ATTACHMENT PYLON FOR AN UNDUCTED FAN
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United States of America Patent
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Issued Date -
Dec 25, 2014
app pub date -
Dec 12, 2012
filing date -
Dec 12, 2011
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
A pylon configured to secure a turbine engine to a structural element of an aircraft, the pylon including a streamlined profile defined by two opposite faces and extending longitudinally between a leading edge and a trailing edge, and at least a first one of the two faces presenting at least locally a succession of non-through hollows and of bumps.
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