Gas turbine blade and method for producing a blade
作者： Martin Schnieder , Jörg Krückels
DOI:
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摘要: A blade (10) for a gas turbine has airfoil (11), the wall (18) of which encloses an interior space (17). For cooling (18), includes arrangement (19) radial passage (20) extending in longitudinal direction and from multiplicity passages (21, 22), branch transverse direction, film-cooling holes (23) are led to outside direction. Particularly efficient is made possible by distribution along being selected independently 22) (20).
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