Module 15 Set-3

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#1. THE THRUST OF GAS TUBINE ENGINE ________________

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

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

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

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




#6. TO PREVENT SEIZURE OF CASE AND TURBINE

#7. PURPOSE OF EEC

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

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

#10. THERMAL EFFICIENCY IS DEPENDS ON ________________________




#11. VAPOUR LOCK ?

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

#13. TURBOSHAFT PREFERRED WHERE REQUIRED IS OF _______________

#14. WHICH TYPE OF ENERGY EXTRACT BY TURBINE ?

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




#16. THE THRUST OF ENGINE CALCULATED BY ____________

#17. PRESSURE RELIEF VALVE SYSTEMS

#18. VAPOUR LOCK IS DUE TO _____________

#19. TURBOJET ENGINE PRODUCE BY ______________

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




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