Air-oil separation system for gas turbine engine
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United States of America
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app pub date -
Mar 4, 2019
filing date -
Mar 4, 2019
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Abstract
An air-oil separation system for a gas turbine engine system comprises a housing that extends circumferentially around an axis to define an interior chamber of the housing and a separation unit located in the chamber. The housing is formed to include an inlet configured to receive a mixture of air and oil, an oil outlet configured to conduct oil to exit the housing, and an air outlet configured to conduct air to exit the housing. The air-oil separation unit separates air from the oil.
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