Pylon for attaching an aircraft turbine engine comprising aligned front wing ties
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United States of America Patent
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Aug 26, 2014
Grant Date -
Mar 8, 2012
app pub date -
Aug 9, 2011
filing date -
Sep 3, 2010
priority date (Note) -
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status (Latency Note)
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Abstract
A pylon for attaching a turbine engine of an aircraft having a rigid structure including protruding fittings each having a first orifice and a plurality of ties to attach the pylon onto a wing of the aircraft, the plurality of ties comprising two side front ties to take the thrust forces, the two side front being secured to the first orifices of the protruding fittings to attach the rigid structure firmly to the wing. The plurality of ties further comprises a center front tie positioned between the two side front ties, the center front tie including a ball joint to take forces in a lateral direction of the rigid structure.
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