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. 13, 2018

Filed:

Jan. 02, 2015
Applicants:

Jose E. Ruberte Sanchez, Jupiter, FL (US);

Timothy J. Mcalice, Jupiter, FL (US);

Kevin L. Rugg, Fairfield, CT (US);

Inventors:

Jose E. Ruberte Sanchez, Jupiter, FL (US);

Timothy J. McAlice, Jupiter, FL (US);

Kevin L. Rugg, Fairfield, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F23M 5/04 (2006.01); F02K 1/82 (2006.01); F23R 3/60 (2006.01);
U.S. Cl.
CPC ...
F23M 5/04 (2013.01); F02K 1/82 (2013.01); F23R 3/002 (2013.01); F23R 3/007 (2013.01); F23R 3/60 (2013.01); F23R 2900/00017 (2013.01); Y10T 29/49231 (2015.01);
Abstract

A combined liner and panel for use in a gas turbine engine comprise a ceramic matrix composite panel having a plurality of extending members extending away from a face of ceramic matrix composite panel which will face hot products of combustion. A liner includes a plurality of spring members that apply a bias force biasing the extending members. The spring members bias the extending members on the panel in a direction away from the face of the panel which will face the hot products of combustion. A gas turbine engine, and a method of attaching a ceramic matrix composite panel to a liner are also disclosed.


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