Lubricating system for gas turbine engines

Lubrication – Systems – Gas turbine

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60 3908, 184 62, 184 622, 184 623, 184 628, F16N 2902, F01M 1112

Patent

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045110166

ABSTRACT:
Components, such as bearings, of gas turbine engines especially for aircraft are lubricated by a lubricant supply system including a main lubricant circulating circuit and an auxiliary lubricant circulating circuit for assuring a sufficient lubricant supply to the lubricating chamber or chambers under all operating conditions including those causing extremely rapid and locally differing displacements of the lubricant fluid in its supply tank. The main lubricant circulating circuit with its pumps, lubricating chamber or chambers, cooler, air separator and accumulator is operatively connected to the component being lubricated and is effective during normal and critical flight conditions. The auxiliary circulatory circuit with its lubricant supply tank and its pump is operatively connected to the main circulatory circuit for supplying lubricant into the main circuit. The auxiliary circulatory circuit is effective during the engine start-up and for replenishing lubricant into the main circuit during normal flight conditions.

REFERENCES:
patent: 1997700 (1935-04-01), Short
patent: 2239098 (1941-04-01), Hunter
patent: 2613498 (1952-10-01), Prendergast
patent: 3451214 (1969-06-01), Bradley
patent: 3554322 (1971-01-01), Deutschmann et al.
patent: 3626693 (1971-12-01), Guillot
patent: 3779345 (1973-12-01), Barnes et al.
patent: 4012012 (1977-03-01), Ligler
patent: 4030566 (1977-06-01), Cobb et al.
patent: 4105093 (1978-08-01), Dickinson
patent: 4153141 (1979-05-01), Methlie
patent: 4171611 (1979-10-01), Hueller
patent: 4197870 (1980-04-01), Hildebrandt et al.
patent: 4373421 (1983-02-01), Camboulives et al.
patent: 4390082 (1983-06-01), Swearingen
A publication entitled "Lubrication", published by the Texas Company (Texaco), vol. XL, Apr. 1954.

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