Look at the text again and answer the questions



1. What can be housed inside the fuselage structure?

2. What loads act on the fuselage in flight?

3. What are the main members of the fuselage structure?

4. How is the skin joined to the stringers and formers?

5. What purposes are the bulkheads used for?

6. What is the best material for the airplane fuselage?

7. What complicates designer’s task?

8. What is the function of the stressed skin?

 

Read these definitions and remember them.

 

Longeron – a main longitudinal member of the fuselage

Rivet – a metal pin that is inserted into holes in larger parts to be joined, and then

             compressed to produce a permanent fastening

Skin – a material which covers the structure of an airplane

Airframe– the basis structure of a plane, including fuselage, wings and so on.

Bulkhead – an upright partition that serves to divide the airplane into compartments

              and to provide structural strength.

Stringer – a longitudinal member that shapes and strengthens the skin.

 

Vocabulary Focus

Give your own definitions for the words from the text.

Crew, fuel, payload, wheel well, assembly, to rivet, aerodynamic load.

A) Check if you know the meaning of the following verbs.

To space, to resist, to reinforce, to rely, to depend, to divide, to cover, to derive.

 

b) Think of other nouns they can go with. Make up your own sentences with the verbs from a).

3. Match the synonyms. Watch out! There is an extra word in the column B.

A                                       B

                              cover                               pressure

                              derive                             strengthen

                              divide                               contain

                             reinforce                             split

                               resist                                frame

                             bulkhead                            shield

                                 bay                               withstand

                             assembly                           obtain

                                stress                           compartment

                                house                              basis

                                                                             unit

In the text, find the words with the meaning opposite to these words.

Started; flexible; different; insufficient; weak; simplify; inner.

 

Choose the best alternative to fill the gaps in these sentences.

1. The main _______ members, longerons, provide the basis of the fuselage strength.

a) transverse                    b) longitudinal                   c) solid

2. Both the monocoque and semimonocoque fuselage structures are referred to as  

 _______ construction.

a) monolithic                  b) welded                           c) stressed-skin

3. The designer’s task is _____ by the presence  of doors, windows, wheel wells, etc.

a) complicated               b) improved                        c) simplified

4. The _____ type fuselage consists of a welded tubular structure covered with skin.

a) monocoque                b) girder                              c) truss

5. _____ are solid or semisolid members placed where greater stresses occur.

a) stringers                   b) bulkheads                         c) longerons

6. Longerons and stringers are _____ to the skin and they carry the main portion of     

the  load.

a) welded                     b) bolted                               c) riveted

 

 

Speaking

Work in group. Imagine that your team is to design a new business airplane for 10 passengers. What type of fuselage answers this purpose best of all? Give your reasons. Compare different types of fuselage structure and give pros and cons of using your choice.

Writing

Translate in a written form.

Three Axes of an Airplane

An aircraft can rotate around three axes which are perpendicular to each other and intersect at the plane’s center of gravity (CG). To control the position and direction a pilot must be able to control rotation about each of them.

Vertical axis. The vertical axis passes through the plane from top to bottom. Rotation about this axis is called yaw. Yaw changes the direction the aircraft nose to the left or right. By using the rudder the pilot can cause the airplane to yaw to either side.

Longitudinal axis. The longitudinal axis passes through the plane from nose to tail. Rotation about this axis is called bank or roll. Bank changes the orientation of the aircraft’s wing with respect to the downward force of gravity. The pilot changes bank angle by increasing the lift on one wing and decreasing it on the other. This differential lift causes bank rotation around the longitudinal axis. The ailerons are the primary control of bank.

Lateral axis. The lateral axis passes through the plane from wingtip to wingtip. Rotation about this axis is called pitch. The nose and the tail surfaces of the airplane can move up and down around the lateral axis. The pilot can use the elevators to raise or lower the nose of the airplane. 

UNIT 10

Preparing to Read

Power Plant

 


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