Lubrication cooling system for aircraft engine accessory

Power plants – Combustion products used as motive fluid – With lubricators

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60226R, 184 611, F02C 706

Patent

active

041517105

ABSTRACT:
This invention serves to cool the lubricant used by a mechanical constant speed drive (CSD) driving an aircraft alternator which aircraft is powered by a turbofan engine. The system cooling capacity is supplemented by an existing engine fuel/oil heat exchanger thereby effectuating a reduction in size of the CSD fan air/oil heat exchanger and minimizing an aircraft engine performance penalty.

REFERENCES:
patent: 2865580 (1958-12-01), Marshall
patent: 3797561 (1974-03-01), Clark et al.
Garrett Corp., TFE 731 Turbofan Pamphlet (1974).
Pratt & Whitney, "The Aircraft Gas Turbine Engine and Its Operation" (1974) p. 126.

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