FIELD: process engineering.
SUBSTANCE: invention relates to production of metal reinforcing part (30) of turbomachine leading or trailing edge (10). Proposed process comprises fabrication of several elements (30a, 30b, 30s, 30d) with V-like cross-section. Said elements form different sectors of reinforcing part (30) distributed between its root (32) and top (34). Said sectors are places on appliance (40) that reproduces the shape of said edge. Said sectors are connected to make a complete profile of reinforcing part (30) with recombination of different sectors. To make said reinforcing part (30), appliance (40) is used composed of interconnected detachable sectors that make the surface reproducing the shape of leading of trailing edge of turbomachine blade.
EFFECT: perfected method.
13 cl, 6 dwg
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