Blade, integrally bladed rotor base body and turbomachine
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United States of America Patent
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Aug 22, 2017
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N/A
app pub date -
May 1, 2012
filing date -
May 2, 2011
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Abstract
A blade for a turbomachine is disclosed. At least one cooling channel is configured in the blade neck, whose inlet is disposed near a platform projection on the high-pressure side and whose outlet is disposed in the region of a platform projection on the low-pressure side. An integrally bladed rotor base body having a plurality of these types of blades as well as turbomachine with such a rotor base body is also disclosed.
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