Thermodynamics is difficult to learn mostly because it is difficult to teach, but it is hampered by 200 years of colloquial terms that sound alike, and are used misleadingly. One of those terms is the new concept of internal energy often confused with heat. Separate them in your mind so that the variables 'U' and 'Q' can be used mathematically to represent them. Please.
In the "Why a temperature difference" thread Matt Brown posted the following:
Taking his first comments:matt brown wrote: ↑Sun Jun 23, 2024 2:09 pmYep, you're missing the most basic issue where heat equals work (ie Q=W) regardless of direction. This basic thermo tenant is what Tom struggles with where Qin=Wout and...Win=Qout. Just as the "heat of expansion" = work out, the returning piston will require work in = the "heat of compression". An ideal Stirling cycle supplies source in at a Thigh DURING expansion and sink out at Tlow DURING compression (2 distinct temperatures) where work out from expansion exceeds work in from compression proportional to the temperature differential measured via the absolute scale (deg K). Another way to view this is simply that the MEP (mean effective pressure) during expansion must exceed the MEP during compression, regardless whether the compression force comes from a flywheel or ambient pressure (aka, there's no free lunch).
An ideal Stirling cycle supplies both Thigh and Tlow isothermally (constant temperature) and whining that there's no such thing as an isothermal process is lame, since an Otto type cycle with 2 adiabatic processes will follow a similar sequence..
"Yep, you're missing the most basic issue where heat equals work (ie Q=W) regardless of direction. This basic thermo tenant is what Tom struggles with where Qin=Wout and...Win=Qout. "
Doesn't everybody? But it gets worse:
Qin=Win applies at times to a single isothermal stroke or at other times to an entire cycle, but, and it's a big but, it never applies to an adiabatic process, single adiabatic stroke, or a complete cyclic set of adiabatic processes. Adiabatic means zero heat transfer. Q=0.0 in the equation.
The following may help.
Remember for an isolated system nothing gets in or out. That differs from a closed system which allow work and heat to enter and leave, but nothing else such as mass. I get those two confused but we are stuck with the terms, try to do your best at memorizing and separating them.
In a closed system where we are concerned with heat and work energy only entering and leaving, internal energy changes of concern are related to heat and work. Gravity, battery, speeding mass, flywheels, and other energy sources inside the system can be eliminated from the equation. They can be added back if needed for more complicated system models. So the equation becomes:
∆U=∆Q+∆W
That comes from the empirical observation of conservation of energy. If you witness a violation of this first law, you are probably fooling yourself. Check and recheck before quietly asking others privately. If they disagree it's still probably you. Rethink you experiment, ask for help. Pons and Fleishman skipped that process an got horribly slammed, and they weren't even violating, nor attempting to violate, that law.
The equation ∆U=∆W+∆Q for an adiabatic process:
∆Q is zero so the equation becomes:
∆U=∆W
During that process there is no such thing as heat. No heat loss, no heat gain, no heat conversion.
The conversion is internal energy to or from work, for an adiabatic processes. It will involve significant temperature, pressure, and volume changes.
∆U=∆W+∆Q for an isothermal process:
∆U=0.0 Internal energy doesn't change so the equation becomes:
∆W=-∆Q
Thus it is applicable to an isothermal process, zero temperature change.
Expansion: Heat comes in from Th, gets converted to internal energy (maintaining temperature and internal energy), internal energy gets converted to work going out (pressure and volume change, internal energy and temperature are maintained), no heat leaves. Colloquially 100% conversion of heat to work. One forward stroke.
Compression: Work comes in, gets converted to internal energy (maintaining temperature and internal energy), internal energy gets converted to heat going out to Tc (pressure and volume change, internal energy and temperature are maintained), no heat enters. Colloquially 100% conversion of work to heat. One reverse stroke.
If Th and Tc are the same forward work will equal reverse work. Zero net work to output. That is why it is desirable to have Th, forward work coming out, be much higher than Tc, reverse work going back in. Hotter Th, colder Tc.
The above is true for all real engines. Additional losses must also be added to be more accurate. The above is the analysis for possible maximum thermodynamic work out of a full cycle.
For a full cycle starting at U1 and ending at U1, ∆U=U1-U2=0.0
So the equation again becomes:
∆W=-∆Q
Or
W=Q
So starting at the first law the second law drops right into place:
Efficiency n=(∆Wf-∆Wr)/(∆Qin)=(Th-Tc)/Th
The second law is a consequence of the first law for the special case of a full cycle. To violate the second law is to violate the first law for the special case of a full cycle.
This means the second law doesn't apply to a single stroke, no matter how 'tricky' the path will be. It can't be violated for a tricky full cycle either. Carnot and Stirling are the target to shoot for, thermodynamically. Real engines will be worse.