公开(公告)号：US10386070B2

公开(公告)日：2019-08-20

申请号：US15105367

申请日：2014-12-23

Applicant: United Technologies Corporation

Inventor： Jonathan P. Sandoval ,  Randolph Smith

IPC: F02C1/00 ,  F23R3/06 ,  F23R3/00 ,  F23R3/50

Abstract: A combustor component defining a dilution hole configuration for a combustor wall assembly of a gas turbine engine has first and second dilution holes that communicate radially with one-another and with respect to respective centerlines of each dilution hole. In operation, each dilution hole forms a respective jet stream along respective centerlines for flowing cooling air into a combustion chamber.

公开(公告)号：US20160327272A1

公开(公告)日：2016-11-10

申请号：US15105367

申请日：2014-12-23

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Jonathan P. Sandoval ,  Randolph Smith

IPC: F23R3/06 ,  F23R3/50 ,  F23R3/00

CPC classification number: F23R3/06 ,  F23R3/002 ,  F23R3/50 ,  F23R2900/03041 ,  Y02T50/675

Abstract: A combustor component defining a dilution hole configuration for a combustor wall assembly of a gas turbine engine has first and second dilution holes that communicate radially with one-another and with respect to respective centerlines of each dilution hole. In operation, each dilution hole forms a respective jet stream along respective centerlines for flowing cooling air into a combustion chamber.

Abstract translation: 限定用于燃气涡轮发动机的燃烧器壁组件的稀释孔构造的燃烧器部件具有第一和第二稀释孔，其相对于每个稀释孔的相应中心线径向连通。 在操作中，每个稀释孔沿着相应的中心线形成相应的喷射流，用于将冷却空气流入燃烧室。