Novel highly porous ceramic and metal aerogels from xerogel powder precursors, and methods for their production and use

Patent metadata

Field	Value
Publication number	US-2020377421-A1
Application number	US-202016842968-A
Country	US
Kind code	A1
Filing date	Apr 8, 2020
Priority date	Apr 6, 2018
Publication date	Dec 3, 2020
Grant date	—

Abstract

The present invention discloses novel methods for producing highly porous ceramic and/or metal aerogel monolithic objects that are hard, sturdy, and resistant to high temperatures. These methods comprise preparing nanoparticulate oxides of metals and/or metalloids via a step of vigorous stirring to prevent gelation, preparing polymer-modified xerogel powder compositions by reacting said nanoparticulate oxides with one or more polyfunctional monomers, compressing said polymer-modified xerogel powder compositions into shaped compacts, and carbothermal conversion of the shaped xerogel compacts via pyrolysis to provide the highly porous ceramic and/or metal aerogel monolithic objects that have the same shapes as to their corresponding xerogel compact precursors. Representative of the highly porous ceramic and/or metal aerogel monolithic objects of the invention are ceramic and/or metal aerogels of Si, Zr, Hf, Ti, Cr, Fe, Co, Ni, Cu, Ru, Au, and the like. Examples include sturdy, shaped, highly porous silicon carbide (SiC), silicon nitride (Si3N4), zirconium carbide (ZrC), hafnium carbide (HfC), chromium carbide (Cr3C2), titanium carbide (TiC), zirconium boride (ZrB2), hafnium boride (HfB2), and metallic aerogels of iron (Fe), nickel (Ni), cobalt (Co), copper (Cu), ruthenium (Ru), gold (Au), and the like. Said aerogel monolithic objects have utility in various applications such as, illustratively, in abrasives, in cutting tools, as catalyst support materials such as in reformers and converters, as filters such as for molten metals and hot gasses, in bio-medical tissue engineering such as bone replacement materials, in applications requiring strong lightweight materials such as in automotive and aircraft structural components, in ultra-high temperature ceramics, and the like.

First claim

1 - 19 . (canceled)

20 . A method for preparing sturdy, shaped, highly porous metal carbide monolithic aerogel objects, wherein the metal carbide is selected from ZrC, HfC, TiC, and Cr 3 C 2 , said method comprising the steps of:
(a) preparing a nanoparticulate polyurea-modified metal-oxide composite xerogel powder in accordance with steps (a), (b) and (d) of the method of claim 16 ; (b) compressing said nanoparticulate polyurea-modified metal-oxide composite xerogel powder in one or more dies under a pressure between about 10,000 psi and about 20,000 psi, to obtain one or more shaped, nanoparticulate polyurea-modified metal-oxide composite xerogel monolithic compacts; (c) subjecting said shaped, nanoparticulate polyurea-modified metal-oxide composite xerogel monolithic compacts to pyrolysis under flowing Ar gas at a temperature between about 1300° C. and about 1700° C. for a period of between about 24 hours and about 48 hours, to obtain the sturdy, shaped, highly porous metal carbide monolithic aerogel objects.

21 . The method of claim 20 , wherein the metal carbide monolithic aerogel objects have porosities ≥35%.

22 . The method of claim 20 , wherein the metal carbide monolithic aerogel objects have porosities ≥85%.

23 . A method for preparing sturdy, shaped, highly porous metal boride monolithic aerogel objects, wherein the metal boride is selected from ZrB 2 and HfB 2 , said method comprising the steps of:
(a) preparing a nanoparticulate polyurea-modified metal-oxide/boron-oxide composite xerogel powder in accordance with steps (a), (c) and (d) of the method of claim 16 ; (b) compressing said nanoparticulate polyurea-modified metal-oxide/boron-oxide composite xerogel powder in one or more dies under a pressure between about 10,000 psi and about 20,000 psi, to obtain one or more shaped, nanoparticulate polyurea-modified metal-oxide/boron-oxide composite xerogel monolithic compacts; (c) subjecting said shaped, nanoparticulate polyurea-modified metal-oxide/boron-oxide composite xerogel monolithic compacts to pyrolysis under flowing Ar gas at a temperature between about 130° C. and about 1700° C. for a period of between about 24 hours and about 48 hours, to obtain the highly porous metal boride monolithic aerogel objects.

24 . The method of claim 23 , wherein the metal boride monolithic aerogel objects have porosities in the range between about 65% and about 90%.

