Module 14 Set-1

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#1. The basic gas turbine engine cycle is

#2. Supervisory EEC sends its output to the

#3. The majority of power in a free turbine engine is used to

#4. . The principle of operation of a DC ratio meter is

#5. The total power in a turboprop engine is the

#6. Propeller speed is measured from

#7. On a twin spool engine, the HP compressor is driven by

#8. How is fuel flow varied in a variable displacement pressure type pump?

#9. An increase in fuel flow through the impeller type fuel flow transmitter is measured by

#10. A modular constructed gas turbine engine means that

#11. The bleed valve on a engine at start up is

#12. E.G.T. thermocouples are usually made of

#13. The EEC is powered and able to operate via

#14. How does a boost gauge compensate for altitude changes?

#15. In a FADEC engine with a hydro mechanical fuel system, how is fuel flow controlled?

#16. Ratiometer pointer movement is achieved by

#17. . Modern oil pressure servo transmitters sense

#18. To measure oil temperature, which of the following would most likely be used?

#19. Manifold pressure is measured

#20. Where is EGT measured?

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