公开(公告)号：US20150323182A1

公开(公告)日：2015-11-12

申请号：US14581568

申请日：2014-12-23

Applicant: United Technologies Corporation

Inventor： Jonathan P. Sandoval ,  Randolph J. Smith

IPC: F23R3/00 ,  F23R3/02

CPC classification number: F23R3/02 ,  F23R3/002 ,  F23R3/005 ,  F23R3/06 ,  F23R2900/03041 ,  F23R2900/03044 ,  Y02T50/675

Abstract: A conjoined grommet assembly for a combustor wall assembly of a gas turbine engine has a first grommet defining at least in-part a first dilution hole, and a second grommet defining at least in-part a second dilution hole. The first and second dilution holes are spaced closely together such that the first grommet is in contact with the second grommet.

Abstract translation: 用于燃气涡轮发动机的燃烧器壁组件的联合索环组件具有至少部分地限定第一稀释孔的第一索环和至少部分地限定第二稀释孔的第二索环。 第一和第二稀释孔紧密地间隔开，使得第一索环与第二索环接触。