ROTOR BLADE FOR A COMPRESSOR OF A TURBOMACHINE, COMPRESSOR, AND TURBOMACHINE
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United States of America Patent
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Issued Date -
Aug 14, 2014
app pub date -
Jun 1, 2012
filing date -
Jun 1, 2011
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Abstract
A rotor blade for a compressor of a turbomachine is disclosed, the rotor blade having an airfoil having a leading edge, a trailing edge, an airfoil tip, as well as a pressure side and a suction side extending therebetween, provision being made for a profile variation on the pressure side, the profile variation extending into the trailing edge and into the airfoil tip. Also disclosed are a compressor and a turbomachine.
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