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:
Dec. 08, 2020

Filed:

Sep. 11, 2018
Applicant:

Honeywell International Inc., Morris Plains, NJ (US);

Inventors:

Don Mittendorf, Mesa, AZ (US);

Jason Smoke, Phoenix, AZ (US);

Brent Ludwig, Scottsdale, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Charlotte, NC (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B22F 5/04 (2006.01); F01D 5/20 (2006.01); B22F 3/15 (2006.01); B23P 15/04 (2006.01); B29C 43/10 (2006.01);
U.S. Cl.
CPC ...
B22F 5/04 (2013.01); B22F 3/15 (2013.01); B22F 3/156 (2013.01); B23P 15/04 (2013.01); F01D 5/20 (2013.01); B29C 2043/106 (2013.01); F05D 2230/23 (2013.01); F05D 2230/42 (2013.01);
Abstract

A method of producing an abrasive tip for a turbine blade includes producing or obtaining a metal powder that is mixed with an abrasive ceramic powder and producing or obtaining a metallic mold that is in the shape of an airfoil. The metallic mold includes a hollow interior portion. The method further includes sealing the metal and ceramic powder mixture within the hollow interior portion of the metallic mold under vacuum and subjecting the sealed mold to a hot isostatic pressing process. The hot isostatic pressing process compacts and binds the metal and ceramic powder mixture together into a solid article in the shape of the airfoil. Still further, the method includes slicing the solid article into a plurality of airfoil-shaped slices and bonding one slice of the plurality of airfoil-shaped slices to a tip portion of a turbine blade.


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