FIELD: aviation.
SUBSTANCE: invention relates to aviation and concerns the development and manufacture of elements of a gas turbine engine of an aircraft. During manufacturing of sections of the carrier lattice of the thrust reverser of the aircraft from polymeric composite materials into the longitudinal and transverse grooves of the mandrel by a continuous tow of unidirectional carbon filaments impregnated with a polymeric binder, the crossing longitudinal and transverse layers of the fins and blades of the grating section are wound. Moreover, they are wound under a certain tension set beforehand on the crescent. In this case winding, clinging a tourniquet at the angles and axes of the ribs and blades installed at a certain angle to the base, when the winding direction is changed.
EFFECT: it is possible to increase processability of laying fibers in curved grooves of variable thickness.
1 cl, 8 dwg
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