JNTU

JNTU B.Tech III AIRCRAFT SYSTEMS Previous Question Paper (December - 2018 - R15)

B.Tech | III | II | R15 | December - 2018

Answer PaperPaper Code: 126YVMaximum Marks: 75Time: 3 hours

Note: This question paper contains two parts A and B. Part A is compulsory which carries 25 marks. Answer all questions in Part A. Part B consists of 5 Units. Answer any one full question from each unit. Each question carries 10 marks and may have a, b, c as sub questions.

Part A

125 marks
a

Mention the different levels of integration.

2 marks

Answer

The different levels of integration include physical integration, functional integration, and data/information integration.

b

What is the need for systems to be integrated?

3 marks

Answer

Systems are integrated to reduce overall weight, minimize complexity, improve operational efficiency, and enhance reliability by sharing resources such as power, data, and cooling. Integration also allows for better coordination between subsystems, leading to optimized aircraft performance and reduced maintenance requirements.

c

What are the generic parts of a typical alternating current (A.C.) aircraft electrical system?

2 marks

Answer

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d

Which control surfaces provide primary flight control in pitch, roll and yaw?

3 marks

Answer

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e

Give few names of hydraulic fluids used for commercial aircrafts.

2 marks

Answer

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f

Determination of the flow rate is a more difficult problem. Why?

3 marks

Answer

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g

What are the functions of PRSOV?

2 marks

Answer

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h

What is the need for a controlled environment?

3 marks

Answer

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i

What is FADEC? What is its function?

2 marks

Answer

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j

What are the characteristics of fuel systems?

3 marks

Answer

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Part B

2

What are the typical operating environments conditions for an aircraft system and its subsystems?

10 marks

Answer

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OR
3

Explain about the interdependence of aircraft systems.

10 marks

Answer

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4

What are the different electrical services covered by electrical power generated by an aircraft? Explain.

10 marks

Answer

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OR
5

Explain about ‘push-pull control system’ method of connecting the pilot’s controls to the rest of the flight control system.

10 marks

Answer

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6

Explain about Panavia tornado hydraulic system in detail.

10 marks

Answer

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OR
7

What are the design requirements of aircraft hydraulic system? Explain.

10 marks

Answer

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8

Draw the schematic of a simplified bleed air system and associated aircraft systems. Explain the working of it.

10 marks

Answer

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OR
9

Explain the working of a vapor cycle refrigeration system.

10 marks

Answer

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10

Explain about the following input signals:

10 marks
a

Throttle position

2 marks

Answer

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b

Air data

2 marks

Answer

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c

Total temperature

2 marks

Answer

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d

Engine speed

2 marks

Answer

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e

Engine temperature

2 marks

Answer

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OR
11

What is the typical starting sequence of an engine? Explain.

10 marks

Answer

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About this paper

This page contains the question paper of AIRCRAFT SYSTEMS from JNTU for B.Tech AE III II, December - 2018, R15.

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