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TECH GENERAL — CH.18

Supercharging and TurbochargingAircraft & Engines — DGCA CPL practice questions

Question 1 of 5

A turbocharger is driven by:

A.Gearing from the crankshaft
B.The energy of the exhaust gases
C.An electric motor
D.Bleed air

All 5 questions — Supercharging and Turbocharging

Aircraft & Engines · DGCA CPL. The correct option is marked on each.

  1. Q1. A turbocharger is driven by:

    • A.Gearing from the crankshaft
    • B.The energy of the exhaust gases
    • C.An electric motor
    • D.Bleed air

    Why: The exhaust stream spins a turbine which drives the compressor — using waste energy, unlike a crankshaft-geared supercharger.

  2. Q2. The waste gate of a turbocharger controls boost by:

    • A.Restricting the air intake
    • B.Bypassing exhaust gas around the turbine
    • C.Varying the propeller pitch
    • D.Cooling the intake charge

    Why: Opening the waste gate sends exhaust overboard, slowing the turbine; closing it speeds the turbine and raises manifold pressure.

  3. Q3. As a turbocharged aircraft climbs, the automatic controller maintains manifold pressure by:

    • A.Progressively opening the waste gate
    • B.Progressively closing the waste gate
    • C.Enriching the mixture
    • D.Reducing RPM

    Why: Thinner air requires more turbine speed, so the Absolute Pressure Controller closes the waste gate as altitude increases.

  4. Q4. Critical altitude is the altitude at which:

    • A.The engine stops
    • B.The waste gate becomes fully closed and rated boost can no longer be maintained above it
    • C.Detonation begins
    • D.The propeller reaches fine pitch

    Why: Above critical altitude the fully-closed waste gate can no longer hold sea-level manifold pressure, and power falls with further climb.

  5. Q5. Density altitude is:

    • A.Pressure altitude corrected for non-standard temperature
    • B.Height above the ground
    • C.Indicated altitude corrected for instrument error
    • D.True altitude above sea level

    Why: Density altitude — pressure altitude corrected for temperature — is what the engine and wings actually 'feel'; high values degrade performance.