FIELD: turbines or turbomachines.
SUBSTANCE: present invention relates to a method for manufacturing turbine assembly (10) comprising at least one profile unit (12) comprising at least substantially hollow profile (14) with at least one cooling channel (16) for cooling medium (18) and at least one input surface (20), wherein at least one cooling channel (16) enters at least one inlet surface (20), and additionally turbine assembly (10) comprises at least one cover plate (22), which at least partially covers at least one inlet surface (20). In order to provide reliable connection, the method includes stage of connection of at least one covering plate (22) with one continuous connection structure (24) to at least one profile unit (12).
EFFECT: invention is aimed at providing reliability of cooling channels seal.
12 cl, 6 dwg
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