The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Apr. 02, 2019
Filed:
Aug. 01, 2017
Applicant:
United Technologies Corporation, Farmington, CT (US);
Inventors:
Thomas N. Slavens, Norman, OK (US);
Mark F. Zelesky, Bolton, CT (US);
Andrew D. Burdick, Somers, CT (US);
Assignee:
United Technologies Corporation, Farmington, CT (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/04 (2006.01); F02C 7/18 (2006.01); F23R 3/00 (2006.01); F23R 3/60 (2006.01); F02C 3/06 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F23R 3/04 (2013.01); F02C 7/18 (2013.01); F23R 3/002 (2013.01); F23R 3/60 (2013.01); F02C 3/06 (2013.01); F02K 3/06 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2250/141 (2013.01); F05D 2250/323 (2013.01); F05D 2260/202 (2013.01); F05D 2260/22141 (2013.01); F23R 2900/03042 (2013.01);
Abstract
A liner panel for use in a combustor of a gas turbine engine, including a multiple of heat transfer ribs located in at least one discrete area of the liner panel. A wall assembly within a gas turbine engine including a support shell, a liner panel mounted to the support shell via a multiple of studs and a multiple of heat transfer ribs located in at least one discrete area on a cold side of the liner panel, each of the multiple of heat transfer ribs account for the multiple of studs.