US2023280508A1PendingUtilityA1

Visible quality additive manufactured aluminum mirror finishing

Assignee: RAYTHEON COPriority: Jul 15, 2020Filed: May 11, 2023Published: Sep 7, 2023
Est. expiryJul 15, 2040(~14 yrs left)· nominal 20-yr term from priority
G02B 5/0808B33Y 80/00B33Y 70/10B32B 15/20B32B 18/00B32B 7/12B32B 7/023B33Y 40/20B32B 15/017C22C 21/02B32B 2310/08B32B 2038/0064B22F 10/28C22C 21/00B22F 2999/00B33Y 70/00B22F 10/60B22F 10/62B22F 10/66Y02P10/25B32B 2307/416B32B 2551/08B32B 2307/536
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Claims

Abstract

A mirrored apparatus includes a substrate having a surface and including an additive manufactured aluminum and about 2 to about 30 weight % (wt. %) silicon. The mirrored apparatus also includes a finish layer arranged directly on the surface of the substrate. The finish layer includes a polished surface opposite the substrate. The mirrored apparatus further includes a reflective layer arranged on the polished surface of the finish layer.

Claims

exact text as granted — not AI-modified
1 - 14 . (canceled) 
     
     
         15 . A method of making a mirrored apparatus, the method comprising:
 forming, using additive manufacturing, a substrate having a surface and comprising aluminum and about 2 to about 30% wt. % silicon;   depositing a binding layer on the surface of the substrate, wherein the binding layer is titanium, nickel, nickel chromium, chromium, gold, aluminum, molybdenum, germanium, zinc sulfide, or any combination thereof;   after depositing the binding layer, depositing a finish layer on the binding layer;   polishing a surface of the finish layer opposite the substrate; and   depositing a reflective layer on the surface of the finish layer.   
     
     
         16 . (canceled) 
     
     
         17 . The method of  claim 15 , wherein the finish layer is silicon, chromium, nickel chromium, germanium, silicon carbide, silicon nitride, aluminum oxide, indium tin oxide, silicon monoxide, aluminum oxide, zirconium oxide, silicon oxide, titanium pentoxide, hafnium oxide, silicon aluminum oxide, or any combinations thereof. 
     
     
         18 . The method of  claim 15 , wherein the finish layer is radiation hardened and does not blister, peel, crack, or melt after being exposed to at least a 30 megarads total ionizing dose, at least a 1.43×10 13  neutrons/cm 2  (1 MeV equivalent) displacement damage dose, or a combination thereof 
     
     
         19 . The method of  claim 15 , wherein the aluminum further comprises about 1.5 to about 15 wt. % of a ceramic material. 
     
     
         20 . The method of  claim 15 , wherein the substrate further comprises an oxide, a nitride, a carbide material, or any combination thereof.

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