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:
May. 25, 2021

Filed:

May. 07, 2018
Applicants:

Rolls-royce North American Technologies Inc., Indianapolis, IN (US);

Rolls-royce Corporation, Indianapolis, IN (US);

Inventors:

Jack D. Petty, Sr., Indianapolis, IN (US);

John D. Holdcraft, Carmel, IN (US);

Kevin M. Sauer, Plainfield, IN (US);

Duane A. Smith, Carmel, IN (US);

Assignees:

Rolls-Royce North American Technologies Inc., Indianapolis, IN (US);

Rolls-Royce Corporation, Indianapolis, IN (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/60 (2006.01); F23R 3/50 (2006.01); F23R 3/00 (2006.01); F23R 3/06 (2006.01); F23M 5/04 (2006.01);
U.S. Cl.
CPC ...
F23R 3/60 (2013.01); F23M 5/04 (2013.01); F23R 3/002 (2013.01); F23R 3/06 (2013.01); F23R 3/50 (2013.01); F23R 2900/00017 (2013.01); F23R 2900/00018 (2013.01); F23R 2900/03043 (2013.01);
Abstract

A combustor liner assembly is provided including an inlet wall, an inner wall, an outer wall, and a plurality of fasteners. The inlet wall has an opening into a combustion chamber. The inner wall is coupled to the inlet wall at a first end of the combustor liner. The inner wall defines a radially inner end of the combustion chamber. The outer wall includes a plurality of segments. The plurality of segments define a radially outer end of the combustion chamber. A first portion of the plurality of fasteners couples each of the plurality of segments to another of the plurality of segments. A second portion of the plurality of fasteners couples at least one of the plurality of segments to the inlet wall at the first end of the combustor liner.


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