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Section 14.4

Starting & Ignition Systems

Pneumatic and electric starting, high-energy capacitor-discharge ignition, the start sequence and ignition-system safety.

Notes

Starting & ignition systems, summary notes

Main ideas
  • Most large turbine engines use an AIR-TURBINE (pneumatic) starter, supplied from the APU, a ground cart or a cross-bleed from a running engine; a starter control (start) valve admits the air, and the start sequence is managed by the EEC. Smaller engines and APUs use an electric starter or starter-generator.
  • Turbine ignition uses a HIGH-ENERGY capacitor-discharge system: an ignition exciter charges a capacitor and dumps it as a powerful spark at the igniter plug (a surface-discharge plug), needed only to light the engine, combustion is then self-sustaining.
  • There are normally two independent ignition systems (two exciters/igniters) for reliability; ignition is armed automatically for start and can be selected CONTINUOUS for flame-out protection (icing, heavy rain, take-off and landing).
  • The start sequence (systems view): starter drives N2 → ignition on → fuel on at light-up speed → EGT rises → engine accelerates to idle → starter and ignition off. Faults the systems must protect against are the hot start (EGT exceedance), hung start (stalls below idle) and wet start (no light-up).
  • SAFETY: the exciter stores a LETHAL electrical charge. Before handling igniter leads or plugs, switch off the system and wait the specified time (and discharge as instructed) for the capacitor to bleed down; also respect pneumatic-starter duct pressure/heat and the running/rotating hazards.
  • ⚠ Exam trap: turbine ignition is HIGH-ENERGY capacitor-discharge storing a lethal charge, observe the safety wait/discharge time before touching igniters; large engines are normally PNEUMATICALLY (air-turbine) started, and ignition is switched off once the engine is self-sustaining.
Solved examples
  1. Before disconnecting an igniter lead after ground runs, what safety step is essential and why?

    The ignition exciter is a high-energy capacitor-discharge unit that stores a potentially lethal charge even after the system is switched off. You must switch off and de-energise the ignition system and wait the manufacturer's specified safety time (and follow any discharge procedure) so the capacitor bleeds down before touching the igniter lead or plug, otherwise a stored discharge could cause a fatal shock.

Simulation

Turbine engine start sequence

Turbine Engine Start SequenceFull screen ↗
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Mind map

Starting & ignition concept map

Starting & Ignition Systems

Quiz

Starting & ignition systems quiz

Starting & Ignition Systems, quiz

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  1. 1. Most large turbine engines use a:

    Pneumatic (air-turbine) starter
    Hand crank
    Hydraulic ram starter
  2. 2. Turbine ignition is a:

    High-energy capacitor-discharge system
    Low-energy magneto system
    Glow-plug system
  3. 3. The main safety hazard of a turbine ignition system is:

    A lethal stored electrical charge in the exciter
    Excess oil
    High fuel pressure only
  4. 4. Before handling igniter leads you must:

    Switch off and wait the specified time to discharge
    Do nothing special
    Increase ignition power
  5. 5. Once the engine is self-sustaining, ignition is:

    Switched off
    Left continuously on always
    Increased
  6. 6. Continuous ignition is selected:

    For flame-out protection (icing, rain, T/O and landing)
    Only during shutdown, so that any residual fuel in the combustor is burnt off safely
    Never in normal service, being reserved for engine ground running and test cell work
  7. 7. Turbine engines normally have:

    Two independent ignition systems for reliability
    One system only
    No ignition system
  8. 8. The start valve controls:

    Air to the pneumatic starter
    Fuel to the burners
    Oil to the bearings