<p>A turbine blade (10) having improved cooling has an airfoil (13) with a root end (16) and a tip end (18) and at least one cooling passageway (14) in the airfoil (13). Each cooling passageway (14) extends from the root end (16) to the tip end (18) and has a circular cross-section. A plurality of turbulation promotion devices (36) are arranged in each cooling passageway (14). Each of the turbulation promotion devices (36) is arcuate in shape and circumscribes an arc less than 180 degrees.</p>
申请公布号
EP1561902(B1)
申请公布日期
2013.05.01
申请号
EP20050250703
申请日期
2005.02.08
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
ABDEL-MESSEH, WILLIAM;PAGE, RICHARD;HERRERA, DANIEL;DUBE, BRYAN P.