FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to deoiler. Deoiler comprises tube 46, first bearing 16 and second bearing 18 arranged in oil chamber 20 wherein oil mist is sustained by rotation of bearings. Said deoiler 30 is fitted in one of oil chamber walls. Deoiler spins oil in suspension in air to allow airflow wherefrom oil is removed to pass inside tube. Tube 46 comprises protective cap 48 furnished with one or several outlet holes 50 at its top part for air removal and oil drain opening 52 at its bottom.
EFFECT: reduced oil consumption nacelle fouling.
6 cl, 5 dwg
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Authors
Dates
2013-05-27—Published
2009-01-28—Filed