Thrust Augmentation
Thrust Augmentation
Thrust Augmentation
AIM
Aim of this presentation is give a brief introduction about the thrust augmentation in gas turbine engines.
Theory
T
=
2 1
T = Thrust w = Weight per unit time of air flow 2 = Exhaust Air speed 1 = Inlet Air Speed
Water Injection
Done by increasing weight of air flow passing through engine. Boosted 10% - 30% of thrust Mixture of De mineral water and Alcohol
Disadvantages very heavy Thermal shock to the engine Compressor blade can be effect on erosion. Generally water air ratios are 1-5 lbs. of water to 100 lbs. of air.
AFTERBURNING
Use in Turbo Jets and Turbo fan engine types. Periodically increase in thrust. Much similar to Ramjet operation Principle of Afterburning is increasing exit air velocity.
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Specific Requirements
Large Temperature Rise Low Dry Loss Wide Temperature Modulation
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Construction
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Construction cont.
Afterburner fuel pump Afterburner fuel control Pressurization valve Spray nozzles or Spray bars Ignition system Flame hoders Variable exhaust nozzle Connections Screech liner
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Ignition Systems
Hot Streak ignition Torch ignition Electric Spark ignition
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Conclusion
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END
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