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Carnot Engine - Practice Questions & MCQ

Edited By admin | Updated on Sep 18, 2023 18:34 AM | #JEE Main

Quick Facts

  • Carnot Engine is considered one of the most asked concept.

  • 25 Questions around this concept.

Solve by difficulty

Even the Carnot engine cannot give 100% efficiency because we cannot

 A Carnot engine absorbs 1000 J of heat energy from a reservoir at 1270C and rejects 600 J of heat energy during each cycle. The   efficiency of the engine and temperature of the sink will be :            

A Carnot engine, whose efficiency is 40%, takes in heat from a source maintained at a temperature of 500 K It is desired to have an engine of efficiency 60%. Then, the intake temperature for the same exhaust (sink) temperature must be

Concepts Covered - 0

Carnot Engine
  • Carnot Engine-

          As shown in the below figure, It consists of the following parts

        

      1.A cylinder with perfectly non-conducting walls and a perfectly conducting base containing an ideal gas as working
         substance and fitted with a non-conducting frictionless piston.

      2. A source of infinite thermal capacity maintained at a constant higher temperature T1

     3. A sink of infinite thermal capacity maintained at a constant lower temperature T2

      4. A perfectly non-conducting stand for the cylinder.

  • Carnot cycle-

  As shown in the below figure, It consists of the following 4 processes.

 

1. Isothermal expansion (curve AB)

The cylinder containing ideal gas as working substance allowed to expand slowly at this constant temperature T1

So Work done = Heat absorbed by the system

W_{1}=Q_{1}=\int_{V_{1}}^{V_{2}} P d V=R T_{1} \log _{e}\left(\frac{V_{2}}{V_{1}}\right)=\text { Area of ABGE }

2. Adiabatic expansion (curve BC)

The cylinder is then placed on the non-conducting stand and the gas is allowed to expand adiabatically till the
temperature falls from T1 to T2

W_{2}=\int_{V_{2}}^{V_{3}} P d V=\frac{R}{(\gamma-1)}\left[T_{1}-T_{2}\right]=\text { Area of } B C H G

 

3. Isothermal compression (curve CD)

The cylinder is placed on the sink and the gas is compressed at constant temperature T2.
Work done = Heat released by the system

W_{3}=Q_{2}=-\int_{V_{3}}^{V_{4}} P d V=-R T_{2} \log _{e} \frac{V_{4}}{V_{3}}=R T_{2} \log _{e} \frac{V_{3}}{V_{4}}=\text { Area of } C D F H

4. Adiabatic compression (curve DA)

Finally, the cylinder is again placed on a non-conducting stand and the compression is continued so that gas returns to its initial stage.

W_{4}=-\int_{V_{4}}^{V_{1}} P d V=-\frac{R}{\gamma-1}\left(T_{2}-T_{1}\right)=\frac{R}{\gamma-1}\left(T_{1}-T_{2}\right)=\text { Area of } A D F E

  • The efficiency of the Carnot cycle (\eta)

The efficiency of the engine is defined as the ratio of work done to the heat supplied.

\eta=\frac{\text { work done }}{\text { Heat input }}=\frac{W}{Q_{1}}

Net work done during the complete cycle

\\ W=W_{1}+W_{2}+\left(-W_{3}\right)+\left(-W_{4}\right)\\ \ As \ W_{2}=W_{4}\\ \Rightarrow W=W_{1}-W_{3}=\text { Area of } A B C D

\eta=\frac{W}{Q_{1}}=\frac{W_{1}-W_{3}}{W_{1}}=\frac{Q_{1}-Q_{2}}{Q_{1}}=1-\frac{W_{3}}{W_{1}}=1-\frac{Q_{2}}{Q_{1}}

Putting the values we get

\eta=1-\frac{R T_{2} \log _{e}\left(V_{3} / V_{4}\right)}{R T_{1} \log _{e}\left(V_{2} / V_{1}\right)} ..... (1)

Since points, B and C lie on the same adiabatic curve 

\therefore T_{1} V_{2}^{\gamma-1}=T_{2} V_{3}^{\gamma-1} \text { or } \frac{T_{1}}{T_{2}}=\left(\frac{V_{3}}{V_{2}}\right)^{\gamma-1}......(2)

Also, point D and A lie on the same adiabatic curve

\therefore T_{1} V_{1}^{\gamma-1}=T_{2} V_{4}^{\gamma-1} \text { or } \frac{T_{1}}{T_{2}}=\left(\frac{V_{4}}{V_{1}}\right)^{\gamma-1}....(3)

From the equation (2) and (3) we get

\frac{V_{3}}{V_{2}}=\frac{V_{4}}{V_{1}} \text { or } \frac{V_{3}}{V_{4}}=\frac{V_{2}}{V_{1}} \Rightarrow \log _{e}\left(\frac{V_{3}}{V_{4}}\right)=\log _{e}\left(\frac{V_{2}}{V_{1}}\right) .....(4) 

Put equation (4)  in equation (1) we get 

The efficiency of the Carnot engine as

\eta=1-\frac{T_{2}}{T_{1}}

      So \eta =\frac{W}{Q_{1}}=1-\frac{T_{2}}{T_{1}}

      where 

            T_{1}= Source temperature  , T_{2}= Sink Temperature   and    \left ( T_{1} > T_{2}\right )

           and    T_{1}\, and\, T_{2}  are in kelvin

   From the above formula, we can conclude that

      1. The efficiency of a heat engine depends only on temperatures of source and sink and is independent of all other factors.

      2. As a Carnot engine is the ideal engine, So no heat engine can be more efficient than Carnot engine.

      3. All reversible heat engines working between same temperatures are equally efficient   

     4. Since  T_{1} > T_{2}  So the efficiency of a Carnot engine is always lesser than unity.

  • Carnot Theorem (The relation between Heat and Temperature in the Carnot cycle)

           i.e     \frac{Q_{1}}{T_{1}}= \frac{Q_{2}}{T_{2}}

              where 

Q_{1}= Heat absorbed

Q_{2}= Heat released

T_{2}= Low temperature

T_{1}= Higher Temperature

 

 

 

 

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