FIELD: process engineering.
SUBSTANCE: invention maybe used for production of composite-shape laminar articles and 3D articles from polymer composite materials, primarily, for Hi-Tech equipment in aircraft engineering and engine production. Two mould-halves of the device feature working surfaces of complicated, mainly, aerodynamically shaped inner space that repeats finished article outer shape. Working surfaces of said mould-halves are provided with recesses to receive layer to be fitted therein. Each said recess is located at preselected point and features shape and height identical to those of layer inserted therein and comprising, at least, one precut monolayer. Working surfaces of said mould-halves are provided with marks for reinforcing guides for monolayer material and through holes for multilayer blank laid therein.
EFFECT: precise arrangement of layer in monolayer blank.
2 cl, 2 dwg
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Authors
Dates
2011-05-27—Published
2009-10-13—Filed