Summary

  • Jet engines consist of intake, compressor stage, combustor, and turbine stage. Air is compressed, fuel is introduced, and expansion creates thrust.
  • N2 compressor must be rotated to start the engine. This can be achieved using electricity or an air starter motor.
  • Startup malfunctions include hot starts (insufficient airflow) and hung starts (low RPM). A blowout cycle is necessary if a start fails to clear excess fuel. In-flight restarts rely on windmilling or assistance from other engines or APU.