FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft nacelle deicing element. Proposed method comprises the following stages: (a) matrix of heating resistors is produced in substrate by photolithography; (b) composite sheet 50, 52 is placed on matrix produced at step (a); (c)inner shell 12 is applied on thus made deicing assy 13.
EFFECT: simplified fabrication.
19 cl, 8 dwg
