A nacelle-to-pylon fairing (20) formed over at least a portion of an inter-region between a nacelle (16) and a pylon (18) of an aircraft may include a longitudinal axis, a lateral axis and a transverse axis, an upper end incorporated to the pylon at a fairing-to-pylon interface (72), and a lower end incorporated to the nacelle at a failing-to-nacelle interface (70), wherein the fairing (20) defines a surface between the upper end and the lower end.
NACELLE-TO-PYLON FAIRING
GONDEL-MAST-VERKLEIDUNG
CARÉNAGE NACELLE-MÂT
2015-11-11
Patent
Elektronische Ressource
Englisch
Improved aircraft pylon fairing, fairing assembly, aircraft pylon and aircraft
Europäisches Patentamt | 2024
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