FIELD: machine building.
SUBSTANCE: invention relates to turbine machines and can be used during production of metal part, intended for turbomachine blade reinforcement on its front and rear edges. Method involves stage, on which, at least, one winding metal strip (102, 102') from thin metal foil with recesses, is positioned on forming equipment. Strip has possibility of manual deformation in cold state in space in three directions (X, Y, Z). At next stage performing isostatic pressing of, at least, one metal winding strip (102, 102') in equipment. At that, metal strip (102, 102') sintering takes place with production of metal part.
EFFECT: result is manufacturing process simplification due to fewer operations and avoiding use of complex equipment.
9 cl, 7 dwg
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|---|---|---|---|
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