US2017197271A1PendingUtilityA1

Repair material preform

Assignee: UNITED TECHNOLOGIES CORPPriority: May 9, 2014Filed: Mar 29, 2017Published: Jul 13, 2017
Est. expiryMay 9, 2034(~7.8 yrs left)· nominal 20-yr term from priority
B23K 35/3046B23K 35/3033B23K 35/0244B23K 1/0018B23K 2201/001F01D 11/08B23P 6/005C22C 19/03C22C 19/07F05D 2240/11F01D 5/005F05D 2230/80B23K 31/02B23P 6/002B23K 2101/001F01D 11/122F05D 2300/177
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Claims

Abstract

A structural element and method for repairing a damaged portion of a metal component utilizes a preform configured to engage with the metal component and receive a repair material. The preform may be made of a material having a first melting point, and the repair material may be made of a material having a second melting point that is lower than the first melting point. The preform may be a mold configured to reconstruct the shape of the damaged portion of the metal component. The repair material may include a first material and an additive material, such as boron. The repair material may have a melting point that is approximately 40 degrees Fahrenheit lower than the melting point of the metal component.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
         1 . A structural element for repairing a metal component comprising:
 a preform configured to receive repair material and repair a damaged portion of the metal component, wherein the metal component melts at a first temperature and the repair material melts at a second temperature that is lower than the first temperature, and wherein the preform has at least one of a preform wear resistance and a preform oxidation resistance that is greater than at least one of a repair material wear resistance and a repair material oxidation resistance of the repair material.   
     
     
         2 . The structural element of  claim 1 , wherein the repair material comprises an additive material. 
     
     
         3 . The structural element of  claim 1 , wherein the preform comprises a mold configured to reconstruct a shape of the damaged portion of the metal component. 
     
     
         4 . The structural element of  claim 1 , wherein the preform comprises an alloy including cobalt or nickel. 
     
     
         5 . The structural element of  claim 2 , wherein the repair material comprises a cobalt- or nickel-boron composition. 
     
     
         6 . The structural element of  claim 1 , wherein the repair material has a melting point that is approximately 40 degrees Fahrenheit lower than a melting point of the metal component.

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