US Patent 11619456 Flow mixer duct for a bleed system
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Patent Inventor Names
Brice Lenoir0
Edits on 8 Apr, 2023
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US Patent 11619456 Flow mixer duct for a bleed system
Article
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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Patent Number
116194560
Date of Patent
April 4, 2023
0Patent Application Number
168304250
Date Filed
March 26, 2020
0Patent Primary Examiner
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