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