Title:
GAS TURBINE ENGINE QUENCH JET PATTERN FOR GAS TURBINE ENGINE COMBUSTOR
Document Type and Number:
WIPO Patent Application WO/2015/102736
Kind Code:
A3
Abstract:
A combustor for a turbine engine includes an inner liner panel with a multiple of inner dilution passages. The multiple of dilution passages includes a repeating pattern of a first major inner air passage, a minor inner air passage, and a second major inner air passage. A combustor for a turbine engine includes an outer liner panel with a multiple of outer dilution passages. The multiple of outer dilution passages includes a repeating pattern of a first major outer air passage, a first minor outer air passage, a second major outer air passage, and a second minor outer air passage.
Inventors:
MOURA DENNIS M (US)
REZVANI REZA (US)
REZVANI REZA (US)
Application Number:
PCT/US2014/061371
Publication Date:
September 11, 2015
Filing Date:
October 20, 2014
Export Citation:
Assignee:
UNITED TECHNOLOGIES CORP (US)
International Classes:
F23R3/42; F02C3/14; F23M5/00
Foreign References:
| US20090308077A1 | 2009-12-17 | |||
| US20130025293A1 | 2013-01-31 | |||
| US6606861B2 | 2003-08-19 | |||
| US20110126543A1 | 2011-06-02 | |||
| US20060130486A1 | 2006-06-22 |
Other References:
See also references of EP 3060852A4
Attorney, Agent or Firm:
O'SHEA, Patrick J. et al. (1500 Main Street Suite 91, Springfield MA, US)
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