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:
Nov. 28, 2017

Filed:

Oct. 29, 2013
Applicant:

Dresser-rand Company, Olean, NY (US);

Inventors:

Byron L. Mohr, Olean, NY (US);

David C. Seib, Olean, NY (US);

Assignee:

Dresser-Rand Company, Olean, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/30 (2006.01); B21K 25/00 (2006.01); B23K 20/02 (2006.01); B23K 20/08 (2006.01); F01D 25/16 (2006.01); F02K 9/34 (2006.01); F16L 58/10 (2006.01); F16L 41/02 (2006.01); F16L 41/08 (2006.01); B23K 101/04 (2006.01); B23K 103/04 (2006.01); B23K 103/08 (2006.01); B23K 103/14 (2006.01); B23K 103/18 (2006.01);
U.S. Cl.
CPC ...
F02C 7/30 (2013.01); B21K 25/00 (2013.01); B23K 20/02 (2013.01); B23K 20/085 (2013.01); F01D 25/16 (2013.01); F02K 9/34 (2013.01); F16L 41/026 (2013.01); F16L 41/084 (2013.01); F16L 58/1036 (2013.01); B23K 2201/04 (2013.01); B23K 2203/04 (2013.01); B23K 2203/08 (2013.01); B23K 2203/14 (2013.01); B23K 2203/18 (2013.01); F05B 2230/239 (2013.01); Y10T 29/4932 (2015.01); Y10T 29/49316 (2015.01); Y10T 29/49323 (2015.01); Y10T 29/49826 (2015.01); Y10T 29/49865 (2015.01); Y10T 29/49885 (2015.01);
Abstract

An apparatus and method for protecting an inner radial surface of a radial member of a turbomachine from corrosion are provided. The method may include shaping the inner radial surface of the radial member and a corresponding outer radial surface of a corrosion-resistant liner. The method may also include heating the radial member to increase a diameter of the inner radial surface of the radial member, and inserting at least a portion of the corrosion-resistant liner into the radial member. The method may further include attaching the corrosion-resistant liner to the inner radial surface of the radial member to thereby protect the inner radial surface of the radial member of the turbomachine from corrosion.


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