

0<br />

0<br />

0% 10% 20% 30% 40% 50% 60% 70% 80% 90% 100%<br />

Disc Position, % Open<br />

Disc Head Force - Equal Percent<br />

<strong>Valve</strong> Differential Pressure<br />

<strong>Valve</strong> DP knee is a good indica<strong>to</strong>r for the F DP knee for BTZ methodology<br />

120<br />

100<br />

80<br />

60<br />

40<br />

20<br />

<strong>Valve</strong> Differential Pressure, psi<br />

Slide #19 # 19


Test Results – Quick Open vs. Equal Percent<br />

Disc Head Force Coefficient<br />

1.2<br />

1.0<br />

0.8<br />

0.6<br />

0.4<br />

0.2<br />

0.0<br />

Equal Percent Trim<br />

Quick Open Trim<br />

0% 10% 20% 30% 40% 50% 60% 70% 80% 90% 100%<br />

Disc Position, % Open<br />

F DP coefficient is dependent on trim flow characteristics<br />

Slide #20 # 20


Key Conclusions<br />

Conclusion from Test Data<br />

FDP DP (and consequently the resultant thrust) for Equal Percent<br />

and Quick Open Trim are significantly different<br />

FDP DP vs. position trend is dependent on Trim Type due <strong>to</strong> DP<br />

and Disc DP force coefficient relationship with position<br />

<strong>Valve</strong> and system resistance governs relationship of valve DP<br />

w.r.t position<br />

Knee location for Equal percent can be as far out as 55%<br />

Open; Quick Open as little as 15%<br />

Slide #21 # 21


Determining Knee Location without Testing<br />

<strong>Valve</strong> Differential Pressure Ratio, ∆PR<br />

1.0<br />

0.9<br />

0.8<br />

0.7<br />

0.6<br />

0.5<br />

0.4<br />

0.3<br />

0.2<br />

0.1<br />

Quick Open<br />

Equal Percent<br />

Linear<br />

0.0<br />

0% 10% 20% 30% 40% 50% 60% 70% 80% 90% 100%<br />

∆P<br />

ratio<br />

∆P<br />

=<br />

∆P<br />

v<br />

sys<br />

Disc Position, % Open<br />

=<br />

K<br />

up<br />

K<br />

+ K<br />

v<br />

v(<br />

x)<br />

( x)<br />

+ Kdown<br />

<strong>Valve</strong> DP ratio can be analytically predicted and used <strong>to</strong> identify knee for BTZ<br />

Slide #22 # 22


BTZ <strong>Prediction</strong> and Test Data Comparison<br />

Disc Head Force, lbs<br />

2000<br />

1800<br />

1600<br />

1400<br />

1200<br />

1000<br />

800<br />

600<br />

400<br />

200<br />

Equal Percent Trim<br />

Running Average Closing Stroke Disk Head Force<br />

<strong>Bound</strong>ing <strong>Thrust</strong> Zone <strong>Prediction</strong><br />

0<br />

0% 10% 20% 30% 40% 50% 60% 70% 80% 90% 100%<br />

Disc Position, % Open<br />

<strong>Prediction</strong>s based on proper location of knee in BTZ<br />

model bound test data<br />

Slide #23 # 23


Conclusions<br />

• BTZ provides bounding prediction of F DP and consequently<br />

the resulting <strong>to</strong>tal thrust<br />

• BTZ eliminates the potential for non-conservative non conservative margin<br />

predictions in AOVs<br />

• BTZ knee location can be analytically predicted using the<br />

valve flow coefficients and system resistance<br />

• Methodology validated by testing and incorporated in the<br />

globe valve thrust prediction model in KVAP software (Kalsi<br />

<strong>Valve</strong> and Actua<strong>to</strong>r <strong>Prediction</strong> software)<br />

Slide #24 # 24

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