Combustion Chamber Cooling Method and System
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[0018]Referring now to the accompanying drawings, there is illustrated a cooling system, generally indicated as 10, for use with a conventional gas turbine combustion assembly as illustrated in FIG. 1, which comprises an inner flame tube F which is fed with gaseous fuel via a feed pipe P, the flame tube F being surrounded by an outer sleeve S into which pressurized air is supplied, and injected into the flame tube F via an array of holes in the outer wall of the flame tube F.
[0019]Referring now in particular to FIGS. 2 and 3, the system 10 is illustrated in combination with the conventional flame tube F and outer sleeve S, the system 10 comprising a vessel 12 which is shaped and dimensioned to be concentrically located about the outer sleeve S, in order to substantially enclose the outer sleeve S. The system 10 further comprises a fluid inlet 14 communicating with the vessel 12 at one end thereof, and a fluid outlet 16, preferably communicating with the vessel 12 at an opposed end t...
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