Questions and Answers
Which section is the combustion section typically located between?
Compressor diffuser and turbine section
What is the primary function of the combustion chamber?
To mix fuel and air
Where is the fuel injection system located?
In the combustion chamber case
What is the typical ignition source for gas turbines?
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What important task does the fuel drainage system accomplish?
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What is the primary function of the high energy capacitor discharge system in a gas turbine engine?
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Where are the fuel nozzles typically located in a gas turbine engine?
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What are the basic elements of a typical combustor in a gas turbine engine?
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Where is the combustion section typically located in a gas turbine engine?
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Study Notes
Combustion Section
- Typically located between the compressor and turbine sections in a gas turbine engine
Combustion Chamber
- Primary function: to mix fuel and air, ignite, and sustain combustion
Fuel Injection System
- Located in the combustion chamber to inject fuel into the combustion zone
Ignition Source
- Typical ignition source for gas turbines: high energy capacitor discharge system
Fuel Drainage System
- Accomplishes the important task of draining excess fuel from the combustion chamber
High Energy Capacitor Discharge System
- Primary function: to provide the high voltage necessary to create a spark for ignition in a gas turbine engine
Fuel Nozzles
- Typically located in the combustion chamber to atomize and distribute fuel
Combustor Elements
- Basic elements of a typical combustor in a gas turbine engine: combustion chamber, fuel nozzles, and igniter
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