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Section 12.11

Fuel Systems

Crash-resistant (self-sealing) tanks and breakaway couplings, boost pumps and crossfeed, and capacitance quantity.

Notes

Fuel systems, summary notes

Main ideas
  • Fuel is held in tanks (often CRASH-RESISTANT, self-sealing bladder tanks with breakaway couplings to prevent post-crash fire); boost pumps deliver fuel under positive pressure to the engine(s).
  • A crossfeed lets either engine draw from either tank on twins; tanks are vented, have water drains at their low points, and fuel is filtered.
  • Fuel QUANTITY is measured by capacitance probes; fuel flow, pressure and low-level/low-pressure warnings are provided.
  • Crash-resistant fuel systems (CRFS), flexible bladder cells, self-sealing breakaway valves and frangible fittings, are a major helicopter safety feature to prevent fuel-fed fires in a survivable crash.
  • Refuel/defuel and bonding/earthing for static control follow the same rules as fixed-wing.
  • ⚠ Exam trap: helicopters emphasise CRASH-RESISTANT fuel systems (self-sealing bladder tanks + breakaway couplings) to prevent post-impact fire; fuel quantity is by capacitance probes, and crossfeed balances a twin.
Solved examples
  1. What features make a helicopter fuel system 'crash-resistant', and why does it matter?

    A crash-resistant fuel system uses flexible, self-sealing bladder tanks that resist tearing, plus breakaway (frangible) couplings and self-sealing valves at every connection so lines separate cleanly and seal rather than spilling fuel. This prevents fuel spraying onto hot or sparking components in an otherwise-survivable crash, dramatically reducing the risk of a post-impact fire, historically a major cause of helicopter accident fatalities.

Mind map

Fuel systems concept map

Fuel Systems

Quiz

Fuel systems quiz

Fuel Systems, quiz

Ref 12.118 of 16Pass 75%
  1. 1. Helicopter fuel tanks are often

    Crash-resistant self-sealing bladder cells
    Rigid glass tanks
    Open containers
  2. 2. Breakaway (frangible) couplings in a crash-resistant fuel system

    Separate cleanly and self-seal in a crash
    Weld shut
    Are non-structural
  3. 3. Fuel quantity is measured by

    Capacitance probes
    Float switches only
    A dipstick in flight
  4. 4. Boost pumps are fitted to

    Deliver fuel under positive pressure and prevent vapour lock
    Cool the cabin by circulating fuel through a heat exchanger in the environmental system
    Charge the battery from the pump generator whenever the engine driven pumps are running
  5. 5. On a twin, a crossfeed allows

    Either engine to draw from either tank
    Only the left engine to run
    Fuel jettison only
  6. 6. Fuel tanks are vented to

    Keep the ullage at ambient pressure
    Increase pressure
    Store extra fuel
  7. 7. The main purpose of a crash-resistant fuel system is to

    Prevent a post-impact fuel-fed fire
    Increase range
    Cool the engine
  8. 8. Water is removed from fuel by

    Draining the tank low points before flight
    Adding more fuel
    Venting air