LUBRICANT RESERVOIR WITH INTEGRATED HEAT EXCHANGER
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United States of America Patent
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N/A
Issued Date -
May 16, 2024
app pub date -
Nov 14, 2022
filing date -
Nov 14, 2022
priority date (Note) -
Published
status (Latency Note)
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Abstract
An apparatus is provided for a gas turbine engine. This engine apparatus includes a lubricant reservoir, a lubricant circuit and a compressed air circuit. The lubricant reservoir includes an internal cavity, a compressed air passage and a reservoir wall at least partially forming an outer peripheral boundary of the internal cavity. The internal cavity is configured to contain lubricant. The compressed air passage extends within the reservoir wall along at least a portion of the outer peripheral boundary of the internal cavity. The lubricant circuit is fluidly coupled with the internal cavity. The compressed air circuit is fluidly coupled with the compressed air passage.
First Claim
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