FLOW MIXER DUCT FOR A BLEED SYSTEM
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United States of America Patent
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Issued Date -
Nov 19, 2020
app pub date -
Mar 26, 2020
filing date -
Apr 3, 2019
priority date (Note) -
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Abstract
A duct for a bleed system of an aircraft, wherein the duct extends from an inlet section to an outlet section along a longitudinal axis, and wherein the duct comprises a continuous piece arranged on and protruding from the internal wall of the duct. The duct is subject to temperature gradients in order to reduce the temperature of the warmest airflow closer to the inner wall rather than rapidly mix the airflow.
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