Counter-flow gas separation modules and methods
US-9340297-B2 · May 17, 2016 · US
US2016136570A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016136570-A1 |
| Application number | US-201414542748-A |
| Country | US |
| Kind code | A1 |
| Filing date | Nov 17, 2014 |
| Priority date | Nov 17, 2014 |
| Publication date | May 19, 2016 |
| Grant date | — |
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An air separation module includes a plurality of fibers located within a casing. A fiber membrane defines an exterior of each of the plurality of fibers. The fiber membrane also forms an interior passage along a length of each of the plurality of fibers. The fiber membrane is configured to permeate a gas through the fiber membrane. At least one perforated canister is placed between the plurality of fibers. The at least one perforated canister is configured to collect a permeated gas from the plurality of fibers.
Opening claim text (preview).
1 . An air separation module comprising: a casing; a plurality of fibers located within the casing; a fiber membrane defining an exterior of each of the plurality of fibers, thereby forming an interior passage along a length of each of the plurality of fibers, the fiber membrane being configured to permeate a gas through the fiber membrane; and at least one perforated canister is placed between the plurality of fibers, wherein the at least one perforated canister is configured to collect a permeated gas from the plurality of fibers. 2 . The air separation module of claim 1 , wherein the at least one perforated canister includes a cross-sectional profile configured to maximize a surface area of the at least one perforated canister with respect to a number of the plurality of fibers in the air separation module. 3 . The air separation module of claim 2 , wherein the at least one perforated canister includes a plurality of perforated canisters. 4 . The air separation module of claim 3 , wherein each of the plurality of perforated canisters is configured to maximize a surface area of the plurality of perforated canisters with respect to a volume in the air separation module. 5 . The air separation module of claim 1 , wherein each of the plurality of fibers is configured to expel a nitrogen-enriched gas from an outlet end of each of the plurality of fibers. 6 . The air separation module of claim 1 , wherein the perforated canister includes perforations, the perforations configured to maximize an amount of collected permeated gas with respect to the number of the plurality of fibers in the air separation module. 7 . The air separation module of claim 1 , wherein the casing includes a casing inlet and a casing outlet. 8 . The air separation module of claim 7 , wherein the air separation module is positioned within an aircraft comprising: a turbine engine; and a compressor with a bleed system connected to the casing inlet. 9 . A method for removing oxygen from engine bleed air, the method comprising: feeding fluid into an air separation module, wherein the air separation module comprises: a casing; a plurality of fibers located within the casing; a fiber membrane defining an exterior of each of the plurality of fibers; at least one perforated canister is inserted between the plurality of fibers; forcing the fluid down the length of the plurality of fibers; permeating a first portion of the fluid through the fiber membrane to create a permeated fluid; collecting a portion of the permeated fluid into the at least one perforated canister; expelling the permeated fluid from the casing; and removing any non-permeated fluid from the casing through an outlet located on an end of the casing. 10 . The method of claim 9 , wherein the at least one perforated canister includes a cross-sectional profile configured to maximize a surface area of the at least one perforated canister with respect to a number of the plurality of fibers in the air separation module. 11 . The method of claim 9 , wherein the perforated canister includes perforations, the perforations configured to maximize an amount of collected permeated gas with respect to the number of the plurality of fibers in the air separation module. 12 . The method of claim 11 , further comprising: introducing the nitrogen-enriched gas into a fuel tank to reduce an oxygen concentration below a level necessary for combustion. 13 . The method of claim 9 , wherein the fluid is bleed air from a compressor. 14 . The method of claim 13 , wherein the fluid is compressed RAM air. 15 . The method of claim 9 , wherein the at least one perforated canister includes a plurality of perforated canisters that contain cross-sectional profiles configured to maximize a surface area of the plurality of perforated canisters with respect to a volume in the air separation module.
by diffusion (manufacturing semi-permeable membranes B01D67/00; form, structure or properties of semi-permeable membranes B01D69/00; material for semi-permeable membranes B01D71/00) · CPC title
Elements in parallel · CPC title
with hollow fibres · CPC title
Oxygen · CPC title
Hollow fibre modules · CPC title
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