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. TURBOJET ENGINE PRODUCE BY ______________

#3. PRESSURE RELIEF VALVE SYSTEMS

#4. THERMAL EFFICIENCY IS DEPENDS ON ________________________

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




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

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

#8. TURBOSHAFT PREFERRED WHERE REQUIRED IS OF _______________

#9. PURPOSE OF EEC

#10. WHICH TYPE OF ENERGY EXTRACT BY TURBINE ?




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

#12. THE THRUST OF ENGINE CALCULATED BY ____________

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

#14. VAPOUR LOCK IS DUE TO _____________

#15. VAPOUR LOCK ?




#16. THE THRUST OF GAS TUBINE ENGINE ________________

#17. TO PREVENT SEIZURE OF CASE AND TURBINE

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

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

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




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