Quiz ATPL | Pagina 23 | Aircraft General Knowledge -

In a compressor stage of a jet engine, the sequence is:	4 risposte
In the axial flow compressor of a turbo-jet engine, the flow duct is tapered. Its shape is calculated so as to:	4 risposte
In the stator of a turbine, the speed V and static pressure Ps vary as follows:	4 risposte
The purpose of a compressor bleed valve is to prevent surging:	4 risposte
A 'fan' stage of a ducted-fan turbine engine is driven by:	4 risposte
The diffuser in a centrifugal compressor is a device in which the:	4 risposte
The fan in a high by-pass ratio turbo-jet engine produces:	4 risposte
A reverse thrust door warning light on the flight deck instrument panel illuminates when:	4 risposte
In a single spool gas turbine engine, the compressor RPM is:	4 risposte
When the combustion gases pass through a turbine the:	4 risposte

ATPL - Airline Transport Pilot license - Aircraft General Knowledge - Airframe, Systems, Powerplant Pagina 23