Module 15 Set-3

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

#2. WHICH TYPE OF ENERGY EXTRACT BY TURBINE ?

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

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

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




#6. VAPOUR LOCK ?

#7. THERMAL EFFICIENCY IS DEPENDS ON ________________________

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

#9. TURBOJET ENGINE PRODUCE BY ______________

#10. TO PREVENT SEIZURE OF CASE AND TURBINE




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

#12. THE THRUST OF GAS TUBINE ENGINE ________________

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

#14. THE THRUST OF ENGINE CALCULATED BY ____________

#15. TURBOSHAFT PREFERRED WHERE REQUIRED IS OF _______________




#16. PRESSURE RELIEF VALVE SYSTEMS

#17. PURPOSE OF EEC

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

#19. VAPOUR LOCK IS DUE TO _____________

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




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