US2014227125A1PendingUtilityA1

Systems and methods for fabricating objects from bulk metallic glass matrix composites using primary crystallization

Assignee: CALIFORNIA INST OF TECHNPriority: Feb 11, 2013Filed: Feb 11, 2014Published: Aug 14, 2014
Est. expiryFeb 11, 2033(~6.5 yrs left)· nominal 20-yr term from priority
C22C 1/11A63B 2209/00C22C 45/00B22D 17/00B22F 3/225A63B 53/04B22D 25/06C22C 45/10B22F 3/087B22F 3/02B22D 17/20
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Claims

Abstract

Systems and methods in accordance with embodiments of the invention implement bulk metallic glass matrix composites in the fabrication of objects. In one embodiment, a method of fabricating an object including a bulk metallic glass matrix composite includes: forming a bulk metallic glass matrix composite composition into the shape of the object to be fabricated; and developing the bulk metallic glass matrix composite composition to include non-equilibrium inclusions that are softer than the surrounding matrix as measured by one of: the shear modulus, the elastic limit, and the hardness; where the bulk metallic glass matrix composite composition is such that the extent of the presence of the inclusions can be made to vary.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
         1 . A method of fabricating an object including a bulk metallic glass matrix composite comprising:
 forming a bulk metallic glass matrix composite composition into the shape of the object to be fabricated; and   developing the bulk metallic glass matrix composite composition to include non-equilibrium inclusions that are softer than the surrounding matrix as measured by one of: the shear modulus, the elastic limit, and the hardness;   wherein the bulk metallic glass matrix composite composition is such that the extent of the presence of the inclusions can be made to vary.   
     
     
         2 . The method of  claim 1 , wherein the forming of the bulk metallic glass matrix composite composition is achieved using one of: a thermoplastic forming technique and a casting technique. 
     
     
         3 . The method of  claim 2  wherein the forming of the bulk metallic glass matrix composite composition is achieved using one of: die casting, injection casting, rapid capacitive discharge forming, powder injection metallurgy, and investment casting. 
     
     
         4 . The method of  claim 2 , wherein the non-equilibrium inclusions are developed such that they impart desired materials properties in the object to be fabricated. 
     
     
         5 . The method of  claim 4 , wherein developing the bulk metallic glass matrix composite composition to include non-equilibrium inclusions comprises subjecting the bulk metallic glass matrix composite composition to an appropriate cooling rate. 
     
     
         6 . The method of  claim 5 , wherein subjecting the bulk metallic glass matrix composite composition to an appropriate cooling rate develops non-equilibrium inclusions in a first region of the object to be fabricated, but not in a second region of the object to be fabricated. 
     
     
         7 . The method of  claim 6 , wherein the second region of the object to be fabricated is locally heat treated to develop non-equilibrium inclusions. 
     
     
         8 . The method of  claim 4 , wherein developing the bulk metallic glass matrix composite comprises heat treating the formed bulk metallic glass matrix composite composition. 
     
     
         9 . The method of  claim 8 , wherein the heat treating is annealing. 
     
     
         10 . The method of  claim 8 , wherein the heat treating is localized to regions of the formed bulk metallic glass matrix composite composition. 
     
     
         11 . The method of  claim 4 , wherein the extent of the presence of the inclusions can be made to vary by thermal processing. 
     
     
         12 . The method of  claim 4 , wherein the crystalline structures that are developed undergo martensitic transformation when subjected to strain beyond a predetermined threshold. 
     
     
         13 . The method of  claim 4 , wherein the bulk metallic glass matrix composite composition does not include beryllium. 
     
     
         14 . The method of  claim 4 , wherein the bulk metallic glass matrix composite composition is Zr 48 Cu 47.5 Al 4 CO 0.5 . 
     
     
         15 . The method of  claim 4 , wherein the non-equilibrium inclusions are B2 phase inclusions. 
     
     
         16 . The method of  claim 4 , wherein, the bulk metallic glass matrix composite composition is Cu 47.5 Zr 47.5 Al 5 . 
     
     
         17 . The method of  claim 4 , wherein the bulk metallic glass matrix composite composition is one of: a CuZr-based composition, a TiCu-based composition, an NiTi-based composition, a CuZnAl-based composition, an FeNi-based composition, NiP-based composition, FeP-based composition, a FeNiCoAlTaB-based composition, a ZrTi-based composition, a ZrNb-based composition, an NiNb-based composition, a ZrV-based composition, a TiNB-based composition, a ZrTiTa-based composition, TiV-based composition, TiTa-based composition, a ZrTa-based composition, and a ZrCu based composition. 
     
     
         18 . The method of  claim 4 , wherein the non-equilibrium inclusions are spherical. 
     
     
         19 . The method of  claim 4 , wherein the object to be formed is a golf head casing. 
     
     
         20 . The method of  claim 19 , wherein a striking surface of the golf head casing is locally heat treated to develop the non-equilibrium inclusions.

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