Steam produced heat transfer heat exchangers

In summary: Again, you need to show and carry thru the units in these calculations. You are just assuming what units appear in the results.You've also neglected to include the flow rate of the flue gases in your heat calculations, which is why the result appears so low.For the heat available:H = eff. * flow * cp * ΔT, which......in this case is the heat supplied from the flue gas, so you need to include the flow rate (kg/h) and the specific heat capacity (kJ/kg-K) of the flue gas, as well as the temperature difference (K) between the inlet and outlet of the gas in the boiler. This will give you the total heat available for steam production
  • #36
I am confused by this question as well.

When i calculate the area as per your last post MCtachyon, i end up with 1.13m2 ( i had a slightly different temp result than you - and 54x328.64 doesn't equal what you calculated its 17746.56)

But when i use this to calculate the number of tubes i end up with n= 1160 for the max and n=913 for the min.

This seems like a really high number of tubes, this also leads me to overall length of 0.1m and 0.12 m respectively.

I know this can't be right because the question directly after requires that the tubes be divided into passes less than 5 m long so the overall length must be greater than what i have calculated.

Any help with this would be greatly appreciated!
 
Last edited:
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  • #37
Show your work for getting phi (total heat transferred).
 
  • #38
Φ =qmhCph (TH1-TH2)
= 50000 x 1.15(1600-200)
= 80.5x106 J/hr
with 10% heat loss = 80.5x106 x 0.9
=724.5 x 105 J/hr

Calculated ΔT as per MCtachyons post above (slightly different answer as i didn't round the 4.26 number)

Φ=UAΔT
724.5x105 = 54 x A(328.4)
A= 724.5x105/3600 / 54 x 328.4
= 1.13m2

qmh = ρAfu
so for u=22m/s
Af= 50000/3600 / 1.108 x 22
=0.569 kg s-1

Af= πd2n / 4 where n=number of tubes
n= 4Af / πd2
= 4 x 0.569 / π(0.025)2
=1159.15 = 1160 tubes.

I have also tried the following equation which gives me an answer of 1160.7

n= qmh / ρπd2uCan anyone see where I am going wrong?
 
  • #39
SeaofEnergy said:
Φ =qmhCph (TH1-TH2)
= 50000 x 1.15(1600-200)
= 80.5x106 J/hr
with 10% heat loss = 80.5x106 x 0.9
=724.5 x 105 J/hr

Calculated ΔT as per MCtachyons post above (slightly different answer as i didn't round the 4.26 number)

Φ=UAΔT
724.5x105 = 54 x A(328.4)
A= 724.5x105/3600 / 54 x 328.4
= 1.13m2

qmh = ρAfu
so for u=22m/s
Af= 50000/3600 / 1.108 x 22
=0.569 kg s-1

Af= πd2n / 4 where n=number of tubes
n= 4Af / πd2
= 4 x 0.569 / π(0.025)2
=1159.15 = 1160 tubes.

I have also tried the following equation which gives me an answer of 1160.7

n= qmh / ρπd2uCan anyone see where I am going wrong?
Don't you want to calculate the surface area of the tubes, rather than the cross sectional area? Isn't the heat transferred thru the circumference of each tube?
 
  • #40
SeaofEnergy said:
Φ =qmhCph (TH1-TH2)
= 50000 x 1.15(1600-200)
= 80.5x106 J/hr
with 10% heat loss = 80.5x106 x 0.9
=724.5 x 105 J/hr
Check your units closely here.
Why not add units to all equations??
Also, I would not deduct the 10% loss here for gross heat transferred.
 
  • #41
SeaofEnergy said:
I am confused by this question as well.

When i calculate the area as per your last post MCtachyon, i end up with 1.13m2 ( i had a slightly different temp result than you - and 54x328.64 doesn't equal what you calculated its 17746.56)

I rushed this as I was on lunch in work when I was posting. See edited post for actual working.
 
  • #42
SteamKing said:
Don't you want to calculate the surface area of the tubes, rather than the cross sectional area? Isn't the heat transferred thru the circumference of each tube?

