Heat exchanger system for an aircraft turbomachine
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United States of America Patent
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Jun 9, 2020
Grant Date -
Dec 22, 2016
app pub date -
Feb 10, 2015
filing date -
Feb 11, 2014
priority date (Note) -
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Abstract
A heat exchange system in a turbomachine that comprises a plurality of members and equipment to be cooled and/or lubricated, the heat exchange system includes a fluid circuit for cooling and/or lubricating the equipment, the heat exchange system being configured to bring the fluid circuit in thermal contact with a fluid, wherein the heat exchange system further includes an open work structure which is in thermal contact with at least one hot section of the fluid circuit and through which the fluid passes.
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