Heat transfer in a nuclear reactor and the electrical equivalent

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SUMMARY

This discussion focuses on the heat transfer equations in a nuclear reactor, specifically modeling the thermal dynamics of fuel, graphite, and coolant. The equations presented include the heat transfer for fuel, graphite, and coolant, incorporating parameters such as power produced (P), specific heat capacities (cp), and thermal resistances (R1, R2). The conversation also explores the relationship between thermal resistance and electrical circuits, suggesting an analogy between temperature gradients and voltage, and heat flux and current. The participants emphasize the importance of understanding stationary conditions and the implications of thermal resistances in reactor design.

PREREQUISITES
  • Understanding of heat transfer principles in nuclear reactors
  • Familiarity with thermal resistance concepts
  • Knowledge of differential equations related to thermal dynamics
  • Basic electrical circuit theory for analogies with thermal systems
NEXT STEPS
  • Study the derivation and application of heat transfer equations in nuclear reactors
  • Learn about thermal resistance networks and their role in reactor design
  • Explore the relationship between thermal dynamics and electrical circuit analogies
  • Investigate the effects of transient conditions on reactor thermal performance
USEFUL FOR

Nuclear engineers, thermal analysts, and students studying reactor physics will benefit from this discussion, particularly those interested in heat transfer modeling and its electrical analogs in nuclear systems.

dRic2
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Homework Statement
see picture below
Relevant Equations
heat transfer equation
Schermata 2019-06-15 alle 19.51.41.png

To write the equation I took as the control volume the following block:
Schermata 2019-06-15 alle 19.56.31.png

and the equation I wrote are:

$$ 6m_{f} c_{p_{f}} \frac {dT_{f}}{dt} = 6P - \frac 1 {R_1} (T_f - T_g) \text{ for the fuel}$$
$$ m_{g} c_{p_g} \frac {dT_{g}}{dt} = \frac 1 {R_1} (T_f - T_g) - \frac 1 {R_2} (T_g - T_c) \text{ for the graphite}$$
$$ 3m_{c} c_{p_c} \frac {dT_{c}}{dt} = \frac 1 {R_1} (T_g - T_c) - 3G c_{p_{c}} (T_{out} - T_{in}) \text{ for the coolant}$$

##P## is the power produced by each fuel element. In stationary condition just drop the time derivative. I'm not totally sure about the last one though...

I have no clue on point b). Can someone give me a hint ?

Thanks Ric
 

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Try drawing a triangular control boundary from the center of the central coolant channel to the center of two outer coolant channels, which has a fuel element in the middle. See the symmetry. The temperature is like the voltage, heat flux like the current through the fuel and graphite into the coolant. There are thermal resistances.
 
Astronuc said:
Try drawing a triangular control boundary
If I take the triangular boundary the equations become:
$$ m_{f} c_{p_{f}} \frac {dT_{f}}{dt} = P - \frac 1 {R_1} (T_f - T_g) \text{ for the fuel}$$
$$ m_{g} c_{p_g} \frac {dT_{g}}{dt} = \frac 1 {R_1} (T_f - T_g) - \frac 1 {R_2} (T_g - T_c) \text{ for the graphite}$$
$$ m_{c} c_{p_c} \frac {dT_{c}}{dt} = \frac 1 {R_1} (T_g - T_c) - G c_{p_{c}} (T_{out} - T_{in}) \text{ for the coolant}$$
They are simpler (thanks for the suggestion :smile: ), but I don't think that my first try was wrong. In fact the mass of moderator inside the boundary in this case is less than what I considered in the previous post. At the end they should give the same result, correct ?
Astronuc said:
There are thermal resistances.
If the system is stationary I think I did it. I can re-arrange the last equation imposing ##T_{c} = \frac {T_{in} + T_{out}} 2## :

$$m_c c_{p_c} \frac {dT_c}{dt} = \frac 1 {R_1} (T_g - T_c) - 2G c_{p_{c}} (T_c - T_{in})$$

And the equivalent electrical network should be:
photo_2019-06-15 21.02.37.jpeg


But in the general case there should be capacitors (the terms with ##mc_p \frac{dT}{dt}##) and I don't know how to insert them properly inside the circuit. Maybe in parallel with the corresponding resistance ?
 
Since part a states "steady-state", then dT/dt = 0. The temperature gradients and heat flux should be constant. The heat leaving the fuel must equal the heat entering the coolant channel.
 
Yes but I'd like to know the general case too, if it doesn't get too complicated. Anyway Thanks for the replies!
 

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