Cooling arrangement for jet engines

Power plants – Reaction motor – Including heat exchange means

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60728, 60736, F02K 1100

Patent

active

052728706

ABSTRACT:
A cooling arrangement for the cooling air of hypersonic jet engines comprises a heat exchanger in which the temperature of the cooling air is reduced by means of the fuel to be burnt in the engine. In order to keep the operating temperatures of the heat exchanger within controllable limits, a partial flow of the cooling air is branched off downstream of the heat exchanger and is admixed to the cooling air upstream of the heat exchanger for reducing the temperature.

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patent: 4041697 (1977-08-01), Coffinberry et al.
patent: 4696156 (1987-09-01), Burr et al.
patent: 5088280 (1992-02-01), Scott-Scott et al.
patent: 5152146 (1992-10-01), Butler

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