公开(公告)号：US20150377029A1

公开(公告)日：2015-12-31

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

IPC: F01D5/14 ,  F01D9/06 ,  F01D5/18

CPC classification number: F01D5/141 ,  F01D5/18 ,  F01D5/181 ,  F01D5/187 ,  F01D9/065 ,  F01D25/08 ,  F05D2240/11 ,  F05D2240/127 ,  F05D2250/71 ,  F05D2260/2212 ,  F05D2260/22141

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.

Abstract translation: 根据本公开的示例性方面的用于燃气涡轮发动机的部件尤其包括形成至少一个空腔的外周的一部分的壁和从所述壁延伸的至少一个弯曲的湍流器。