IMPINGEMENT COOLING MECHANISM, TURBINE BLADE, AND COMBUSTOR
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United States of America Patent
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May 5, 2014
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Nov 8, 2011
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Abstract
It has a flat impingement hole (2) of which the opening width (D1) in the flow direction of a crossflow (F) in the gap between a cooling target (10) and an opposing member (20) is set greater than the opening width (D2) in a direction orthogonal with the flow direction of the crossflow F. Accordingly, the cooling efficiency is further improved by the impingement cooling mechanism.
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