公开(公告)号：US20140374566A1

公开(公告)日：2014-12-25

申请号：US14364981

申请日：2012-12-12

Applicant: SNECMA

Inventor： Rasika Fernando ,  Nicolas Mehier ,  Fabien Monti ,  Nicolas Sirvin

IPC: B64D27/26

CPC classification number: B64D27/26 ,  B64C21/10 ,  B64C23/00 ,  B64C23/06 ,  B64C2230/04 ,  B64C2230/14 ,  B64C2230/26 ,  B64C2230/28 ,  B64D27/14 ,  B64D29/04 ,  B64D2027/005 ,  B64D2027/262 ,  Y02T50/162 ,  Y02T50/166 ,  Y02T50/66

Abstract: A pylon configured to secure a turbine engine to a structural element of an aircraft, the pylon including a streamlined profile defined by two opposite faces and extending longitudinally between a leading edge and a trailing edge, and at least a first one of the two faces presenting at least locally a succession of non-through hollows and of bumps.

Abstract translation: 一种构造成将涡轮发动机固定到飞行器的结构元件的吊架，所述托架包括由两个相对的面限定的并且在前缘和后缘之间纵向延伸的流线型轮廓，并且所述两个面中的至少第一个呈现 至少在本地一连串的非通孔和颠簸。