JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD

JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD B.Tech III AIRCRAFT SYSTEMS Previous Question Paper (April - 2018 - R15)

B.Tech | III | II | R15 | April - 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

Define Airframe system.

2 marks

Answer

An Airframe system refers to the collection of mechanical, electrical, and structural components integrated into an aircraft's primary structure to support flight operations, including flight control, landing gear, environmental control, and utility systems.

b

List out various information levels in systems.

3 marks

Answer

The information levels in aircraft systems are generally categorized as follows:

  • Sensor/Transducer Level: Data acquisition from physical parameters.
  • Processing/Computation Level: Analysis and logic execution by computers.
  • Display/Interface Level: Presentation of information to the crew.
  • Actuation Level: Execution of commands based on processed information.
c

What do you mean by Q feel?

2 marks

Answer

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d

Write a short note on FBW control laws.

3 marks

Answer

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e

Discuss the system loads relevant to hydraulic systems.

2 marks

Answer

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f

What are the principle components of hydraulic system?

3 marks

Answer

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g

Explain engine anti icing concept.

2 marks

Answer

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h

Draw a schematic layout of Pneumatic circuit.

3 marks

Answer

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i

Define EGT and its indication.

2 marks

Answer

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j

How the off take effects on engine performance?

3 marks

Answer

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PART - B

210 marks
a

Describe the interdependence of aircraft system with a suitable example.

5 marks

Answer

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b

Give a brief description on aspects of safety and integrity.

5 marks

Answer

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OR
3

Enumerate the major aircraft systems and their sub systems of a civil transport aircraft.

10 marks

Answer

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4

Explain Electro hydrostatic actuation in aircraft control system. Differentiate with electro mechanical actuation with the aid of sketches.

10 marks

Answer

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OR
510 marks
a

Explain how the aircraft electrical systems have control over power generations and voltage regulation?

5 marks

Answer

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b

Distinguish between primary and secondary power distribution.

5 marks

Answer

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610 marks
a

Explain the operating principle of aircraft hydraulic system with neat schematic layout.

5 marks

Answer

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b

What is the significance of Flight control actuation? Explain any two types of actuations.

5 marks

Answer

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OR
7

With a neat schematic diagram explain the application of hydraulic system in landing gear and brake management systems.

10 marks

Answer

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810 marks
a

Does all aircraft need cabin pressurization system? What are its advantages and disadvantages?

5 marks

Answer

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b

Explain the operating principle and constructional features of Bleed Air control in pneumatic system.

5 marks

Answer

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OR
9

What are various types of Air cycle refrigeration systems? Explain any two types with neat sketches. Mention their advantages and disadvantages.

10 marks

Answer

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10

Explain the following terms related to engine control system:

10 marks
a

Engine monitoring sensors

5 marks

Answer

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b

Engine monitoring indicators.

5 marks

Answer

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OR
11

Describe in detail, the fuel system characteristics and operating modes of control engine components.

10 marks

Answer

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This page contains the solved question paper with answers of AIRCRAFT SYSTEMS from JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD for B.Tech AE III II, April - 2018, R15.

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