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公开(公告)号：US10316668B2
公开(公告)日：2019-06-11
申请号：US14765390
申请日：2014-01-31
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Mosheshe Camara-Khary Blake , Lisa K. Osborne , Thomas N. Slavens
Abstract: A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a wall that forms a portion of an outer periphery of at least one cavity and at least one curved turbulator that extends from said wall.
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