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:
May. 21, 2019

Filed:

Mar. 11, 2015
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Joseph Parkos, Jr., East Haddam, CT (US);

James O. Hansen, Glastonbury, CT (US);

Christopher J. Hertel, Wethersfield, CT (US);

Andrew J. Murphy, Old Saybrook, CT (US);

Ashley P. Phillips, Rocky Hill, CT (US);

Jay Thomas Abraham, Stamford, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); C25D 1/00 (2006.01); C25D 1/02 (2006.01); F04D 29/32 (2006.01);
U.S. Cl.
CPC ...
C25D 1/00 (2013.01); C25D 1/02 (2013.01); F01D 5/147 (2013.01); F04D 29/324 (2013.01); F05D 2230/30 (2013.01); F05D 2230/90 (2013.01); F05D 2240/303 (2013.01); F05D 2300/603 (2013.01);
Abstract

An electroformed sheath for protecting an airfoil includes a sheath body and a mandrel insert is provided. The sheath body includes a leading edge. The sheath body includes a pressure side wall and an opposed suction side wall, which side walls meet at the leading edge and extend away from the leading edge to define a cavity between the side walls. The sheath body includes a head section between the leading edge and the cavity. The mandrel insert is positioned between the pressure side and suction side walls, and includes a generally wedge-shaped geometry. A method for protecting an airfoil includes: 1) securing a mandrel insert to a mandrel; 2) electroplating a sheath body onto the mandrel and the mandrel insert; 3) removing the mandrel from the sheath body so that a sheath cavity is defined within the sheath body; and 4) securing the airfoil within the sheath cavity.


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