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:
Mar. 29, 2016

Filed:

May. 01, 2012
Applicants:

Jonathan Jeffery Eastwood, Newington, CT (US);

Kevin Joseph Low, Portland, CT (US);

Inventors:

Jonathan Jeffery Eastwood, Newington, CT (US);

Kevin Joseph Low, Portland, CT (US);

Assignee:

United Technologies Corporation, Hartford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/50 (2006.01); F23R 3/60 (2006.01); F02C 7/20 (2006.01); F23R 3/00 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F23R 3/50 (2013.01); F01D 25/24 (2013.01); F23R 3/002 (2013.01); F23R 3/60 (2013.01); F02C 7/20 (2013.01); F23R 2900/00005 (2013.01);
Abstract

A combustor assembly for a gas turbine engine includes a static structure and an annular combustor extending around a central axis and located radially inwards of the static structure. The annular combustor includes an annular outer shell and an annular inner shell that define an annular combustion chamber there between. The annular combustor is free of any rigid attachments directly between the static structure and the annular outer shell. The annular outer shell includes a radially-outwardly extending flange. A stop member is rigidly connected with the static structure and is located adjacent the radially-outwardly extending flange such that axial-forward movement of the annular combustor is limited.


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