FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to production of acoustic panel for aircraft intake edge and to air intake edge with such panel and to gas turbine nacelle. Method of making acoustic panel 12 for edge 2 at nacelle air intake 1 comprises production of deicing assy 14 including gauze of conducting elements made by photolithography. Note here that said deicing assy 14 is secured to structure 13 with cellular core.
EFFECT: simplified production.
15 cl, 12 dwg
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