Base Metal Catalyst
US-2015360178-A1 · Dec 17, 2015 · US
US11524276B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11524276-B2 |
| Application number | US-202017060770-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 1, 2020 |
| Priority date | Apr 17, 2020 |
| Publication date | Dec 13, 2022 |
| Grant date | Dec 13, 2022 |
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Provided is a p-type TiO 2 /n-type WO 3 heterojunction catalyst and a preparation method and use thereof. The catalyst comprises p-type TiO 2 and n-type WO 3 supported on a surface of the p-type TiO 2 .
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What is claimed is: 1. A p-type TiO 2 /n-type WO 3 heterojunction catalyst comprising: p-type TiO 2 ; and n-type WO 3 supported on a surface of the p-type TiO 2 ; wherein the p-type TiO 2 /n-type WO 3 heterojunction catalyst has a p-type TiO 2 content of 60% by mass to 80% by mass with respect to a total mass of the p-type TiO 2 /n-type WO 3 heterojunction catalyst. 2. A method for preparing the p-type TiO 2 /n-type WO 3 heterojunction catalyst according to claim 1 , the method comprising: supporting the n-type WO 3 onto a surface of the p-type TiO 2 to obtain the p-type TiO 2 /n-type WO 3 heterojunction catalyst. 3. The method according to claim 2 , further comprising: dissolving a titanium salt in a mixed solution of glycerol and a first alcohol to form a first mixture; dissolving a tungsten salt and a product resulting from a first heating process for heating the first mixture in a second alcohol to form a second mixture; and calcining a product resulting from a second heating process for heating the second mixture to produce the p-type TiO 2 /n-type WO 3 heterojunction catalyst. 4. The method according to claim 3 , wherein the first heating process is carried out at a temperature of 50° C. to 250° C. for 1 hour to 48 hours; wherein the first alcohol comprises at least one of methanol, ethanol, propanol, and isopropanol; wherein the titanium salt comprises at least one of titanium acetate, titanium oxalate, titanium chloride, tetrabutyl titanate, titanium nitrate, and titanium sulfate; wherein the second heating process is carried out at a temperature of 50° C. to 250° C. for 1 hour to 48 hours; wherein the calcining step is carried out at a temperature of 200° C. to 800° C. for 2 hours to 24 hours; wherein the tungsten salt comprises at least one of tungsten chloride, ammonium tungstate, ammonium metatungstate, and ammonium paratungstate; and wherein the second alcohol comprises at least one of methanol, ethanol, propanol, and isopropanol. 5. A method of producing a fuel, the method comprising: photochemically synthesizing the fuel from a fuel substrate in the presence of the p-type TiO 2 /n-type WO 3 heterojunction catalyst of claim 1 . 6. The method according to claim 5 , wherein photochemically synthesizing the fuel from the fuel substrate is carried out under light irradiation; wherein the fuel substrate comprises at least one of norbornene, dicylopentadiene, norbornadiene, isophorone, and cyclohexenone; and wherein an amount of the p-type TiO 2 /n-type WO 3 heterojunction catalyst is from 1% by mass to 10% by mass with respect to a total amount of the fuel substrate. 7. The method according to claim 6 , wherein the fuel is photochemically synthesized from the fuel substrate in a solvent; wherein the solvent comprises at least one of dichloromethane, normal pentane, dichloroethane, and cyclohexane. 8. The method according to claim 6 , wherein photochemically synthesizing the fuel from the fuel substrate in the presence of the p-type TiO 2 /n-type WO 3 heterojunction catalyst is carried out at a temperature of 0° C. to 80° C. for 1 hour to 24 hours under irradiation of a high-pressure mercury lamp. 9. The method according to claim 7 , wherein photochemically synthesizing the fuel from the fuel substrate in the presence of the p-type TiO 2 /n-type WO 3 heterojunction catalyst is carried out at a temperature of 0° C. to 80° C. for 1 hour to 24 hours under irradiation of a high-pressure mercury lamp. 10. The method according to claim 5 , wherein the fuel comprises a high-density fuel that is a multi-cyclic fuel for aerospace propulsion; wherein the fuel comprises at least one of pentacyclo[8.2.1.1 4,7 .0 2,9 .0 8,3 ]tetradecane, pentacyclo[5.3.0.0 2,6 .0 3,9 .0 5,8 ]decane, and quadricyclane.
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