公开(公告)号：US20170037813A1

公开(公告)日：2017-02-09

申请号：US14818596

申请日：2015-08-05

Applicant: General Electric Company

Inventor： Mustafa DINDAR ,  Scott Andrew BURTON ,  Keith Edward James BLODGETT ,  Richard David CEDAR

IPC: F02K1/78 ,  F02K3/06 ,  F01D25/24 ,  F02C3/04

CPC classification number: F02K1/78 ,  F01D25/24 ,  F01D25/30 ,  F02K1/00 ,  F02K1/06 ,  F02K1/08 ,  F02K1/09 ,  F02K3/06 ,  F05D2250/14

Abstract: A turbofan exhaust nozzle includes: a conical inner shell disposed coaxially inside a surrounding outer shell to define an annular flow duct therebetween terminating in an outlet at a trailing edge of the outer shell and the inner shell terminates in a trailing edge aft of the outlet; and a pylon interrupting circumferentially the duct, wherein at least a portion of the trailing edge of the outer shell is vertically non-coplanar.

Abstract translation: 涡轮风扇排气喷嘴包括：圆锥形内壳，同轴地设置在周围的外壳内，以限定其间的环形流动管道，其终止于外壳的后缘处的出口，并且内壳终止于出口后部的后缘; 以及托架，其周向地中断所述管道，其中所述外壳的后缘的至少一部分是垂直非共面的。