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The Art of the Helicopter John Watkinson - Karatunov.net

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208 <strong>The</strong> <strong>Art</strong> <strong>of</strong> <strong>the</strong> <strong>Helicopter</strong><br />

away from <strong>the</strong> spark plug. Unfortunately when charge is compressed <strong>the</strong> temperature<br />

will be raised and it can detonate instantly when ignited. This causes a rapid pressure<br />

step that creates shock waves travelling through <strong>the</strong> engine. A metallic ringing noise<br />

called ‘pinking’ or knock can be heard. If sustained, engine damage will result.<br />

<strong>The</strong> ability <strong>of</strong> a fuel to resist detonation must be matched to <strong>the</strong> compression ratio <strong>of</strong><br />

<strong>the</strong> engine it will be used in. <strong>The</strong> detonation resistance <strong>of</strong> fuel is measured in a special<br />

variable compression test engine. <strong>The</strong> fuel under test is used to drive <strong>the</strong> engine and<br />

<strong>the</strong> compression is increased until detonation commences. <strong>The</strong> engine is <strong>the</strong>n run on<br />

iso-octane, a relatively detonation resistant hydrocarbon, and this is steadily diluted<br />

with heptane, a detonation prone fuel, until detonation commences. <strong>The</strong> percentage<br />

<strong>of</strong> octane at which this takes place is <strong>the</strong> octane number <strong>of</strong> <strong>the</strong> fuel. Since <strong>the</strong> test was<br />

devised, more detonation resistant fuels have been developed, and <strong>the</strong> scale has been<br />

extended above 100 by extrapolation.<br />

Using fuel <strong>of</strong> inadequate octane number for <strong>the</strong> engine causes damage through detonation.<br />

<strong>The</strong> machine carries mandatory placards adjacent to <strong>the</strong> fuel fillers stating <strong>the</strong><br />

octane number <strong>of</strong> <strong>the</strong> fuel that must be used.<br />

A rich mixture helps to prevent detonation by reducing <strong>the</strong> temperature increase<br />

during compression. Fuels are <strong>of</strong>ten specified by two octane numbers; <strong>the</strong> second is<br />

for a rich mixture. For example, many piston helicopters burn 100/130 LL fuel. At<br />

normal mixtures this is 100 octane, but at full rich mixture it is 130 octane. LL stands<br />

for low lead. In <strong>the</strong> 1920s it was discovered that <strong>the</strong> addition <strong>of</strong> tetra-ethyl lead to<br />

fuel increased <strong>the</strong> octane number. Decades later it was proved that <strong>the</strong> resultant lead<br />

pollution was slowing <strong>the</strong> rate <strong>of</strong> brain development <strong>of</strong> children living near busy roads<br />

and less damaging alternatives have had to be found.<br />

Whilst fuel <strong>of</strong> inadequate octane rating causes damage, occasional use <strong>of</strong> higher<br />

octane fuel is acceptable. Prolonged use <strong>of</strong> high octane fuel may result in spark plugs<br />

being fouled by <strong>the</strong> octane-boosting additives. No power increase will be observed<br />

because <strong>the</strong> power output is determined by <strong>the</strong> engine design, particularly <strong>the</strong> compression<br />

ratio.<br />

<strong>The</strong> carburettor has to mix <strong>the</strong> air and fuel in <strong>the</strong> chosen proportion. Figure 6.9 shows<br />

that it is a fairly simple device. Engine power is controlled by throttle (3): a disc that<br />

pivots in <strong>the</strong> intake tract. With <strong>the</strong> throttle wide open, <strong>the</strong> pressure in <strong>the</strong> inlet manifold<br />

will be nearly atmospheric, whereas with <strong>the</strong> throttle closed down to <strong>the</strong> idle position,<br />

<strong>the</strong> manifold pressure will be near zero. Manifold pressure is displayed on a gauge in <strong>the</strong><br />

cockpit as it indicates <strong>the</strong> proportion <strong>of</strong> maximum power <strong>the</strong> engine is producing. <strong>The</strong><br />

pilot needs to know how much reserve power is necessary before committing himself<br />

to a manoeuvre needing higher power: a procedure called a power check.<br />

<strong>The</strong> result <strong>of</strong> throttling <strong>the</strong> engine is to reduce <strong>the</strong> flow <strong>of</strong> air through <strong>the</strong> carburettor.<br />

<strong>The</strong> fuel flow must remain proportional to <strong>the</strong> mass flow. This is done by <strong>the</strong> creation<br />

<strong>of</strong> a small constriction or venturi in <strong>the</strong> inlet tract. <strong>The</strong> air must go faster through <strong>the</strong><br />

smaller cross-section. This increases <strong>the</strong> dynamic pressure <strong>of</strong> <strong>the</strong> air. As <strong>the</strong> static and<br />

dynamic pressures sum to a constant, <strong>the</strong> static pressure must reduce, as described by<br />

Bernoulli’s <strong>the</strong>ory. <strong>The</strong> reduction in static pressure causes a pressure difference across<br />

<strong>the</strong> fuel in <strong>the</strong> carburettor body making it flow through a metering orifice or jet (2) and<br />

mix with <strong>the</strong> air. Clearly <strong>the</strong> depth <strong>of</strong> fuel could affect <strong>the</strong> pressure and <strong>the</strong> carburettor<br />

has a float valve (1) that admits fuel as it is used to prevent <strong>the</strong> level falling.<br />

<strong>The</strong> system is self-balancing, because greater airflow causes greater suction at <strong>the</strong><br />

venturi and increases <strong>the</strong> fuel flow. If <strong>the</strong> throttle is opened suddenly, <strong>the</strong> fuel inertia<br />

prevents a rapid increase in fuel delivery and <strong>the</strong> mixture will weaken momentarily.<br />

Weakening is prevented by <strong>the</strong> action <strong>of</strong> a small pump (4) that produces a jet <strong>of</strong> fuel<br />

when <strong>the</strong> throttle is opened quickly.

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