Gas separation membrane module and gas separation method

US9718023B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9718023-B2
Application numberUS-201113288095-A
CountryUS
Kind codeB2
Filing dateNov 3, 2011
Priority dateNov 4, 2010
Publication dateAug 1, 2017
Grant dateAug 1, 2017

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  1. Title

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  2. Abstract

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Abstract

Official abstract text for this publication.

A process for producing nitrogen-rich air by feeding high temperature air at 150° C. or more to an air separation membrane module is described. After being placed at 175° C. for two hours, the air separation module exhibits a shape-retention ratio of 95% or more in one embodiment. The nitrogen-rich air can be fed to a fuel tank for an aircraft, for example.

First claim

Opening claim text (preview).

The invention claimed is: 1. A process for producing nitrogen-rich air from the air using an air separation membrane module including an air separation membrane, the process comprising feeding the air at 175° C. or higher to the air separation membrane, wherein the air separation membrane in the air separation membrane module comprises a material having no glass-transition temperature at 300° C. or lower, wherein for the air separation membrane module, at the initiation of the use, an oxygen-gas permeation rate (P′ O2 ) at 175° C. is 20×10 −5 cm 3 (STP)/cm 2 ·sec ·cmHg or more and a ratio of an oxygen-gas permeation rate to a nitrogen-gas permeation rate (P′ O2 /P′ N2 )at 175° C. is 1.8 or more; and after the use at 175° C. for 140 hours, P′ O2 and P′ O2 /P′ N2 are retained in levels of 90% or more of P′ O2 and P′ O2 /P′ N2 before the initiation of the use, respectively. 2. A process for producing nitrogen-rich air from the air using an air separation membrane module including an air separation membrane, the process comprising feeding the air at 175° C. or higher to the air separation membrane, wherein the air separation membrane in the air separation membrane module comprises a material having no glass-transition temperature at 300° C. or lower, wherein after being placed at 175° C. for 2 hours, the air separation membrane exhibits a shape-retention ratio of 95% or more. 3. A method for explosion protection of an aircraft, comprising producing nitrogen-rich air by the production process as claimed in claim 1 and feeding the nitrogen-rich air to a fuel tank for an aircraft. 4. A method for explosion protection of an aircraft, comprising producing nitrogen-rich air by the production process as claimed in claim 2 and feeding the nitrogen-rich air to a fuel tank for an aircraft. 5. The process according to claim 1 , wherein the material having no glass-transition temperature at 300° C. or lower in the air separation membrane comprises polyimide. 6. The process according to claim 2 , wherein the material having no glass-transition temperature at 300° C. or lower in the air separation membrane comprises polyimide.

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What does patent US9718023B2 cover?
A process for producing nitrogen-rich air by feeding high temperature air at 150° C. or more to an air separation membrane module is described. After being placed at 175° C. for two hours, the air separation module exhibits a shape-retention ratio of 95% or more in one embodiment. The nitrogen-rich air can be fed to a fuel tank for an aircraft, for example.
Who is the assignee on this patent?
Kanetsuki Yutaka, Tanihara Nozomu, Nakamura Tomohide, and 1 more
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 Aug 01 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).