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:
Sep. 10, 2019

Filed:

Feb. 17, 2016
Applicant:

Siemens Aktiengesellschaft, München, DE;

Inventors:

Gary B. Merrill, Orlando, FL (US);

Jonathan E. Shipper, Jr., Lake Mary, FL (US);

Cora Hitchman, Charlotte, NC (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/12 (2006.01); F01D 5/18 (2006.01); F01D 5/28 (2006.01); F01D 5/14 (2006.01); B23K 26/382 (2014.01); B23H 1/00 (2006.01); B23P 15/02 (2006.01); B22C 7/02 (2006.01); B22C 9/24 (2006.01); B22D 25/02 (2006.01); B22D 29/00 (2006.01); C23C 4/02 (2006.01); C23C 4/18 (2006.01); C23C 28/00 (2006.01); F01D 11/08 (2006.01); F04D 29/52 (2006.01); F04D 29/68 (2006.01); C23C 4/073 (2016.01);
U.S. Cl.
CPC ...
F01D 11/122 (2013.01); B22C 7/02 (2013.01); B22C 9/24 (2013.01); B22D 25/02 (2013.01); B22D 29/001 (2013.01); B23H 1/00 (2013.01); B23K 26/382 (2015.10); B23P 15/02 (2013.01); C23C 4/02 (2013.01); C23C 4/073 (2016.01); C23C 4/18 (2013.01); C23C 28/3215 (2013.01); C23C 28/3455 (2013.01); F01D 5/14 (2013.01); F01D 5/18 (2013.01); F01D 5/186 (2013.01); F01D 5/28 (2013.01); F01D 5/288 (2013.01); F01D 11/08 (2013.01); F01D 11/127 (2013.01); F04D 29/526 (2013.01); F04D 29/685 (2013.01); F05D 2230/10 (2013.01); F05D 2230/30 (2013.01); F05D 2230/90 (2013.01); F05D 2250/12 (2013.01); F05D 2250/15 (2013.01); F05D 2250/182 (2013.01); F05D 2250/183 (2013.01); F05D 2250/184 (2013.01); F05D 2250/185 (2013.01); F05D 2250/23 (2013.01); F05D 2250/282 (2013.01); F05D 2250/292 (2013.01); F05D 2250/294 (2013.01); F05D 2250/75 (2013.01); F05D 2260/202 (2013.01); F05D 2260/22141 (2013.01); F05D 2300/175 (2013.01); F05D 2300/611 (2013.01);
Abstract

Delamination of thermal barrier coatings ('TBC's') () from superalloy substrates () of components () for turbine engines (), such as engine blades (), vanes (), or castings in transitions (), is inhibited during subsequent cooling passage () formation. Partially completed cooling passages (), which have skewed passage paths that end at a terminus (), which is laterally offset from the passage entrance (), are formed in the superalloy component () prior to application of the TBC layer(s) (). The skewed, laterally offset path of each partially completed cooling passage () establishes an overhanging shield layer () of superalloy material that protects the TBC layer () during completion of the cooling passage ().


Find Patent Forward Citations

Loading…