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Module 15 Set-3 | DGCA MODULE

Module 15 Set-3

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1 thought on “Module 15 Set-3”

Pravin

June 24, 2024 at 7:38 pm

Nice
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Module 15 Set-3

Results

#1. PURPOSE OF EEC

#2. PRESSURE RELIEF VALVE SYSTEMS

#3. WHICH TYPE OF ENERGY EXTRACT BY TURBINE ?

#4. TURBOJET ENGINE PRODUCE BY ______________

#5. TO PREVENT SEIZURE OF CASE AND TURBINE

#6. WHICH TYPE FILTER USE JUST BEFORE OIL PASS FROM THE SPRAY NOZZLE ON TO THE BEARING SURFACE __________

#7. THERMAL EFFICIENCY IS DEPENDS ON ________________________

#8. TYPE OF INLET DUCT USE IN GAS TURBINE ENGINE _______________

#9. VAPOUR LOCK ?

#10. CORROSIVE TYPE OF COMPOUND ARE WHICH TYPE OF PRODUCT ?

#11. VAPOUR LOCK IS DUE TO _____________

#12. TURBOSHAFT PREFERRED WHERE REQUIRED IS OF _______________

#13. THE ABILITY OF AN ENGINE TO RUN SMOOTHLY AND GIVE DESIRED PERFORMANCE AT ALL SPEED FROM IDLING TO FULL POWER OUTPUT ?

#14. THE THRUST OF ENGINE CALCULATED BY ____________

#15. WHICH TYPE DUCT HAVE A BELL SHAPE FUNNEL HAVING CAREFULLY ROUNDED SHOULDER WHICH OFFER PRACTICALLY NO AIR RESISTANCE ?

#16. THE THRUST OF GAS TUBINE ENGINE ________________

#17. IN CAN TYPE COMBUSTION CHAMBER THE AIR ENTER THROUGH THE ____________

#18. IN TURBOPROP ENGINE CONSTANT RPM IS FUNCTION OF ____________

#19. THE BASIC PARAMETER FOR DESCRIBING THE FUEL ECONOMY OF THE AIRCRAFT ENGINE _____________

#20. THE POWER PRODUCED BY A TURBINE ENGINE DEPENDS ON __________

1 thought on “Module 15 Set-3”

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