As far as I am aware the A in the Φ=UAΔT equation gives you the surface area of the heat transfer. Which is what I'm after no?

insightful said:
Check your units closely here.
Why not add units to all equations??
Also, I would not deduct the 10% loss here for gross heat transferred.

That's what Steamking basically confirmed was ok to Mitch earlier? i.e Mitch said 'So, (1600-200)*1.15*.9*50,000=72450000kj/hr'

Steamking said, 'that looks much better' all i did was separate out the x0.9 stage.

Any help beyond these pretty vague clues? I have looked at the units over and over before i came on here to try and get some help.
 
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  • #43
MCTachyon said:
So we now just add to the equation:

Φ = U*A*LMTD

Therefore:

A = Φ / U*LMTD

A = 72.45 x 106Jh-1 / (54 Wm-2k-1 * 328.64°C)

Balancing units gives

(72.45x106) / 3600 = 20125 Js-1

Completing:

A = 20125 / 17746.56

A = 1.13m2Close? Or have I missed something out?

*Edited from post 35.
 
  • #44
SeaofEnergy said:
As far as I am aware the A in the Φ=UAΔT equation gives you the surface area of the heat transfer. Which is what I'm after no?
Yes, but in order to calculate the number of tubes which gives this surface area, you don't use the cross-sectional area of each tube like you did in your calculations:
SeaofEnergy said:
Af= πd2n / 4 where n=number of tubes
n= 4Af / πd2
= 4 x 0.569 / π(0.025)2
=1159.15 = 1160 tubes.

Can anyone see where I am going wrong?

For an individual tube, SA ≠ π d2 / 4
 
  • #45
SeaofEnergy said:
Φ =qmhCph (TH1-TH2)
= 50000 x 1.15(1600-200)
= 80.5x106 J/hr
with 10% heat loss = 80.5x106 x 0.9
=724.5 x 105 J/hr
Should this be kJ/hr??
 
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  • #46
A note on the "10% loss."

Since we don't know exactly where the heat loss occurs, it is prudent to consider it to occur after the heat is transferred through the tubes. (Prudent because it results in 10% greater surface area and is thus more conservative.)
That is why I would not incorporate the loss when calculating phi.
 
  • #47
SteamKing said:
Yes, but in order to calculate the number of tubes which gives this surface area, you don't use the cross-sectional area of each tube like you did in your calculations:For an individual tube, SA ≠ π d2 / 4
My materials state this as the route to determine number of tubes.

qmh=ρAfu

where
qmh - mass flowrate of the liquid/gas = 50000/3600 kJ/s
ρ is the density of the liquid/gas = 1.108 kg m-3
Af is the flow area - (unknown calculated as 0.569 m2 using this equation)
u is the velocity of the liquid/gas = 22 ms-1

then

Af= πd2n / 4

where
d is the internal diameter of the tubes = 0.025m
n is the number of tubes.

or alternatively:

n= 4qmh / ρπd2u
The problem i am having is that i cannot get these equations to return a viable answer. There must be something i am missing here but i still cannot see what it is. I have tried recalculating this with the revised surface area of 1134.8 m2 but still have 1160 tubes at max and 913 tubes at min with 65 and 85 passes respectively when restricted to 5m length passes. I am new to heat exchangers but this seems like an unrealistically high amount of tubes/passes?

insightful said:
Should this be kJ/hr??

Yes your right. Cheers!
 
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  • #48
SeaofEnergy said:
I have tried recalculating this with the revised surface area of 1134.8 m2 but still have 1160 tubes
Use these numbers. How long would a single tube bundle be to give the required surface area?
 
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  • #49
Thanks I have got there now. Just needed a nudge in the right direction!Appreciate the help folks! :)
 
  • #50
surface area of 1134.8 m2

Is this surface area correct for his part of the question?
 
  • #51
MCTachyon said:
Is this surface area correct for his part of the question?
I originally had 1.13m2 but that was due to a units error, the 724.5 x 105 is in KJ/hr which means when it comes to calculating the Area it is 724.5 x 108 as the coefficient is in W m-2 K-1. This balances the units. I think that's correct anyway.
 
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