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.

Date of Patent:
Jun. 23, 2020

Filed:

Mar. 31, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Tracy A. Propheter-Hinckley, Manchester, CT (US);

Mark F. Zelesky, Bolton, CT (US);

Atul Kohli, Tolland, CT (US);

Dustin W. Davis, Marlborough, CT (US);

Ricardo Trindade, Mansfield, CT (US);

Steven Bruce Gautschi, Milton, MA (US);

Brandon W. Spangler, Vernon, CT (US);

Trevor Rudy, Morgantown, WV (US);

Benjamin Bellows, Glastonbury, CT (US);

Dave J. Hyland, Portland, CT (US);

James B. Hoke, Tolland, CT (US);

Stephen K. Kramer, Cromwell, CT (US);

Dennis M. Moura, South Windsor, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F23R 3/60 (2006.01); F23R 3/06 (2006.01); F16B 43/00 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F23R 3/06 (2013.01); F23R 3/60 (2013.01); F16B 43/00 (2013.01); F23R 2900/03044 (2013.01); Y02T 50/675 (2013.01);
Abstract

A combustor for a gas turbine engine includes a combustor shell having a shell opening therethrough, a combustor panel having a stud attached thereto, the stud extending through the shell opening. The stud includes a standoff to define an intermediate passage between the combustor shell and the combustor panel. A retainer is attached to the stud. A washer surrounds the stud and is positioned between the retainer and the combustor shell. The washer at least partially defines a cooling flow passage configured to direct a cooling airflow through the shell opening to impinge the cooling flow on at least one of the stud or the standoff.


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