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United States of America Patent
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Issued Date -
Jul 11, 2024
app pub date -
Jan 7, 2023
filing date -
Jan 7, 2023
priority date (Note) -
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Abstract
A fluid system for an aircraft engine can include a pumped fluid circulation circuit including a fluid tank, the fluid circulation circuit configured to circulate a fluid through at least a part of the aircraft engine and means, in the fluid circulation circuit, for selectively directing the fluid of the fluid circulation circuit as a function of a pressure of fluid in the fluid circulation circuit to one of: a part of the aircraft engine, and a fluid bypass in the fluid circulation circuit that is fluidly upstream of the part.
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