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Journal of the Royal Naval Scientific Service. Volume 27, Number 2 ...

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Materials Development: Conde and Godfrey 117<br />

TABLE 3.<br />

Some Sub Zero Temperatures <strong>of</strong> Technological<br />

Importance.<br />

Chemical Substance<br />

or Process<br />

Liquifying Temp.<br />

Boiling Point or<br />

Operating Temp.<br />

°C<br />

GasjLiquid<br />

<strong>Volume</strong> Ratio<br />

Ammonia 334 —<br />

Propane 42 3 316<br />

Propylene 477 —<br />

Carbonyl Sulphide - 50 2 —<br />

Chlorine 55 —<br />

SO., dewaxing in<br />

refining<br />

- 60 —<br />

Hydrogen sulphide 59-7 —<br />

Carbon dioxide - 785 —<br />

Acetylene 84 —<br />

Ethane - 8S7 —<br />

Purification <strong>of</strong><br />

nitrous oxide<br />

Butyl rubber<br />

production<br />

- 90 —<br />

100 —<br />

Ethylene — 104 485<br />

Krypton —1532 —<br />

Methane —162 —<br />

Natural Gas 162 600<br />

Oxygen -183 843<br />

Argon - 186 —<br />

Fluorine -188 —<br />

Nitrogen 196 683<br />

Neon 246 —<br />

Dueterium 2496 —<br />

Hydrogen -253 850<br />

Helium —269 753<br />

packed hexagonal structure (e.g. magnesium,<br />

zinc) become brittle at low temperatures and<br />

face centred cubic metals (e.g. aluminium,<br />

copper, nickel) remain ductile. There are exceptions<br />

however and to demonstrate <strong>the</strong><br />

suitability <strong>of</strong> a material for low temperature<br />

service <strong>the</strong> properties must be evaluated. The<br />

growth <strong>of</strong> cryogenic engineering in <strong>the</strong> past<br />

thirty years has led to extensive literature on<br />

properties. Important properties at low temperatures<br />

include conventional mechanical<br />

strength, elastic modules and ductility, fatigue<br />

strength, impact behaviour, notch ductility<br />

and resistance to crack propagation, <strong>the</strong>rmal<br />

conductivity and expansion. In addition<br />

fabricability by brazing or welding and <strong>the</strong><br />

properties <strong>of</strong> <strong>the</strong> resulting joints are important<br />

as well as any adverse effects which may arise<br />

from structural changes in heat-affected zones<br />

<strong>of</strong> <strong>the</strong> parent material. The effect <strong>of</strong> lung term<br />

exposures at low temperatures is also significant<br />

as well as that <strong>of</strong> <strong>the</strong>rmal cycling from<br />

ambient to sub-zero levels since some materials,<br />

such as certain types <strong>of</strong> stainless steel, may<br />

be unstable and embrittle due to transformation<br />

effects. Economic factors are important<br />

in commercial applications such as liquid<br />

gas storage or transport but in specialised<br />

aerospace applications specific strength<br />

(strength/density ratio) may be <strong>of</strong> greater<br />

significance. Corrosion rates reduce with reduction<br />

in temperature and corrosion is not<br />

normally a serious factor but in certain instances<br />

may have to be taken into account<br />

since <strong>the</strong> corrosion rate in <strong>the</strong> cryogenic substance<br />

may be small but significant or corrosion<br />

may occur from <strong>the</strong> environment in contact<br />

with <strong>the</strong> outside <strong>of</strong> <strong>the</strong> cryogenic containment.<br />

The mechanical properties at low temperatures<br />

<strong>of</strong> a selection <strong>of</strong> metals and alloys are<br />

given in Table 4, and <strong>the</strong> chemical analyses <strong>of</strong><br />

<strong>the</strong>se materials are presented in Table 5. In<br />

general fatigue properties improve with deceasing<br />

temperature in parallel with <strong>the</strong> increase<br />

in tensile and yield properties. Conventional<br />

mechanical properties may indicate<br />

useful ductility at low temperatures but o<strong>the</strong>r<br />

data are required to assess behaviour under<br />

shock loads or triaxial stresses. Charpy Vee<br />

notch impact data toge<strong>the</strong>r with notched<br />

tensile strength (see Table 4) provide some<br />

indications <strong>of</strong> performance. The cast nickelaluminium-bronze<br />

in Table 4 shows evidence<br />

<strong>of</strong> serious degradation <strong>of</strong> impact value at low<br />

temperatures and hence must be considered<br />

suspect for cryogenic applications. To examine<br />

<strong>the</strong> notch ductility behaviour and resistance<br />

to crack propagation under severe service conditions<br />

<strong>of</strong> low temperature and complex<br />

stresses more sophisticated tests such as <strong>the</strong><br />

Tipper notched tensile test and <strong>the</strong> U.S. Navy<br />

tear test have been evolved. In such tests a

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