25 . A method for preparing sturdy, shaped, highly porous, pure metal monolithic aerogel objects, wherein the metal is selected from Fe, Co, Ni, Cu, Ru, and Au, said method comprising the steps of:
(a) preparing a first solution comprising a metal oxide-precursor in a first solvent, wherein the metal oxide-precursor is a metal chloride salt, and the first solvent is an alcohol selected from MeOH and EtOH; (b) treating the first solution of metal oxide-precursor under vigorous stirring with an amount of H 2 O such that the mol/mol ratio of H 2 O:metal oxide-precursor is between about 5 and about 7, followed by addition of a proton-scavenging agent in an amount such that the mol/mol ratio of proton-scavenging agent:metal oxide-precursor is between about 7 and about 12, then with addition of a non-polar solvent selected from hexane and pentane in an amount between about 1000 mL and about 2000 mL per mol of metal oxide-precursor, then followed by continued vigorous stirring at ambient temperature for an initial period of time between about 25 minutes and about 40 minutes, then with a second addition of a non-polar solvent selected from hexane and pentane in an amount between about 500 mL to about 1000 mL per mol of metal oxide-precursor, then with an aging period of time ranging between about 18 hours and about 30 hours under continued vigorous stirring, to provide a metal-oxide suspension, followed by subjecting the metal-oxide suspension to between 1 and 5 washings with one or more wash solvents selected from an ester solvent and a ketone solvent, and removing of the solvents, to provide a nanoparticulate metal-oxide slurry; (c) reacting the nanoparticulate metal-oxide slurry obtained in step (b) with one or more polyisocyanate compound in an ester solvent at a temperature between about 55° C. and about 75° C. for a period of time between about 2 days and about 4 days, followed by 1-3 washings with an ester solvent, and drying under vacuum at a temperature between about 50° C. and about 80° C., to obtain a nanoparticulate polyurea-modified metal-oxide composite xerogel powder, wherein the polyisocyanate compound is a compound of the general formula G 1 -(NCO) q , in which G 1 is a moiety selected from C 1 -C 10 straight chain alkyl or branched alkyl or cycloalkyl, alkylaryl, aryl, heteroalkyl, heterocyclylalkyl, or heteroaryl, each of which is optionally substituted, and q is an integer in the range 2-6, and wherein the amount of polyisocyanate compound used is such that the ratio of total NCO groups per mol of metal-oxide precursor is in the range of between about 0.2 and about 0.5; (d) compressing said nanoparticulate polyurea-modified metal-oxide composite xerogel powder in one or more dies under a pressure between about 10,000 psi and about 20,000 psi, to obtain one or more shaped, nanoparticulate polyurea-modified metal-oxide composite xerogel monolithic compacts; (e) subjecting said shaped, nanoparticulate polyurea-modified metal-oxide composite xerogel monolithic compacts to one or more pyrolysis under one or more flowing gas, to obtain the pure, sturdy, shaped, highly porous metal monolithic aerogel objects;
wherein the one or more pyrolysis in step (e) includes a first pyrolysis at a temperature between about 700° C. and about 900° C. for a period between about 3 hours and about 7 hours under flowing Ar gas, to result in impure metal aerogels that contain residual carbon, followed by a second pyrolysis at a temperature between about 700° C. and about 900° C. under water-saturated H 2 for a period between about 30 hours and about 42 hours to remove the residual carbon.

26 . The method of claim 25 , wherein the proton-scavenging agent is epichlorohydrin, and wherein the polyisocyanate compound is one or more compound of the general formula (II):

wherein the isocyanate groups of compound (II) are independently attached to their respective aryl rings at the 2, 3, or 4-positions of the aryl rings; and, wherein R1, R2, and R3 are independently one or more substituents selected from H, alkyl, cycloalkyl, alkoxy, alkylthio, aryl, aryloxy, arylthio, each of which is optionally substituted, and halogen, nitro, or cyano.

27 . A nanoparticulate polyurea-modified metal-oxide composite xerogel powder composition obtained in accordance with steps (a)-(c) of the method of claim 25 , wherein the metal is selected from Fe, Co, Ni, Cu, Ru, and Au.

28 . The method of claim 25 , wherein the porous metal monolithic aerogel objects have porosities ≥35%.

29 . The method of claim 25 , wherein the porous metal monolithic aerogel objects have porosities ≥85%.

Assignees

• Univ Missouri

Inventors

• Leventis Nicholas
• Sotiriou-Leventis Chariklia
• Saeed Malik Adnan
• Rewatkar Parwani
• Taghvaee Tahereh

Classifications

• B22F1/054

  Nanosized particles · CPC title

• C04B38/0045 Primary

  by a process involving the formation of a sol or a gel, e.g. sol-gel or precipitation processes · CPC title

• B22F3/1103 Primary

  with particular physical characteristics · CPC title

• B22F3/1143

  involving an oxidation, reduction or reaction step · CPC title

• B22F9/24

  starting from liquid metal compounds, e.g. solutions · CPC title