Gas separation device with nanocomposite membrane

US9815019B1 · US · B1

Patent metadata
FieldValue
Publication numberUS-9815019-B1
Application numberUS-201715683225-A
CountryUS
Kind codeB1
Filing dateAug 22, 2017
Priority dateOct 22, 2015
Publication dateNov 14, 2017
Grant dateNov 14, 2017

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  5. First independent claim

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Abstract

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A nanocomposite membrane including α-Al 2 O 3 membrane support, a γ-Al 2 O 3 intermediate layer that is 300-1200 nm thick and coats a surface of the membrane support, and a nanocomposite layer including SiO 2 and Y 2 O 3 that is 25-150 nm thick and coats a surface of the intermediate layer, wherein the nanocomposite layer is porous with an average largest radius micropore of 0.2-0.6 nm. A method of manufacturing the nanocomposite membrane, whereby the membrane support is coated with the γ-Al 2 O 3 , a silica source is hydrolyzed with a mixture of water, an alcohol solvent, and a Y source with a sol-gel technique yield a Si/Y sol-gel, the membrane support is dip coated with the Si/Y sol-gel, and the nanocomposite membrane is calcined. A method of separating a mixture of gas, whereby the mixture of gas is introduced into a permeance cell and fed through the nanocomposite membrane.

First claim

Opening claim text (preview).

The invention claimed is: 1. A gas separation device, comprising: a permeance cell having an upstream feed end and a downstream permeate end, and a nanocomposite membrane between the upstream feed end and the downstream permeate end of the permeance cell, wherein the nanocomposite membrane is configured to separate a first gas having high permeance through the nanocomposite membrane from a second gas having low permeance through the nanocomposite membrane; wherein the nanocomposite membrane comprises: a tubular α-Al 2 O 3 membrane support; an intermediate layer comprising γ-Al 2 O 3 , wherein the intermediate layer is 300-1200 nm thick and coats a surface of the tubular α-Al 2 O 3 membrane support; a nanocomposite layer comprising SiO 2 and Y 2 O 3 , wherein the nanocomposite layer is 25-150 nm thick and coats a surface of the intermediate layer; wherein the nanocomposite layer is porous with an average largest radius micropore 0.2-0.6 nm. 2. The gas separation device of claim 1 , wherein the intermediate layer comprises at least two distinct γ-Al 2 O 3 layers, each distinct γ-Al 2 O 3 layer being 150-600 nm thick. 3. The gas separation device of claim 1 , wherein the Y 2 O 3 the form of nanoparticles with a largest dimension of 1-6 nm, the nanocomposite layer is in the form of a SiO 2 matrix, and the Y 2 O 3 nanoparticles are dispersed in or deposited onto the SiO 2 matrix. 4. The gas separation device of claim 3 , wherein the nanocomposite layer is porous with an average mesopore radius of 1-4 nm. 5. The gas separation device of claim 1 , wherein the molar ratio of Si:Y in the nanocomposite membrane is 1:1 to 5:1. 6. The gas separation device of claim 1 , wherein the nanocomposite membrane has a membrane permeance of 1e −8 -1e −6 mol/m 2 ·sec·Pa for the first gas, and a membrane permeance of 1e −10 -1e −9 mol/m 2 ·sec·Pa for the second gas when a mixture of gas comprising the first gas and the second gas is fed through the permeance cell at a temperature of 100-650° C. 7. The gas separation device of claim 6 , wherein the first gas is H 2 , He, or both, and the second gas is N 2 , CO 2 , or both. 8. The gas separation device of claim 1 , wherein the nanocomposite membrane has a membrane permeance of 1e −8 -1e −6 mol/m 2 ·sec·Pa for the first gas, and a membrane permeance of 1e −10 -1e −9 mol/m 2 ·sec·Pa for the second gas when a mixture of gas comprising the first gas, the second gas, and up to 5 wt % of steam relative to the total weight of the mixture of gas is fed through the nanocomposite membrane. 9. A method of separating a mixture of gas comprising a first gas and a second gas, comprising: introducing the mixture of gas into the upstream feed end of the permeance cell of the gas separation device of claim 1 , wherein the nanocomposite layer of the nanocomposite membrane faces toward the upstream feed end and forms a permeable barrier between the upstream feed end and the downstream permeate end; applying a vacuum to the downstream permeate end; and separating the first gas from the second gas by allowing the first gas to pass through the nanocomposite membrane and to the downstream permeate end, and prohibiting the second gas from passing through the nanocomposite membrane. 10. The method of claim 9 , wherein the first gas is H 2 , He, or both, and the second gas is N 2 , CO 2 , or both.

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What does patent US9815019B1 cover?
A nanocomposite membrane including α-Al 2 O 3 membrane support, a γ-Al 2 O 3 intermediate layer that is 300-1200 nm thick and coats a surface of the membrane support, and a nanocomposite layer including SiO 2 and Y 2 O 3 that is 25-150 nm thick and coats a surface of the intermediate layer, wherein the nanocomposite layer is porous with an average largest radius micropore of 0.2-0.6 nm. A m…
Who is the assignee on this patent?
Univ King Fahd Pet & Minerals
What technology area does this patent fall under?
Primary CPC classification B01D53/228. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Nov 14 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 5 related publications on this page (citations in our corpus or others sharing the same primary CPC).