US2015132495A1PendingUtilityA1

Machine component with a cavitation resistant coating

Assignee: CATERPILLAR INCPriority: Dec 19, 2011Filed: Jan 16, 2015Published: May 14, 2015
Est. expiryDec 19, 2031(~5.4 yrs left)· nominal 20-yr term from priority
F02F 1/004C23C 30/00Y10T428/12958C23C 4/04C22C 38/34Y10T428/26C22C 38/16C22C 38/24Y10T428/31678C23C 26/00C23C 2/04Y10T428/12972C22C 38/22C22C 38/36C22C 38/20C22C 38/12C23C 14/06Y10T428/12965B32B 15/011C22C 38/04C22C 38/02Y10T428/12979C22C 38/32C22C 38/002C23C 24/103C22C 33/0257C23C 30/005
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Claims

Abstract

A machine component may include a body made of an iron alloy. The body may include a surface, and a coating fused to the surface. The coating may be an alloy including phosphorous, carbon, and iron. The coating may have solidus temperature of less than or equal to about 1000° C., and a hardness greater than or equal to about 50 HRC.

Claims

exact text as granted — not AI-modified
1 - 10 . (canceled) 
     
     
         11 . A method of forming a cavitation-resistant coating on a surface of a machine component, comprising:
 preparing the surface of the component for coating;   applying a coating including phosphorous, carbon, and iron to the surface;   heating the surface to at least partially melt the applied coating at a temperature less than or equal to about 1000° C.; and   cooling the at least partially melted coating to fuse the coating to the surface, the fused coating having a hardness greater than or equal to about 50 HRC.   
     
     
         12 . The method of  claim 11 , wherein cooling the at least partially melted coating includes cooling the coating to ambient temperature at cooling rate of less than or equal to about 10° C./sec. 
     
     
         13 . The method of  claim 11 , wherein applying the coating includes applying a coating including about 4-12% by weight of phosphorous, and about 0.5-3.5% by weight of carbon to the surface. 
     
     
         14 . The method of  claim 13 , wherein the coating further includes copper between about 0.1-15% by weight. 
     
     
         15 . The method of  claim 13 , wherein the coating further includes at least one of boron less than or equal to 1% by weight, silicon less than or equal to about 3% by weight, manganese between about 0.1-5% by weight, nickel less than or equal to about 5% by weight, chromium between about 0.1-15% by weight, molybdenum less than or equal to about 11% by weight, and vanadium less than or equal to 6% by weight. 
     
     
         16 . The method of  claim 11 , wherein applying the coating includes applying a coating including about 7-9% by weight of phosphorous, and about 1.5-2.5% by weight of carbon. 
     
     
         17 - 20 . (canceled)

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