15.5 Combustion section
15.5 Combustion section
Quiz
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The major part of this energy developed during combustion process is required to drive,…..?
- Fuel pump
- The compressor
- To drive turbine
This type of engine develop its 100 % thrust by accelrating the gasses out of the ?nozzle ?
- Turbo fan
- Turbo jet
- Turboshaft
In the combustion chamber pressure and volume are…….?
- Static pressure and volume remains constant
- Static pressure and volume decreases
- Static pressure decreases slightly and volume increases
Which component creates a vortex in a gas turbine flame tube ?
- Swirl vanes
- Louvers
- Tertiary holes
The heat released by a combustion chamber is dependent on ?
- Pressure and speed of flame
- Volume of the combustion area
- Pressure of mixture
Which air is used for combustion ?
- Secondary
- Primary
- Primary and secondary
Modern Gas turbine engines usually have an ………?
- Can-annular type
- Can-type combustion chamber
- Annular combustion chamber
Which type of fuel nozzle is required in the use of flow divider ?
- Duplex nozzle
- Air blast simplex
- Simplex nozzle
Which type of combustion chamber is typicaly used on turbo shaft and Apu ?
- Can-type combustion chamber
- Can-annular type
- Annular type
Combustion section is located between…………….. ?
- Exhaust section and turbine section
- Exhaust and compressor
- Compressor and turbine