Module 15 Set-3

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#1. PRESSURE RELIEF VALVE SYSTEMS

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

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

#4. VAPOUR LOCK ?

#5. VAPOUR LOCK IS DUE TO _____________




#6. TO PREVENT SEIZURE OF CASE AND TURBINE

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

#8. TURBOSHAFT PREFERRED WHERE REQUIRED IS OF _______________

#9. TURBOJET ENGINE PRODUCE BY ______________

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




#11. THERMAL EFFICIENCY IS DEPENDS ON ________________________

#12. THE THRUST OF GAS TUBINE ENGINE ________________

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

#14. WHICH TYPE OF ENERGY EXTRACT BY TURBINE ?

#15. THE THRUST OF ENGINE CALCULATED BY ____________




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

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

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

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

#20. PURPOSE OF EEC




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