Counter-flow gas separation modules and methods

Patent metadata

Field	Value
Publication number	US-9340297-B2
Application number	US-201313770146-A
Country	US
Kind code	B2
Filing date	Feb 19, 2013
Priority date	Feb 19, 2013
Publication date	May 17, 2016
Grant date	May 17, 2016

Abstract

A gas separation method includes flowing a gas feed along a feed flow path within a housing directionally from a product end to a feed end of a gas separation membrane. After the feed flow path, the gas feed flows along a membrane flow path defined by the membrane from the feed end to the product end. The feed flow path is counter to the membrane flow path. Heat may be exchanged between the feed flow path and the membrane flow path and increase separation efficiency. Also, heat exchanged may compensate for some temperature drop in the membrane due to enthalpy of gas separation. A gas separation module includes a feed flow path within a housing extending directionally from a product end to a feed end of a membrane. The feed flow path is counter to a membrane flow path defined by the membrane.

First claim

What is claimed is:

1. A gas separation method comprising:
using an air separation module of an aircraft fuel tank flammability reduction system, the air separation module including a housing and a gas separation membrane within the housing, the gas separation membrane having a feed end and a product end with a retentate interior side and a permeate exterior side between the feed end and the product end;
supplying an air feed into the housing, the air feed containing oxygen gas and nitrogen gas;
flowing the air feed along a feed flow path within the housing directionally from the product end to the feed end of the gas separation membrane, the air feed being segregated from contact with the permeate exterior side;
after the feed flow path, flowing the air feed along a membrane flow path defined by the gas separation membrane from the feed end to the product end of the gas separation membrane, the feed flow path being counter to the membrane flow path;
contacting the retentate interior side with the air feed in the membrane flow path, permeating at least some of the oxygen gas from the air feed through the air separation membrane to the permeate exterior side, and producing retentate that is enriched in the nitrogen gas as a result of removing at least some of the oxygen gas from the air feed;
exchanging heat between the membrane flow path and the feed flow path counter to the membrane flow path and reducing a temperature drop along the membrane flow path compared to an arrangement with a feed flow path concurrent with the membrane flow path;
providing a configuration for the air separation module, selecting one or more process conditions, and, as a result, establishing a temperature of the product end of the gas separation membrane that is within 10° F. of a temperature of the feed end of the gas separation membrane, the established temperature of the product end increasing a separation efficiency of the air separation module compared to when the temperature of the product end is more than 10° F. below the temperature of the feed end; and
supplying the retentate, which contains nitrogen-enriched air, to a fuel tank on board the aircraft.

2. The method of claim 1 further comprising flowing the air feed along another feed flow path directionally from the product end to the feed end of the gas separation membrane, the other feed flow path being separated from the feed flow path, the air feed in the other feed flow path contacting the housing and, thereafter, flowing inside the hollow fiber membranes along the membrane flow path, and the other feed flow path being counter to the membrane flow path.

3. The method of claim 1 wherein the feed flow path is at least partially filled with structurally supportive porous material that allows gas flow through the porous material.

4. The method of claim 1 wherein establishing the temperature of the product end of the gas separation membrane within 10° F. of the temperature of the feed end of the gas separation membrane comprises compensating for at least a portion of the temperature drop in the gas separation membrane due to enthalpy of gas separation by increasing air feed flow rate compared to when the temperature of the product end is more than 10° F. below the temperature of the feed end and thus increasing the temperature of the product end of the gas separation membrane compared to when the temperature of the product end is more than 10° F. below the temperature of the feed end.

5. The method of claim 1 wherein the housing comprises an inner shell and an outer shell, the gas separation membrane is within the inner shell, and flowing the air feed along the feed flow path comprises flowing the air feed along a passage between the inner shell and the outer shell.

6. The method of claim 1 wherein flowing the air feed along the feed flow path or flowing the air feed along the membrane flow path or both comprise flowing the air feed along a plurality of separated flow paths.

7. The method of claim 1 wherein the gas separation membrane comprises a plurality of hollow fiber membranes, the gas separation module comprises a feed tubesheet within the housing securing the feed end of the plurality of hollow fiber membranes and a product tubesheet within the housing securing the product end of the plurality of hollow fiber membranes, and the method further comprises:
segregating the air feed and the permeate exterior side of the plurality of hollow fiber membranes with the feed tubesheet; and
segregating the permeate exterior side of the plurality of hollow fiber membranes and the retentate with the product tubesheet.

8. The method of claim 7 wherein the feed flow path extends among the plurality of hollow fiber membranes.

9. A gas separation method comprising:
using an air separation module of an aircraft fuel tank flammability reduction system, the air separation module including a housing and a gas separation membrane within the housing, the gas separation membrane having a feed end and a product end with a retentate interior side and a permeate exterior side between the feed end and the product end and including a plurality of hollow fiber membranes;
supplying an air feed into the housing, the air feed containing oxygen gas and nitrogen gas;
flowing the air feed along a feed flow path within the housing directionally from the product end to the feed end of the gas separation membrane, the feed flow path extending among and being surrounded by the plurality of hollow fiber membranes and the air feed being segregated from contact with the permeate exterior side;
after the feed flow path, flowing the air feed inside the hollow fiber membranes along a membrane flow path defined by the gas separation membrane from the feed end to the product end of the gas separation membrane, the feed flow path being counter to the membrane flow path;
contacting the retentate interior side with the air feed in the membrane flow path, permeating at least some of the oxygen gas from the air feed through the gas separation membrane to the permeate exterior side, and producing retentate that is enriched in the nitrogen gas as a result of removing at least some of the oxygen gas from the air feed;
exchanging heat between the membrane flow path and the feed flow path counter to the membrane flow path and reducing a temperature drop along the membrane flow path compared to an arrangement with a feed flow path concurrent with the membrane flow path;
compensating for at least a portion of the temperature drop in the gas separation membrane due to enthalpy of gas separation; and
supplying the retentate, which contains nitrogen-enriched air, to a fuel tank on board the aircraft.

10. The method of claim 9 further comprising flowing the air feed along another feed flow path directionally from the product end to the feed end of the gas separation membrane, the other feed flow path being separated from the feed flow path, the air feed in the other feed flow path contacting the housing and, thereafter, flowing inside the hollow fiber membranes along the membrane flow path, and the other feed flow path being counter to the membrane flow path.

11. The method of claim 9 wherein exchanging heat between the membrane flow path and the feed flow path counter to the membrane flow path increases a separation efficiency of the gas separation module compared to an arrangement with a feed flow path concurrent with the membrane flow path.

12. The method of claim 9 wherein compensating for at least a portion of the temperature drop comprises establishing a temperature of the product end of the gas separation membrane that is within 10° F. of a temperature of the feed end of the

Assignees

• Boeing Co

Inventors

• Cao Tuan Q

Classifications

• B01D2053/224

  with hollow fibres · CPC title

• B01D2259/4575

  in aeroplanes or space ships · CPC title

• B64D37/32 Primary

  Safety measures not otherwise provided for, e.g. preventing explosive conditions · CPC title

• B01D2256/10

  Nitrogen · CPC title

• B01D2257/104

  Oxygen · CPC title