How Does a Heat Engine's Efficiency Affect Final Temperature and Work Output?

AI Thread Summary
The discussion revolves around the efficiency of a heat engine operating between two water tanks at different temperatures, T_A and T_B. When the engine is completely inefficient, the final equilibrium temperature T_f of the tanks is the average of the two initial temperatures, T_f = (T_A + T_B)/2. In the case of a perfectly efficient engine, the final temperature is higher than this average due to the extraction of work from the system, which results in less heat being transferred to the cold tank. The conversation highlights the importance of understanding the concepts of efficiency, heat transfer, and the thermodynamic principles governing the system. Ultimately, the participants are working through the calculations to determine the final temperatures and work output of the engine.
spaghetti3451
Messages
1,311
Reaction score
31

Homework Statement



Two identical tanks of water are at absolute temperatures ##T_A## and ##T_B## respectively, where ##T_{A} > T_{B}##. The tanks each have a heat capacity ##C##, and they are thermally isolated from their environment. Suppose that a heat engine is installed in contact with the two tanks, in order to extract useful work from their temperature difference.

(a) Suppose that the engine is completely inefficient and generates no work. What will be the final temperature ##T_{f}## of the tanks at equilibrium?

(b) Suppose instead that the engine is the most efficient engine possible. What will be the final temperature ##T_{f}## of the tanks at equilibrium?

(c) How much work will have been generated by the efficient engine of part (b)?

Homework Equations



The Attempt at a Solution



(a) If the engine is completely inefficient and generates no work, then heat energy is being transferred from the hot tank with temperature ##T_A## to the cold tank with temperature ##T_B##. The tanks are identical, so each of them have the same mass ##m##. Therefore,

##mC(T_{A}-T_{f})=mC(T_{f}-T_{B})##

##\implies T_{f}=\frac{T_{A}+T_{B}}{2}##

Am I correct so far?
 
Physics news on Phys.org
Yes, you are correct for the part (a)
 
For (b), do I have to assume that the tanks are heat baths, so the temperatures of the tanks remain unchanged?
 
Last edited:
No that happens when they have infinite heat capacity.
 
Well, if part of the heat energy (being transferred from the hot tank to the cold tank) is sucked out by the heat engine and converted to work, then only the wasted heat energy is absorbed by the cold tank. Will the transfer of the wasted amount of heat energy from the hot tank to the cold tank determine the final temperature of the two tanks?

Now, doesn't efficiency = ##1 - \frac{T_{B}}{T_{A}}## mean that the wasted heat energy = ##\frac{T_{B}}{T_{A}}(C)(T_{f}-T_{B})##?

Where do I go from here?

P.S. : In my answer to part (a), the ##m##'s will be missing because ##C = mc##.
 
Assume that at the end of the cycle both become Tf', which will be more than (TA + TB)/2 and the total energy available is C(TA - TB), which was wasted in part (a) of the problem with no work done. So now do you understand what is the correct expression of wasted energy for part (b)? You are using the Carnot formula for a non-Carnot engine. You need to just use the everyday idea of what is efficiency!
 
Last edited:
Do the temperatures of the tanks necessarily have to become the unique final equilibrium temperature ##T'_{f}## at the end of the cycle, and not at some other point of the cycle?
 
This will not be a reversible process so there is cycle but not reversible, in the sense that the engine might come back to its original state but te reservoirs have not come back to original temperatures at least. Just think in terms of the end results.
 
I think you misunderstood my question. I am not asking about the reversibility of the heat engine cycle.

I am asking how you knew that it's only at the end of the cycle, and not at some other point in the cycle, that the tanks reach the equilibrium temperature. Is this because, once the tanks reach equilibrium temperature, then no heat exchange between them is possible, so that the heat engine cannot extract heat energy to do useful work?
 
  • #10
Exactly there comes the idea of reversibility, in a reversible process system and reservoirs are all the time in equilibrium but in all other processes we consider them in equilibrium at certain points after which or before which there is no change in the macroscopic variables in this case temperature. The problem is also asking about the final temperature of the reservoirs after you have got the necessary work from the system/systems. As far as end states are concerned the thermodynamic laws hold for them.
 
Last edited:
  • #11
Why is the final equilibrium temperature of the tanks greater than ##\frac{T_{A}+T_{B}}{2}##?
 
  • #12
because if it is more more heat will be wasted, which the system does not have.
 
  • #13
I am having difficulty understanding your explanation. Would you please elaborate?
 
  • #14
failexam said:
Why is the final equilibrium temperature of the tanks greater than ##\frac{T_{A}+T_{B}}{2}##?
I, as I think you do, believe the final temperature for Part (b) is less than (TA+TB)/2.

Have you solved Parts (b) and (c)?
 
  • #15
I haven't.

Can you please provide the first two to three lines of the solutions so I know exactly how to proceed?

I am completely lost.
 
  • #16
First, clearly define variables:

TA, TB, Tf, C=mc as above.
Ta = variable temperature of tank A.
Tb = variable temperature of tank B.
QA = variable heat leaving tank A and entering engine.
QB = variable heat leaving engine and entering tank B.
W = variable work produced by engine.

We know the engine will have Carnot efficiency as you've stated in #5, but it's a variable = (1-Tb/Ta).

We know the efficiency is also W/QA.

We know the efficiency changes during the course of the process, so an integration is needed.

Do a differential energy balance on the engine.
Combine with differential temperature changes in the tanks, e.g., dQA = -CdTa.
Eliminate W and Q's.
 
Back
Top