Title:
DILUTION PASSAGE ARRANGEMENT FOR GAS TURBINE ENGINE COMBUSTOR
Document Type and Number:
WIPO Patent Application WO/2015/147932
Kind Code:
A3
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.
Inventors:
EASTWOOD JONATHAN J (US)
MOURA DENNIS M (US)
BOULDIN LEE E (US)
PACHECO-TOUGAS MONICA (US)
MOURA DENNIS M (US)
BOULDIN LEE E (US)
PACHECO-TOUGAS MONICA (US)
Application Number:
PCT/US2014/071615
Publication Date:
November 26, 2015
Filing Date:
December 19, 2014
Export Citation:
Assignee:
UNITED TECHNOLOGIES CORP (US)
International Classes:
F23R3/02; F23M5/00; F23R3/04; F23R3/26
Foreign References:
| US20020116929A1 | 2002-08-29 | |||
| US4653279A | 1987-03-31 | |||
| US5687572A | 1997-11-18 | |||
| US20130255265A1 | 2013-10-03 | |||
| US4695247A | 1987-09-22 |
Other References:
See also references of EP 3084307A4
Attorney, Agent or Firm:
O'SHEA, Patrick J. (1500 Main Street Suite 91, Springfield Massachusetts, US)
Download PDF: