- Patent Title: Multi-streamed dilution hole configuration for a gas turbine engine
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Application No.: US15105367Application Date: 2014-12-23
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Publication No.: US10386070B2Publication Date: 2019-08-20
- Inventor: Jonathan P. Sandoval , Randolph Smith
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: O'Shea Getz P.C.
- International Application: PCT/US2014/072200 WO 20141223
- International Announcement: WO2015/100346 WO 20150702
- Main IPC: F02C1/00
- 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.
Public/Granted literature
- US20160327272A1 MULTI-STREAMED DILUTION HOLE CONFIGURATION FOR A GAS TURBINE ENGINE Public/Granted day:2016-11-10
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