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:
Feb. 26, 2019

Filed:

Jul. 12, 2016
Applicant:

Siemens Energy, Inc., Orlando, FL (US);

Inventor:

Anthony L. Schiavo, Oviedo, FL (US);

Assignee:

SIEMENS ENERGY, INC., Orlando, FL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F23R 3/42 (2006.01); F23R 3/60 (2006.01); F23R 3/00 (2006.01);
U.S. Cl.
CPC ...
F01D 9/023 (2013.01); F23R 3/007 (2013.01); F23R 3/425 (2013.01); F23R 3/60 (2013.01); F05D 2240/40 (2013.01); F05D 2250/141 (2013.01); F23R 2900/00005 (2013.01);
Abstract

A ducting arrangement () for a combustion turbine engine is provided. The arrangement includes a ceramic liner () defining a hot gas path throughout a length of the ducting arrangement. A cooling sleeve () is disposed circumferentially outwardly onto the ceramic liner along the length. A metallic support frame () is disposed circumferentially outwardly onto the cooling sleeve along the length. The cooling sleeve may be structured with structural features along the length for biasing against the ceramic liner and the metallic support frame to resiliently accept mechanical and thermal growth induced loading that develops between the ceramic liner and the metallic support frame during operating conditions of the combustion turbine engine.


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