US2016273080A1PendingUtilityA1

Metal matrix composite

Assignee: MATERION CORPPriority: Mar 17, 2015Filed: Mar 17, 2016Published: Sep 22, 2016
Est. expiryMar 17, 2035(~8.6 yrs left)· nominal 20-yr term from priority
B22F 3/15B22F 2304/058C22C 21/16B22F 2999/00B22F 2302/105B22F 2301/052C22C 21/12C22C 21/06C22C 21/08B22F 2302/20B22F 2302/10B22F 2998/10C22C 1/051C22C 32/0047C22C 32/0063C22C 1/1084C22C 1/05C22C 32/0057C22C 32/0068C22C 32/0078C22C 32/0073C22C 1/0416C22C 32/0031C22C 49/06
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Claims

Abstract

A metal matrix composite material includes a reinforcement phase dispersed in an aluminum or aluminum alloy matrix. The reinforcement phase includes particles having an average particle size (D50) of from 0.1 μm to 0.5 μm.

Claims

exact text as granted — not AI-modified
1 . A metal matrix composite comprising:
 an aluminum or aluminum alloy matrix; and   reinforcement particles dispersed in the matrix, the reinforcement particles having an average particle size (D 50 ) of from 0.1 μm to 0.5 μm.   
     
     
         2 . The metal matrix composite of  claim 1 , wherein the reinforcement particles comprise at least one ceramic material selected from the group consisting of carbides, oxides, silicides, borides, and nitrides. 
     
     
         3 . The metal matrix composite of  claim 1 , wherein the reinforcement particles comprise at least one ceramic material selected from the group consisting of silicon carbide, titanium carbide, boron carbide, silicon nitride, titanium nitride, and zirconium oxide. 
     
     
         4 . The metal matrix composite of  claim 1 , wherein the aluminum alloy comprises at least one element selected from the group consisting of chromium, copper, lithium, magnesium, manganese, zinc, iron, nickel, silver, scandium, vanadium and silicon. 
     
     
         5 . The metal matrix composite of  claim 1 , wherein the aluminum alloy comprises from about 91.2 wt % to about 98.6 wt % aluminum, from about 0.15 wt % to about 4.9 wt % copper, from about 0.1 wt % to about 1.8 wt % magnesium, and from about 0.1 wt % to about 1 wt % manganese. 
     
     
         6 . The metal matrix composite of  claim 1 , wherein the aluminum alloy comprises from about 91.2 wt % to about 94.7 wt % aluminum, from about 3.8 wt % to about 4.9 wt % copper, from about 1.2 wt % to about 1.8 wt % magnesium, and from about 0.3 wt % to about 0.9 wt % manganese. 
     
     
         7 . The metal matrix composite of  claim 1 , wherein the aluminum alloy comprises from about 92.8 wt % to about 95.8 wt % aluminum, from about 3.2 wt % to about 4.4 wt % copper, from 0 to about 0.2 wt % iron, from about 1.0 to about 1.6 wt % magnesium, from 0 to about 0.6 wt % oxygen, from 0 to about 0.25 wt % silicon, and from 0 to about 0.25 wt % zinc. 
     
     
         8 . The metal matrix composite of  claim 1 , wherein the aluminum alloy comprises from about 95.8 wt % to about 98.6 wt % aluminum, from about 0.8 wt % to about 1.2 wt % magnesium, and from about 0.4 wt % to about 0.8 wt % silicon. 
     
     
         9 . The metal matrix composite of  claim 1 , wherein the average particle size of the reinforcement particles is about 0.3 μm. 
     
     
         10 . The metal matrix composite of  claim 1 , wherein the composite comprises from about 15 vol % to about 50 vol % of the reinforcement particles. 
     
     
         11 . The metal matrix composite of  claim 1 , wherein the metal matrix composite has a 0.2% offset yield strength of about 400 MPa to about 680 MPa; an elastic modulus of about 80 GPa to about 150 GPa; and about 3% to about 8% elongation to failure, measured according to ASTM E8M. 
     
     
         12 . A method for making a metal matrix composite, comprising:
 high energy mixing (i) particles of an aluminum or aluminum alloy with (ii) reinforcement particles having an average particle size (D50) of from 0.1 μm to 0.5 μm; and   processing the mixture to achieve an even distribution of the reinforcement particles.   
     
     
         13 . The method of  claim 12 , wherein the high energy mixing is performed in an inert atmosphere. 
     
     
         14 . The method of  claim 12 , wherein the reinforcement particles comprise at least one ceramic material selected from the group consisting of carbides, oxides, silicides, borides, and nitrides. 
     
     
         15 . The method of  claim 12 , wherein the aluminum alloy comprises at least one element selected from the group consisting of chromium, copper, lithium, magnesium, manganese, zinc, iron, nickel, silver, scandium, vanadium and silicon. 
     
     
         16 . The method of  claim 12 , wherein the composite comprises from about 15 vol % to about 50 vol % of the reinforcement particles. 
     
     
         17 . A method for producing an article from a metal matrix composite, comprising:
 compacting the metal matrix composite to produce a billet; and   processing the billet to form the article.   
     
     
         18 . The method of  claim 17 , wherein the compacting is performed at a pressure of about 30 MPa to about 150 MPa. 
     
     
         19 . The method of  claim 17 , wherein the compacting is performed by hot isostatic pressing (HIP). 
     
     
         20 . An article formed from a metal matrix composite, the metal matrix composite comprising:
 an aluminum or aluminum alloy matrix; and   reinforcement particles dispersed in the matrix, the reinforcement particles having an average particle size (D50) of from 0.1 μm to 0.5 μm.

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