JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD

JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD B.Tech III THERMAL ENGINEERING Previous Question Paper (July/August - 2023 - R16)

B.Tech | III | I | R16 | July/August - 2023

Answer PaperPaper Code: 135BNMaximum Marks: 75Time: 3 Hours

i) Question paper consists of Part A, Part B. ii) Part A is compulsory, which carries 25 marks. In Part A, answer all questions. iii) In Part B, Answer any one question from each unit. Each question carries 10 marks and may have a, b as sub questions.

Part A

1.a

How are heat engines classified?

2 marks

Answer

Heat engines are primarily classified into two categories based on the location of the combustion process:

  1. External Combustion Engines (ECE): Engines where the fuel burns outside the main cylinder, such as steam engines and steam turbines, where heat is transferred to a working fluid.
  2. Internal Combustion Engines (ICE): Engines where the fuel burns inside the cylinder, such as petrol (spark ignition) and diesel (compression ignition) engines, where the products of combustion act as the working fluid.
1.b

What is the function of a carburettor?

3 marks

Answer

The primary function of a carburettor in a spark-ignition engine is to prepare a combustible mixture of air and fuel by atomizing the fuel and mixing it with the incoming air in the correct proportions. It ensures that the engine receives the appropriate air-fuel ratio required for different operating conditions, such as starting, idling, cruising, and acceleration.

1.c

Define Indicated power.

2 marks

Answer

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1.d

What is brake horse power?

3 marks

Answer

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1.e

How are gas turbines classified?

2 marks

Answer

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1.f

What is meant by stage compression?

3 marks

Answer

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1.g

State the uses of steam produced by the boilers.

2 marks

Answer

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1.h

What are the functions of a steam nozzle?

3 marks

Answer

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1.i

Define a steam condenser and state its objects.

2 marks

Answer

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1.j

What do you mean by compounding of steam turbines?

3 marks

Answer

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Part B

210 marks
a

With a neat sketch, explain the working principle of a simple carburetor.

5 marks

Answer

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b

Explain the phenomenon of diesel knock.

5 marks

Answer

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OR
310 marks
a

List various assumptions made in air - standard cycle analysis.

5 marks

Answer

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b

Briefly explain the stages of combustion in CI engines.

5 marks

Answer

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410 marks
a

Briefly discuss the various efficiency terms associated with an engine.

5 marks

Answer

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b

Define mean effective pressure and distinguish between mean effective pressure and indicated mean effective pressure.

5 marks

Answer

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OR
5

A four-cylinder engine running at 1200 rpm gave 18.6 kW brake power. The average torque when one cylinder was cut out was 105 N-m. Determine the indicated thermal efficiency if the calorific value of the fuel is 42000 kJ/kg and engine uses 0.34 kg of petrol per break power hour.

10 marks

Answer

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610 marks
a

What do you mean by multi-stage compression? State its advantages.

5 marks

Answer

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b

Differentiate between fan, blower and compressor.

5 marks

Answer

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OR
710 marks
a

Describe with neat sketches the working of a simple constant pressure open cycle gas turbine.

5 marks

Answer

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b

Enumerate the various uses of gas turbine.

5 marks

Answer

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810 marks
a

Enumerate the factors which should be considered while selecting a boiler.

5 marks

Answer

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b

List the advantages of high pressure boilers.

5 marks

Answer

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OR
9

Steam is expanded in a set of nozzles from 10 bar and 200°C to 5 bar. What type of nozzle is it? Neglecting the initial velocity, find minimum area of the nozzle required to allow a flow of 3 kg/s under the given conditions. Assume that expansion of steam to be isentropic.

10 marks

Answer

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10

In a De-Laval turbine steam issues from the nozzle with a velocity of 1200 m/s. The nozzle angle is 20°, the mean blade velocity is 400 m/s, and the inlet and outlet angles of blades are equal. The mass of steam flowing through the turbine per hour is 1000 kg. Calculate: a) Blade angles. b) Relative velocity of steam entering the blades. c) Tangential force on the blades. d) Power developed. e) Blade efficiency. Take blade velocity co-efficient as 0.8.

10 marks

Answer

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OR
1110 marks
a

Explain the difference between an impulse turbine and a reaction turbine.

5 marks

Answer

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b

Explain the reasons for inefficiency in surface condensers.

5 marks

Answer

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About this paper

This page contains the solved question paper with answers of THERMAL ENGINEERING from JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD for B.Tech MSNT III I, July/August - 2023, R16.

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