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Exercise 10. True or false? Express your agreement or disagreement using “You are right”, “I’m of the same opinion”, “I can’t agree with you”.
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1. A rocket engine is not a jet engine; it uses atmospheric air as the propulsive fluid stream.
2. A rocket engine can not operate outside the earth’s atmosphere.
3. There are two basic types of rocket engines: liquid-propellant and solid-propellant rocket engines.
4. A rocket propulsion system may also be used as a primary power plant of an airplane.
5. The simplest type of air-breathing engines is the pulsejet engine.
6. The ramjet has found wide application in aviation.
7. The ramjet is more complicated than the pulsejet.
8. The pulsejet is suitable as an aircraft power plant because it has high fuel consumption.
9. Turbojet, turboprop and turbofan belong to the family of gas-turbine engines.
10. In a turbojet engine the diffuser takes the air and delivers it to the combustion chamber
11. The main function of the turbine is to provide power for the combustion chamber.
12. There are two types of compressors: centrifugal and axial compressors.
13. The majority of modern turbojets are equipped with centrifugal compressors.
14. The turboprop engine differs considerably from the turbojet.
15. The turboprop is lighter than a turbojet of equivalent size and power.
16. A variation of the turboprop engine is known as the turboshaft engine often used for powering guided missiles.
17. It is well known that there are liquid and solid-propellant rocket engines.
18. The turbofan engine doesn’t combine the features of both the turbojet and turboprop engines.
19. Turbofans are widely used in aviation, especially in large multi-engine aircraft.
Exercise 11. Answer the questions.
1. What can you say about the number and location of engines in the aircraft?
2. How are jet engines classified?
3. What is the difference between rocket and air-breathing engines?
4. What are two types of rocket engines?
5. What is the simplest type of air-breathing engines?
6. Is the pulsejet engine more complicated that the ramjet one?
7. What engines belong to the family of gas-turbine engines?
8. How are turbojets divided?
9. What are essential components of a turbojet engine?
10. What are the advantages of a turbofan engine?
Exercise 12. The most important types of engines are turbojet and turboprop engines. Let’s compare them according to the following parameters. (Find the additional information to do this task properly)
| Turbojet engines | Turboprop engines | |
| Thrust is produced by | the jet of hot gases ejected from the rear | the propellers |
| Weight | ||
| Size | ||
| Speed | ||
| Fuel consumption | ||
| Use in airplanes |
1. What engine is heavier?
2. What about their size?
3. What engine develops higher speed?
4. What engine consumes more fuel?
5. What airplanes are powered by turboprop engines?
6. What airplanes are powered by turbojet engines?
Exercise 13. Make questions to the underlined words
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1. Types of engines, their number and location on the airplane depend on the airplane performances.
2. Jet engines fall into two main classes: air-breathing engines and rocket engines.
3. The jet is produced by the combustion of the fuel in the compressed air.
4. Rockets find extensive use.
5. The simplest type of air-breathing engines is the ramjet engine.
6. The main components of the ramjet are: the diffuser, the combustion chamber and the jet nozzle.
7. Turbofans are widely used in aviation, especially in large multi-engine aircraft.
Exercise 14. Read the texts and write annotations.
A) The Ramjet Engine
The simplest type of jet engine is the ramjet. This engine consists of a diffuser, a combustion chamber, a discharge nozzle. The function of a diffuser is to convert the kinetic energy of the entering air into a pressure. The diffuser delivers the air at a static pressure higher than atmospheric pressure to the combustion chamber. There fuel is mixed with the air and ignited.
The burning causes the specific volume of the air to increase. The air is accelerated in the combustion chamber, where it burns at constant pressure to a high temperature. High temperature gases are delivered to the discharge nozzle to produce exit velocity greater than the entrance velocity. The fuel used in this type of engine is usually a liquid one.
Theoretically, ramjet operation is limited to altitudes below 90000 feet because atmospheric oxygen is necessary for combustion. The velocity that can be obtained by a ramjet engine is unlimited, theoretically
Really the faster it travels the better it operates and the more thrust it develops. Its speed is limited, however, at Mach 5,0 because the skin temperature has a harmful effect on the metals used in construction.
Ramjet engines are used in guided missiles. Ramjets are sometimes used experimentally on helicopters and in pods on fighters and bombers.
B)The Turbojet Engine
This engine consists of a diffuser, a mechanical compressor, a combustion chamber, a mechanical turbine and a discharged nozzle.
The function of a diffuser is to transform the kinetic energy of the entering air into a static pressure. The diffuser delivers its air to the mechanical compressor which compresses the air and delivers it to the combustion chamber. The high temperature gases then enter the turbine.
The turbine is directly connected to the compressor, and all the power developed by the turbine is absorbed by the compressor and the auxiliary apparatus. The main function of the turbine is to provide power for the mechanical compressor. After the gases leave the turbine, they enter the discharged nozzle and are ejected with a velocity greater than the flight velocity. This produces a thrust for propulsion.
The turbojet engine is product of one of the most intensive engineering development programs in aviation history. Since its introduction, the increase in its performance has been phenomenal and it is now in mass production for various airplanes.
It is now the standard power plant for nearly all high-speed military fighters and bombers.
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