Title:
QUENCH APERTURE BODY FOR A TURBINE ENGINE COMBUSTOR
Document Type and Number:
WIPO Patent Application WO/2015/116269
Kind Code:
A3
Abstract:
An assembly for a turbine engine includes a combustor wall. The combustor wall includes a shell, a heat shield and an annular land. The heat shield is attached to the shell. The land extends vertically between the shell and the heat shield. The land extends laterally between a land outer surface and an inner surface, which at least partially defines a quench aperture in the combustor wall. A lateral distance between the land outer surface and the inner surface varies around the quench aperture.
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Inventors:
MOURA DENNIS M (US)
EASTWOOD JONATHAN J (US)
BOULDIN LEE E (US)
PACHECO-TOUGAS MONICA (US)
EASTWOOD JONATHAN J (US)
BOULDIN LEE E (US)
PACHECO-TOUGAS MONICA (US)
Application Number:
PCT/US2014/063440
Publication Date:
October 08, 2015
Filing Date:
October 31, 2014
Export Citation:
Assignee:
UNITED TECHNOLOGIES CORP (US)
International Classes:
F23M5/00; F23M5/08; F23R3/42
Foreign References:
US20130025293A1 | 2013-01-31 | |||
US20130298564A1 | 2013-11-14 | |||
US4653279A | 1987-03-31 | |||
US20030213250A1 | 2003-11-20 | |||
US20020184893A1 | 2002-12-12 |
Other References:
See also references of EP 3066387A4
Attorney, Agent or Firm:
BALICH, Garrett W. (1500 Main Street Suite 91, Springfield Massachusetts, US)
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