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The Art of the Helicopter John Watkinson - Karatunov.net

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

In <strong>the</strong> case <strong>of</strong> an engine, <strong>the</strong> input power is <strong>the</strong> heat released by burning <strong>the</strong> fuel.<br />

In practical engines, this exceeds <strong>the</strong> output shaft power considerably. <strong>The</strong> percentage<br />

<strong>of</strong> <strong>the</strong> <strong>the</strong>rmal energy in <strong>the</strong> fuel that emerges as shaft power is <strong>the</strong> <strong>the</strong>rmal efficiency<br />

<strong>of</strong> <strong>the</strong> engine. <strong>The</strong> waste heat has to be removed by a cooling system to prevent <strong>the</strong><br />

temperature <strong>of</strong> <strong>the</strong> engine rising to <strong>the</strong> point where components are damaged. Cooling<br />

systems waste fur<strong>the</strong>r power in driving fans and pumps and usually increase <strong>the</strong> drag<br />

<strong>of</strong> <strong>the</strong> airframe.<br />

Given <strong>the</strong> necessary high power to weight ratio in helicopters, <strong>the</strong> power plant and<br />

fuel form a significant part <strong>of</strong> <strong>the</strong> all-up weight. It is beneficial to explore means to<br />

improve <strong>the</strong> <strong>the</strong>rmal efficiency <strong>of</strong> <strong>the</strong> engine. Not only will this reduce <strong>the</strong> weight <strong>of</strong><br />

<strong>the</strong> fuel to be carried for a given range, but it may also allow <strong>the</strong> cooling system to be<br />

lighter, to consume less power and to cause less intake drag. Thus a small improvement<br />

in <strong>the</strong>rmal efficiency may result in a significant increase in performance.<br />

Passenger aircraft may be compared using specific air range (<strong>the</strong> mass <strong>of</strong> fuel used per<br />

unit <strong>of</strong> distance), but in a hovering helicopter this figure is meaningless. In helicopters,<br />

it may be better to compare <strong>the</strong> power actually used to hover with <strong>the</strong> <strong>the</strong>oretical power<br />

needed by an ideal rotor under <strong>the</strong> same conditions.<br />

2.9 Gases and <strong>the</strong> atmosphere<br />

<strong>The</strong> atmosphere is <strong>the</strong> medium in which helicopters fly but it is also one <strong>of</strong> <strong>the</strong> fuels<br />

for <strong>the</strong> engine and <strong>the</strong> occupants brea<strong>the</strong> it. It is a highly variable medium that is<br />

constantly being forced out <strong>of</strong> equilibrium by heat from <strong>the</strong> sun and in which <strong>the</strong><br />

pressure, temperature, and humidity can vary with height and with time and in which<br />

winds blow in complex time- and height-variant patterns. <strong>The</strong> effect <strong>of</strong> atmospheric<br />

conditions on flight is so significant that no pilot can obtain qualifications without<br />

demonstrating a working knowledge <strong>of</strong> <strong>the</strong>se effects.<br />

<strong>The</strong> atmosphere is a mixture <strong>of</strong> gases. About 78% is nitrogen–arelativelyunreactive<br />

element – whereas about 21% is oxygen, which is highly reactive. <strong>The</strong> remainder is a<br />

mixture <strong>of</strong> water in <strong>the</strong> gaseous state and various o<strong>the</strong>r traces. <strong>The</strong> reactive nature <strong>of</strong><br />

oxygen is both good and bad. <strong>The</strong> good part is that it provides a source <strong>of</strong> energy<br />

for life and helicopters alike because hydrocarbons can react with oxygen to release<br />

energy. <strong>The</strong> bad part is that many materials will react with oxygen when we would<br />

ra<strong>the</strong>r <strong>the</strong>y didn’t. Chemically, combustion and corrosion are one and <strong>the</strong> same thing.<br />

<strong>The</strong> difference is based on <strong>the</strong> human reaction to <strong>the</strong> chemical reaction.<br />

Gases are <strong>the</strong> highest energy state <strong>of</strong> matter, for example <strong>the</strong> application <strong>of</strong> energy<br />

to ice produces water and <strong>the</strong> application <strong>of</strong> more energy produces water vapour. <strong>The</strong><br />

reason that a gas takes up so much more room than a liquid is that <strong>the</strong> molecules<br />

contain so much energy that <strong>the</strong>y break free from <strong>the</strong>ir neighbours and rush around at<br />

a high speed, which is a function <strong>of</strong> absolute temperature. As Figure 2.12(a) shows, <strong>the</strong><br />

innumerable elastic collisions <strong>of</strong> <strong>the</strong>se high speed molecules produce pressure on <strong>the</strong><br />

walls <strong>of</strong> any gas container. In fact <strong>the</strong> distance a molecule can go without a collision,<br />

<strong>the</strong> mean free path, is quite short at atmospheric pressure. Consequently gas molecules<br />

also collide with each o<strong>the</strong>r elastically, so that if left undisturbed, in a container at a<br />

constant temperature, every molecule would end up with essentially <strong>the</strong> same energy<br />

and <strong>the</strong> pressure throughout would be constant and uniform.<br />

Pressure is measured by physicists and by engineers in units <strong>of</strong> force per unit <strong>of</strong> area<br />

using imperial units <strong>of</strong> pounds per square inch or SI units <strong>of</strong> Newtons per square metre.<br />

At sea level, <strong>the</strong> atmosphere exerts a pressure <strong>of</strong> about 15 pounds per square inch<br />

and has a density <strong>of</strong> about 0.075 pounds per cubic foot or in metric units about

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