TURBINE ENGINE COMPRISING IMPROVED HARNESS SUPPORT MEANS
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United States of America Patent
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Issued Date -
Nov 16, 2023
app pub date -
Sep 28, 2021
filing date -
Sep 28, 2021
priority date (Note) -
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Abstract
An aircraft turbine engine with a main axis includes: an arm that is radial with respect to the main axis, extending through an air flow duct; a support wall belonging to the radial arm and which has two openings; a plurality of electric harnesses extending partially through the radial arm and for which a section of each harness is secured to the support wall of the arm; and two mounting blocks, in which each mounting block is associated with a group of sections of harness.
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