21-11. Turbine Engines
All questions: 171
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Questions for exams: 10
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1. A gas turbine blade is usually of the:
2. The accessory units driven by the accessory gearbox of a turbo-jet engine are the:
1) tacho-generator N1
2) tacho-generator N2
3) thrust reverser pneumatic motors
4) AC generator and its Constant Speed Unit
5) oil pumps
6) hydraulic pumps
7) high pressure fuel pumps
The combination regrouping all the correct statements is:
3. A convergent/divergent nozzle located in a gas turbine exhaust unit:
4. In a multi-spool turbofan engine, the fan is driven by:
5. Pressure recovery within the air intake means that:
