Title:
GAS TURBINE ENGINE COMBUSTOR LINER ASSEMBLY WITH CONVERGENT HYPERBOLIC PROFILE
Document Type and Number:
WIPO Patent Application WO/2014/189556
Kind Code:
A3
Abstract:
A heat shield for a combustor of a gas turbine engine includes a first edge with a first set of cantilevered members and a second edge with a second set of cantilevered members.
Inventors:
CUNHA FRANK J (US)
ERBAS-SEN NURHAK (US)
ERBAS-SEN NURHAK (US)
Application Number:
PCT/US2014/014819
Publication Date:
January 29, 2015
Filing Date:
February 05, 2014
Export Citation:
Assignee:
UNITED TECHNOLOGIES CORP (US)
International Classes:
F23M5/04; F02C7/12; F23M5/08; F23R3/42
Foreign References:
| US4843825A | 1989-07-04 | |||
| US7886540B2 | 2011-02-15 | |||
| US20030213250A1 | 2003-11-20 | |||
| US20100223931A1 | 2010-09-09 | |||
| US5079915A | 1992-01-14 |
Other References:
See also references of EP 2954261A4
Attorney, Agent or Firm:
O'SHEA, Patrick (1500 Main Street Suite 91, Springfield MA, US)
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