Recuperated turbine engine

Power plants – Combustion products used as motive fluid – With exhaust treatment

Patent

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Details

165 9, F02C 710

Patent

active

044740000

ABSTRACT:
The disclosure relates to an improved recuperative heat exchanger for a turbine engine. Heat exchanger modules have discrete passages therein for the relatively high pressure compressor discharge air and relative low pressure exhaust gases. A continuous seal is provided at each end of the exhaust passages in the heat exchanger that is expandable into positive engagement with the heat exchange module.

REFERENCES:
patent: 3401740 (1968-09-01), Trudeau
patent: 3692097 (1972-09-01), Penny
patent: 3893505 (1975-07-01), Fujikake et al.
patent: 4213297 (1980-07-01), Forster et al.

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