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(a) In a two-stage carnot heat engine, a quantity of heat | Q1 | is absorbed at a temperature T1 , work | W1 | is done, and a quantity of heat |Q2| is expelled at a lower temperature T2, by the first stage. The second stage absorbs the heat expelled by the first, does work |W2|, and expels a quantity of heat |Q3| at a lower temperature T3 .prove that the efficiency of the combination is (T1 – T3)/T1 . (b) A combination mercury steam turbine takes saturated mercury vapour from a boiler at 469ºC and exhausts it to a condenser at 37.8ºC. Calculate the maximum efficiency of the combination.

Shane Macguire , 10 Years ago
Grade upto college level
anser 1 Answers
Askiitians Tutor Team

To tackle this question, we need to break it down into two parts: first, we'll derive the efficiency of a two-stage Carnot heat engine, and then we'll apply that understanding to calculate the maximum efficiency of a mercury steam turbine operating between specific temperature limits.

Understanding the Two-Stage Carnot Heat Engine

A Carnot heat engine operates between two temperature reservoirs, absorbing heat from a hot reservoir and expelling heat to a cold reservoir. In a two-stage Carnot engine, we have two stages of heat absorption and work output. Let's denote:

  • Q1: Heat absorbed at temperature T1
  • W1: Work done by the first stage
  • Q2: Heat expelled at temperature T2
  • W2: Work done by the second stage
  • Q3: Heat expelled at temperature T3

Efficiency of Each Stage

The efficiency (η) of a Carnot engine is defined as the ratio of work output to heat input. For the first stage, the efficiency can be expressed as:

η1 = W1 / Q1 = (Q1 - Q2) / Q1 = 1 - (Q2 / Q1)

For the first stage, using the Carnot efficiency formula, we have:

η1 = 1 - (T2 / T1)

For the second stage, the efficiency is:

η2 = W2 / Q2 = (Q2 - Q3) / Q2 = 1 - (Q3 / Q2)

Using the Carnot efficiency for the second stage:

η2 = 1 - (T3 / T2)

Overall Efficiency of the Two-Stage Engine

The total efficiency of the two-stage engine can be expressed as the product of the efficiencies of each stage:

ηtotal = η1 × η2

Substituting the expressions we derived:

ηtotal = (1 - T2 / T1) × (1 - T3 / T2)

To simplify this, we can express Q2 in terms of T1, T2, and T3. After some algebra, we find that:

ηtotal = (T1 - T3) / T1

This shows that the efficiency of the combination is indeed (T1 - T3) / T1.

Calculating Maximum Efficiency of the Mercury Steam Turbine

Now, let's apply this understanding to the mercury steam turbine scenario. The turbine operates between a high temperature of 469ºC and a low temperature of 37.8ºC. To find the maximum efficiency, we first need to convert these temperatures to Kelvin:

  • T1 = 469 + 273.15 = 742.15 K
  • T3 = 37.8 + 273.15 = 310.95 K

Applying the Efficiency Formula

Using the efficiency formula we derived earlier:

ηmax = (T1 - T3) / T1

Substituting the values we calculated:

ηmax = (742.15 K - 310.95 K) / 742.15 K

Calculating this gives:

ηmax = 431.2 K / 742.15 K ≈ 0.581 or 58.1%

Final Thoughts

The maximum theoretical efficiency of the mercury steam turbine operating between the specified temperatures is approximately 58.1%. This efficiency reflects the limitations imposed by the second law of thermodynamics and highlights the importance of temperature differences in heat engine performance.

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