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. 16, 2010

Filed:

Jan. 20, 2006
Applicants:

David A. Litton, Rocky Hill, CT (US);

Kevin W. Schlichting, Storrs, CT (US);

Melvin Freling, West Hartford, CT (US);

John G. Smeggil, Simsbury, CT (US);

David B. Snow, Glastonbury, CT (US);

Michael J. Maloney, Marlborough, CT (US);

Inventors:

David A. Litton, Rocky Hill, CT (US);

Kevin W. Schlichting, Storrs, CT (US);

Melvin Freling, West Hartford, CT (US);

John G. Smeggil, Simsbury, CT (US);

David B. Snow, Glastonbury, CT (US);

Michael J. Maloney, Marlborough, CT (US);

Assignee:

United Technologies Corporation, Hartford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B32B 9/00 (2006.01);
U.S. Cl.
CPC ...
Abstract

A turbine engine component is provided which has a substrate and a thermal barrier coating applied over the substrate. The thermal barrier coating comprises at least one layer of a first material selected from the group consisting of a zirconate, a hafnate, a titanate, and mixtures thereof, which first material has been mixed with, and contains, from about 25 to 99 wt % of at least one oxide. The at least one oxide comprises at least one oxide of a material selected from the group consisting of lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, lutetium, scandium, indium, and yttrium. If desired, a metallic bond coat may be present between the substrate and the thermal barrier coating system. A method for forming the thermal barrier coating system of the present invention is described.


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