Oil cooler for fan jet engines

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

60 3908, 165168, F02K 304

Patent

active

049149040

ABSTRACT:
A turbo fan gas turbine engine is disclosed which includes a central engine and a shroud-enclosed fan, the shroud being supported by a plurality of structural struts extending from the central engine to the shroud. A plurality of tubes internal to each strut are provided with fins to increase their effective internal surface areas. Means are provided for connecting the tubes to a source of heated hydrocarbon liquid and for providing a return from the tubes to the source of hydrocarbon liquid, whereby the tubes provide cooling for the liquid. In a preferred embodiment of the invention, the tubes are surrounded by a highly conductive cement to provide support and improved heat transfer between the tubes and the struts.

REFERENCES:
patent: 3792586 (1974-02-01), Kasmarik et al.
patent: 3830058 (1974-08-01), Ainsworth
patent: 4645415 (1987-02-01), Hovan et al.
patent: 4674295 (1987-06-01), Curtis, Sr.
patent: 4771825 (1988-09-01), Chen et al.
patent: 4782658 (1988-11-01), Perry
patent: 4796430 (1989-01-01), Malaker et al.

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