Pylon with noise attenuating fairing
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United States of America Patent
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Aug 8, 2017
Issued Date -
N/A
app pub date -
Jun 22, 2015
filing date -
Jun 22, 2015
priority date (Note) -
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Abstract
A pylon is provided for connecting a propulsion system to an aircraft. The pylon includes a structure configured to structurally tie the propulsion system to the aircraft. The pylon also includes a pylon fairing configured to house and provide an aerodynamic cover for the structure. A lower aft fairing segment of the pylon fairing includes a plurality of apertures. The apertures are fluidly coupled with a sealed, sound attenuating chamber within the pylon.
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