Jawaharlal Nehru Technological University Hyderabad

Jawaharlal Nehru Technological University Hyderabad B.Tech III THERMAL ENGINEERING – II Previous Question Paper (October - 2020 - R13)

B.Tech | III | I | R13 | October - 2020

Answer PaperPaper Code: 115ERMaximum Marks: 75Time: 2 hours

Answer any five questions

All questions carry equal marks

Main

115 marks
a

What is the importance of Reheating in Rankine cycle? Derive the expression for efficiency.

7 marks

Answer

The primary importance of Reheating in a Rankine cycle is to increase the dryness fraction of steam at the turbine exhaust, thereby preventing erosion of the turbine blades caused by moisture droplets. Additionally, it improves the thermal efficiency of the cycle by allowing for a higher mean temperature of heat addition.

For a cycle with reheat, the efficiency is derived as the ratio of net work done to the total heat supplied:

η = (W_T1 + W_T2 - W_P) / (Q_s1 + Q_s2)

Where W_T1 is the work from the high-pressure turbine, W_T2 is the work from the low-pressure turbine, W_P is the pump work, Q_s1 is the heat added in the boiler, and Q_s2 is the heat added during the reheating process.

b

Steam leaves the boiler in a Steam turbine plant at 2MPa, 300°C and is expanded to 3.5kPa before entering the condenser. A Reheat cycle with Steam reheated to 300°C at the pressure when it becomes saturated vapour?

8 marks

Answer

Given: P1 = 2 MPa (20 bar), T1 = 300°C. P_condenser = 3.5 kPa (0.035 bar). Reheat pressure (P_reheat) is the pressure where steam becomes saturated vapor during expansion from 2 MPa, 300°C.

  1. From steam tables at 2 MPa, 300°C: h1 = 3023.5 kJ/kg, s1 = 6.7664 kJ/kgK.
  2. Expansion to saturation: Saturated vapor entropy at 2 MPa is 6.339 kJ/kgK. Since s1 > sg, the steam is superheated. Find P_reheat where s = sg. By interpolation, P_reheat is approximately 0.5 MPa (5 bar).
  3. At 5 bar, h_g = 2747.5 kJ/kg.
  4. Work of HP turbine: W_T1 = h1 - h_g = 3023.5 - 2747.5 = 276 kJ/kg.
  5. Reheat to 300°C at 5 bar: h3 = 3064.2 kJ/kg, s3 = 7.547 kJ/kgK.
  6. Expansion to 0.035 bar: s3 = sf + x3(sfg). 7.547 = 0.391 + x3(8.13), giving x3 = 0.879.
  7. h4 = hf + x3(hfg) = 112 + 0.879(2437) = 2254 kJ/kg.
  8. Work of LP turbine: W_T2 = h3 - h4 = 3064.2 - 2254 = 810.2 kJ/kg.
  9. Total Work = 276 + 810.2 = 1086.2 kJ/kg.
  10. Heat Supplied = (h1 - hf_pump) + (h3 - h_g) = (3023.5 - 112) + (3064.2 - 2747.5) = 3228.2 kJ/kg.
  11. Efficiency = (1086.2 / 3228.2) * 100 = 33.65%.
215 marks
a

What is Flue gas analysis?

7 marks

Answer

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b

Natural gas containing 80% CH4, 15% C2H6 and 5% C3H8 is burnt with 50% excess air. Assuming that 90% of the Carbon in the hydrocarbons are converted to CO2 and the rest to CO, Determine Flue gas analysis?

8 marks

Answer

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315 marks
a

What are the features of High Pressure Boilers?

7 marks

Answer

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b

What are the different Mountings and Accessories used in Boilers?

8 marks

Answer

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415 marks
a

How nozzles are classified based on Mach number of the flow passing through?

7 marks

Answer

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b

Air at 7.8 bar and 180°C expands through a convergent-divergent nozzle into a space at 1.03 bar. The flow rate of air is 3.6 kg/s. Assuming isentropic flow throughout and neglecting the inlet velocity, calculate the throat and exit areas of the nozzle.

8 marks

Answer

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515 marks
a

What is Impulse turbine? Explain its Working principle.

6 marks

Answer

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b

Derive the expression for Power produced in Impulse turbine with neat sketch of Velocity diagrams.

9 marks

Answer

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615 marks
a

What are the working principles of different Steam Condensers?

7 marks

Answer

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b

Explain the term Degree of Reaction. What is the value of DoR for different turbines?

8 marks

Answer

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715 marks
a

Explain Closed and Semi-closed Gas turbine cycles with neat sketch.

7 marks

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b

Explain the following terms: i) Reciprocating compressor ii) Scroll compressor iii) Rotary compressor.

8 marks

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815 marks
a

What is the working principle of Jet propulsion system? Explain with T-S diagram.

8 marks

Answer

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b

What are the needs and demands met by Turbo jet?

7 marks

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About this paper

This page contains the question paper of THERMAL ENGINEERING – II from Jawaharlal Nehru Technological University Hyderabad for B.Tech ME III I, October - 2020, R13.

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