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Eclipse Combustion Engineering Guide - Burnerparts

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CHAPTER 1 – ORIFICES & FLOWS<br />

COEFFICIENTS OF DISCHARGE FOR VARIOUS TYPES OF ORIFICES<br />

Sharp Edge<br />

C d = 0.60<br />

Reentrant<br />

0.72<br />

Round Edge<br />

0.97<br />

Short Pipe<br />

0.82<br />

Converging<br />

depends on angle. See<br />

curve at right.<br />

Coefficient of Discharge (C d )<br />

0.95<br />

Orifices and Nozzles Discharging from Plenum<br />

0.93<br />

0.91<br />

0.89<br />

0.87<br />

NOTE: The loss is least at 13˚<br />

0.85<br />

0.83<br />

0 2 4 6 8 10 12 14 16 18 20 22 24<br />

Angle of Convergence in Degrees<br />

ORIFICE FLOW FORMULAS<br />

The flow of air or gas through an orifice can be determined 3.Effect of Changes in Operating Conditions on Pressure<br />

Drop Across an Orifice–General Relationship:<br />

by the formula<br />

h<br />

Q = 1658.5 x Ax C d g<br />

h 2<br />

= Q 2 2 x A 1 2 x C d1 2 x g 2<br />

h 1<br />

(<br />

Q 1<br />

) (<br />

A 2<br />

) (<br />

C d2<br />

)<br />

g 1<br />

where Q =flow, cfh<br />

Again, if any of the factors in this equation are unchanged<br />

A =area of the orifice, sq. in. (see Pages 57 & 58) from Condition 1 to Condtion 2, they can be dropped out to<br />

C d =discharge coefficient of the orifice<br />

form simplified relationships:<br />

(see above)<br />

3a.Pressure Drop Change vs. Flow Change<br />

h =pressure drop across the orifice,″ w.c.<br />

h<br />

g =specific gravity of the gas, based on standard<br />

2<br />

= Q 2 2<br />

h<br />

air at 1.0 (see Pages 19, 20, & 22 thru 24.)<br />

1<br />

(<br />

Q 1<br />

)<br />

This is the square root law, stated another way.<br />

1. Sizing Orifice Plates<br />

To calculate the size of an orifice plate, this equation can 3b.Pressure Drop Change vs. Orifice Area Change<br />

be rearranged as follows:<br />

h 2<br />

= A 1 2<br />

h<br />

A= Q x<br />

g<br />

1<br />

(<br />

A 2<br />

)<br />

1658.5 x C d<br />

h<br />

3c.Pressure Drop Change vs. Specific Gravity Change<br />

h 2<br />

= g 2<br />

2. Effect of Changes in Operating Conditions on h 1<br />

g 1<br />

Flow through an Orifice – General Relationship This relationship may not apply where specific gravity has<br />

Q 2<br />

= A2 x Cd2 x h2 x g 1<br />

been changed by a change in gas temperature. See Page 25.<br />

Q 1 A 1 C d1 h 1<br />

g 2<br />

4. Effect of Changes in Gas Temperature on Flow and<br />

If any of the factors in this relationship remain constant Pressure Drop through an Orifice<br />

from Condition 1 to Condition 2, they can be dropped out of Raising a gas’s temperature has two effects – it increases<br />

the equation, yielding these simplified relationships. Each of the volume and decreases the specific gravity, both in proportion<br />

to the ratio of the absolute temperatures. If we are con-<br />

them assumes only one factor has been changed.<br />

2a.Flow Change vs. Orifice Area Change<br />

cerned with changes in mass flows (scfh), these relationships<br />

Q 2<br />

= A must be used:<br />

2<br />

Q 1 A 1<br />

4a.Flow Change vs. Temperature Change<br />

2b.Flow Change vs. Pressure Drop Change<br />

Q 2<br />

= T ADS1<br />

Q 2<br />

= h Q 1 T ABB2<br />

2<br />

Q 1 h 1<br />

4b.Pressure Drop Change vs. Temperature Change<br />

This is the so-called “square root law.”<br />

h 2<br />

= T ABS2<br />

h 1 T to maintain constant scfh<br />

ABS1<br />

2c.Flow Change vs. Specific Gravity Change<br />

Q 2<br />

= g 1<br />

Q 1<br />

g 2<br />

4

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