Describe the function of subsonic air intakes

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Reference no: EM131389516 , Length: word count:1700

Aircraft Gas Turbine Science Assignment title: Gas Turbine performance

Learning Outcomes: On successful completion of this unit a learner will:

Understand the application of thermodynamic principles in the design of gas turbine modules and control systems.

  • Explain the design criteria for a gas turbine intake
  • Explain the design criteria for a gas turbine compressor
  • Explain the design criteria for a gas turbine combustion chamber

Assignment Task/title: Gas Turbine Performance

Demonstrate an understanding of the operating characteristics of air intakes, compressors and combustors as used in aircraft gas turbines.

Part 1 - Air intakes

You are to:

  • Describe the function of subsonic air intakes.
  • Describe the function of a supersonic air intake.
  • Explain how the formation of shock waves can influence their design and performance.
  • Include and refer to examples from service.

Part 2 - Compressors

You are to:

Describe the role of the rotor and stator.

Explain the nature and cause of compressor stall and surge.

Explain how surge can be prevented by using the following methods:

  • Variable inlet guide vanes
  • Variable stators
  • Bleed valves
  • Multi-shafting

Part 3 - Combustors

You are to:

  • Describe the main types of combustor used in aircraft gas turbine engines.
  • Compare their operating characteristics.
  • Describe the airflow pattern through a typical cannular combustor.
  • Explain the function of the simplex type burner, and suggest why the duplex burner was developed.

Report - The assignment is to be:

  • Written in formal report style, and include a content page, indicating the different report chapters and sections, an introduction and a conclusion
  • Accompanied by a bibliography with references using the Harvard Referencing system
  • A minimum of 1700 words (excluding appendices)
  • Word processed in Arial font size 12
  • Double spaced with titles and sub-titles
  • Supplemented with relevant labelled diagrams
  • Accompanied by the front sheets (which have been completed and signed)

Other information:

Resources - L.S.C. (ICAT)

Textbooks - The JET engine Rolls Royce ISBN-13: 9781119065999

Employer Links - An electrical/electronic/Aerospace programme is an essential building block that will provide the underpinning knowledge required for further study of appropriate applications.

Reference no: EM131389516

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len1389516

2/10/2017 2:35:20 AM

Write in 1700 words. Meet all requirements above. Written in formal report style, and include a content page, indicating the different report chapters and sections, an introduction and a conclusion. Describe and explain function of gas turbine air intakes and the influence of shockwave formation of gas flow characteristics. Describe the behaviour of airflow through an axial flow compressor and discuss the function of various types of stall protection. Explain the function of the combustor section and compare the differences between various types. Compare the function of simplex and duplex burners.

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