Invention Grant
- Patent Title: Dilution passage arrangement for gas turbine engine combustor
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Application No.: US15105427Application Date: 2014-12-19
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Publication No.: US10655856B2Publication Date: 2020-05-19
- Inventor: Jonathan J. Eastwood , Dennis M. Moura , Lee E. Bouldin , Monica Pacheco-Tougas
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Getz Balich LLC
- International Application: PCT/US2014/071615 WO 20141219
- International Announcement: WO2015/147932 WO 20151001
- Main IPC: F23R3/06
- IPC: F23R3/06 ; F23R3/00 ; F23R3/60
Abstract:
A liner panel is provided for use in a combustor of a gas turbine engine. The liner panel includes a major dilution passage having a lip and a first seal boss. The liner panel also includes a minor dilution passage having a second seal boss adjacent the first seal boss.
Public/Granted literature
- US20160334103A1 DILUTION PASSAGE ARRANGEMENT FOR GAS TURBINE ENGINE COMBUSTOR Public/Granted day:2016-11-17
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