Double spiral devices have been employed as combustors for exceedingly
lean mixtures (for example, for methane, mixtures of fuel content cor
responding to less than 1/5 of the lower limit of flammability have be
en successfully burned), and the leanest mixture combustible is determ
ined by losses. For any given burner an optimum flow exists as at low
flows, losses are critical, and at high flows there is inadequate area
for heat transfer (also at high flows, large pressure losses occur).
Mathematical modeling of the spiral device demonstrates that radiation
is significant even at modest elevations in temperature and that spir
als of many turns help control these losses. With metal burners, condu
ction losses can be critical. Several parameters are presented to iden
tify design limits for spirals including wall emissivity, conductivity
, and thickness.