FIELD: machine building.
SUBSTANCE: oil filter is installed inside the housing of oil tank, the housing of the filter being rigidly fixed by the butt bases on the two opposite sidewalls of oil tank. The internal cavities of the oil filter and oil tank are insulated from each other.
EFFECT: implementation of the invention will improve reliability of the oil tank and lubrication system of aircraft gas turbine engine as a whole.
1 dwg
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