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Dust Nuisance at Fuel Feed System in AFBC boiler

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The theory<br />

As long as the fluid speed is sufficiently<br />

subsonic (V < mach 0.3), the<br />

<strong>in</strong>compressible Bernoulli's equ<strong>at</strong>ion (<br />

equ<strong>at</strong>ion 1) describes the flow. Apply<strong>in</strong>g<br />

Bernoulli equ<strong>at</strong>ion to air stream<br />

travell<strong>in</strong>g down the axis of the horizontal<br />

tube gives the equ<strong>at</strong>ion 2 & 3.<br />

2<br />

Va<br />

<br />

Pa<br />

gZ<br />

2<br />

2<br />

a<br />

P<br />

2<br />

b<br />

2<br />

Vb<br />

<br />

gZ<br />

2<br />

Va<br />

Vb<br />

<br />

Pa<br />

Pb<br />

( equ<strong>at</strong>ion<br />

2)<br />

2 2<br />

P<br />

P<br />

P<br />

Q <br />

<br />

a<br />

1<br />

2<br />

P<br />

b<br />

V<br />

2P<br />

<br />

Q C *<br />

2<br />

2<br />

Vb<br />

Va<br />

<br />

( equ<strong>at</strong>ion<br />

3)<br />

2 2<br />

2<br />

a<br />

<br />

A<br />

<br />

<br />

<br />

A<br />

a<br />

b<br />

<br />

<br />

<br />

2<br />

Aa<br />

<br />

A <br />

a<br />

<br />

<br />

<br />

<br />

Ab<br />

<br />

2 * P<br />

<br />

2<br />

<br />

1(<br />

equ<strong>at</strong>ion<br />

<br />

( equ<strong>at</strong>ion<br />

<br />

1<br />

<br />

Aa<br />

<br />

A <br />

a<br />

<br />

<br />

<br />

<br />

Ab<br />

<br />

2<br />

b<br />

( equ<strong>at</strong>ion1)<br />

4)<br />

5)<br />

( equ<strong>at</strong>ion<br />

<br />

1<br />

<br />

6)<br />

From cont<strong>in</strong>uity, the thro<strong>at</strong> velocity V b<br />

can be substituted out of the above<br />

equ<strong>at</strong>ion to give, Solv<strong>in</strong>g for the<br />

upstream velocity V a and multiply<strong>in</strong>g by<br />

the cross-sectional area A a gives the<br />

volumetric flow r<strong>at</strong>e Q,<br />

Ideal, non-viscous fluids would obey the<br />

above equ<strong>at</strong>ion. The small amounts of<br />

energy converted <strong>in</strong>to he<strong>at</strong> with<strong>in</strong><br />

viscous boundary layers tend to lower<br />

the actual velocity of real fluids<br />

somewh<strong>at</strong>. A discharge coefficient C is<br />

typically <strong>in</strong>troduced to account for the<br />

viscosity of fluids, C is found to depend<br />

on the Reynolds Number of the flow,<br />

and usually lies between 0.90 and 0.98<br />

for smoothly taper<strong>in</strong>g venturis.<br />

Higher PA header pressure results <strong>in</strong><br />

<strong>in</strong>creased pressure drop (ΔP) and thus<br />

the Q <strong>in</strong>creases. If PA header pressure is<br />

<strong>in</strong>creased and as the downstream<br />

pressure is fairly constant due to<br />

fluidized bed back pressure, the suction<br />

<strong>at</strong> thro<strong>at</strong> improves.<br />

Calcul<strong>at</strong>ion & <strong>in</strong>ference<br />

1. Us<strong>in</strong>g Bernoulli pr<strong>in</strong>ciple, we calcul<strong>at</strong>ed th<strong>at</strong> the l<strong>in</strong>e velocity to be as high as 24 m/s. Even then<br />

the suction was not enough. It meant the energy was not used up <strong>in</strong> cre<strong>at</strong><strong>in</strong>g good suction <strong>at</strong><br />

venturi.<br />

2. It was also seen th<strong>at</strong> the PA l<strong>in</strong>es were currently oper<strong>at</strong><strong>in</strong>g on high l<strong>in</strong>e velocities. The erosion<br />

seen <strong>in</strong> bed coils confirmed this. The erosion r<strong>at</strong>e was more where the coils were close the fuel<br />

nozzle cap.<br />

3. Two mix<strong>in</strong>g nozzles were dismantled & seen. The thro<strong>at</strong> diameters were measured to be 50 & 48<br />

mm. We recommended th<strong>at</strong> the mix<strong>in</strong>g nozzle is replaced with 42 mm thro<strong>at</strong> mix<strong>in</strong>g nozzles so<br />

th<strong>at</strong> the air flow is reduced simultaneously improv<strong>in</strong>g the suction.

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