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Quiz on Composites in Aircraft Construction

Total questions: 21

Worksheet time: 11mins

Name
Class
Date
1.

What was the last significant aircraft to use timber construction?

a)

De Havilland Comet

b)

Boeing 737

c)

Airbus A320

d)

The Mosquito

2.

Which material was first integrated by Boeing into their civilian aircraft in 1958?

a)

Fibreglass

b)

Aramid Fibre

c)

Carbon Fibre

d)

Metal Matrix Composites

3.

What is a key disadvantage of carbon fibre in aircraft?

a)

High density

b)

Sudden and catastrophic failure

c)

Low resistance to corrosion

d)

Poor tensile strength

4.

Which fibre is better known under the trade name Kevlar?

a)

Boron Fibre

b)

Glass Fibre

c)

Carbon Fibre

d)

Aramid Fibre

5.

What is the primary role of the matrix in a composite?

a)

Reduce weight

b)

Increase electrical conductivity

c)

Provide tensile strength

d)

Bind the fibres together

6.

Which of the following is NOT a property of composites?

a)

High density

b)

High strength

c)

Outstanding corrosion resistance

d)

Excellent fatigue resistance

7.

What type of composite uses a metal matrix?

a)

Carbon Fibre Composites

b)

Epoxy Composites

c)

Metal Matrix Composites (MMC)

d)

Aramid Fibre Composites

8.

What is the main advantage of using hollow fibres in composites?

a)

Enhance electrical conductivity

b)

Increase compressive strength

c)

Reduce cost

d)

Improve thermal properties

9.

What is the purpose of a 'smart patch' in aircraft repair?

a)

Increase tensile strength

b)

Transmit information about serviceability

c)

Reduce weight

d)

Enhance thermal resistance

10.

Which material is used in the fan cowls of jet engines for protection?

a)

Aramid fibres

b)

Glass fibres

c)

Ceramic fibres

d)

Carbon fibres

11.

Which of the following is a common application of carbon fibre composites?

a)

Construction of bridges

b)

Manufacturing of sports equipment

c)

Production of glass bottles

d)

Making of ceramic tiles

12.

What is the primary benefit of using composites in the automotive industry?

a)

Lower tensile strength

b)

Increased fuel efficiency

c)

Reduced color options

d)

Higher production costs

13.

Which process is commonly used to manufacture composite materials?

a)

Hand lay-up

b)

Injection molding

c)

Extrusion

d)

Die casting

14.

What is the main function of fibres in a composite material?

a)

Provide thermal insulation

b)

Enhance tensile strength

c)

Reduce production costs

d)

Improve electrical conductivity

15.

Which composite material is known for its use in bulletproof vests?

a)

Metal Matrix Composites

b)

Aramid Fibre

c)

Glass Fibre

d)

Carbon Fibre

16.

What is a common disadvantage of using composites in construction?

a)

High weight

b)

Low durability

c)

High cost

d)

Poor thermal resistance

17.

What is a significant advantage of using composites in aerospace applications?

a)

Improved fuel efficiency

b)

Increased weight

c)

Reduced durability

d)

Higher maintenance costs

18.

Which of the following is a typical characteristic of glass fibre composites?

a)

High corrosion resistance

b)

Low tensile strength

c)

Excellent thermal insulation

d)

High electrical conductivity

19.

What is the main role of the reinforcement in a composite material?

a)

Provide structural strength

b)

Reduce manufacturing costs

c)

Improve thermal conductivity

d)

Enhance electrical properties

20.

Which of the following materials is commonly used in the construction of wind turbine blades?

a)

Aluminum

b)

Glass fibre composites

c)

Steel

d)

Wood

21.

Which property of carbon fibre makes it suitable for use in aerospace applications?

a)

Low cost

b)

High density

c)

Low thermal expansion

d)

High electrical conductivity