Air separation modules, nitrogen generation systems, and methods of making air separation modules

US11420151B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11420151-B2
Application numberUS-202016787764-A
CountryUS
Kind codeB2
Filing dateFeb 11, 2020
Priority dateFeb 12, 2019
Publication dateAug 23, 2022
Grant dateAug 23, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

An air separation module includes a canister, a separator, and a first end cap. The canister has an interior, a first open end in fluid communication with the interior of the canister, and a second end opposite the first open end of the canister. The separator is arranged within the interior of the canister, the separator fluidly coupling the second open end of the canister with the first open end of the canister. The first end cap has a one-piece first end cap body, is fixed to the first open end of the canister and has a first flange portion and a first aircraft-mounting portion. The canister supported by the first aircraft-mounting portion through the first flange portion of the one-piece first end cap body without an intermediate support structure. Nitrogen generation systems and methods of making nitrogen generation systems are also described.

First claim

Opening claim text (preview).

What is claimed is: 1. An air separation module, comprising: a canister having an interior, a first open end in fluid communication with the interior of the canister, and a second open end opposite the first open end of the canister, wherein the canister comprises stiffeners formed unitarily with the canister as a one-piece body and which extend radially outwardly from an outer surface of the canister and longitudinally along the canister between the first and second open ends to stiffen the canister and to eliminate a need to support the air separation module using a support structure, each of the stiffeners comprising fillets at respective bases thereof; a separator arranged within the interior of the canister, the separator fluidly coupling the second open end of the canister with the first open end of the canister; and a first end cap with a one-piece first end cap body fixed to the first open end of the canister, wherein the one-piece first end cap body has a flange portion and an aircraft-mounting portion, the canister supported by the aircraft-mounting portion through the flange portion of the one-piece first end cap body without an intermediate support structure. 2. The air separation module of claim 1 , wherein the one-piece first end cap body has a boss portion defining an inlet therethrough, the inlet in fluid communication with the separator through the first open end of the canister. 3. The air separation module of claim 1 , wherein the flange portion defines therethrough a fastener pattern and further comprising a plurality of fasteners fixing the first end cap to the first open end of the canister. 4. The air separation module of claim 1 , wherein the canister has a boss with a port, the boss arranged between the first open end of the canister and the second open end of the canister, the port in fluid communication with the first open end of the canister through the separator. 5. The air separation module of claim 1 , wherein the separator is configured to separate nitrogen molecules from oxygen molecules in air received at the first open end of the canister, the separator arranged to fluidly communicate the nitrogen molecules to the second open end of the canister, the separator further arranged to fluidly communicate the oxygen molecules to a port defined between first open end and the second open end of the canister. 6. The air separation module of claim 2 , further comprising a second end cap with a one-piece second end cap body, the one-piece second end cap body having a second flange portion and a conduit portion, the second flange portion of the one-piece second end cap body fixing the second end cap to the second open end of the canister, the conduit portion of one-piece second end cap body in fluid communication with the separator. 7. The air separation module of claim 6 , wherein the second end cap one-piece body comprises: an oxygen sensor seat portion with an oxygen sensor seated directly thereon, wherein the conduit portion is in fluid communication with the oxygen sensor seat portion; an oxygen sensor probe seat portion with an oxygen sensor probe seated directly on the oxygen sensor seat portion; a flow control valve seated directly on the conduit; a temperature sensor seat portion with a temperature sensor seated directly thereon; and a probe conduit integrated with the one-piece first end cap body and fluidly coupling the oxygen sensor probe to the oxygen sensor. 8. The air separation module of claim 1 , wherein the aircraft- mounting portion extends radially outward from the flange portion, the aircraft-mounting portion defining a first clevis and a second clevis. 9. The air separation module of claim 1 , further comprising a bleed air conduit fluidly coupled to the canister by the one-piece first end cap body and in fluid communication therethrough with the separator, and wherein the air separation module is a single canister air separation module having one and not more than one canister. 10. A nitrogen generator system, comprising: an air separation module as recited in claim 1 , wherein the one-piece first end cap body has a boss portion defining an inlet therethrough, the inlet in fluid communication with the separator through the first open end of the canister; a second end cap with a one-piece second end cap body, the one-piece second end cap body having a second flange portion and a conduit portion, the second flange portion of the one-piece second end cap body fixing the second end cap to the second open end of the canister, the conduit portion of one-piece second end cap body in fluid communication with the separator; and a fuel tank fluidly coupled to the canister by the one-piece second end cap body and in fluid communication therethrough through the separator. 11. The nitrogen generator system of claim 10 , wherein the flange portion defines therethrough a fastener pattern and further comprising a plurality of fasteners fixing the first end cap to the first open end of the canister; and wherein the canister has a boss with a port, the boss arranged between the first open end of the canister and the second open end of the canister, the port in fluid communication with the first open end of the canister through the separator. 12. The nitrogen generator system of claim 10 , wherein the second end cap one-piece body has a temperature sensor seat portion, and further comprising: a temperature sensor seated directly on the temperature sensor seat portion and without an intermediate duct; and a flow control valve seated directly on the conduit portion of the one-piece second end cap body and without an intermediate duct. 13. A method of making an air separation module, comprising: defining a canister having an interior, a first open end in fluid communication with the interior of the canister, and a second open end opposite the first open end of the canister, wherein the canister comprises stiffeners formed unitarily with the canister as a one-piece body and which extend radially outwardly from an outer surface of the canister and longitudinally along the canister between the first and second open ends to stiffen the canister and to eliminate a need to support the air separation module using a support structure, each of the stiffeners comprising fillets at respective bases thereof; arranging a separator within the interior of the canister, the separator fluidly coupling the second open end of the canister with the first open end of the canister; defining a first end cap with a one-piece first end cap body, wherein the one-piece first end cap body has a first flange portion and an aircraft-mounting portion; fixing the first flange portion of the one-piece first end cap body to the first open end of the canister; and supporting the canister with the aircraft mounting portion through the first flange portion of the one-piece first end cap body without an intermediate support structure. 14. The method of claim 13 , further comprising: defining a second end cap with a one-piece second end cap body, the one-piece second end cap body having a second flange portion and a conduit portion; and fixing the second flange portion of the one-piece second end cap body to the second open end of the canister such that the conduit of the one-piece second end cap body is in fluid communication with the separator. 15. The method of claim 14 , further comprising: defining a temperature sensor seat portion on the one-piece second end cap body; seating a temperature sensor directly on the temperature sensor seat portion and without an intermediate duct; and seating a flow contro

Assignees

Inventors

Classifications

  • B64D37/32Primary

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

  • the air being conditioned (pressurising B64D13/02) · CPC title

  • B01D53/22Primary

    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

  • comprising on board oxygen generator systems · CPC title

  • using gases or vapours that do not support combustion, e.g. steam, carbon dioxide · CPC title

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What does patent US11420151B2 cover?
An air separation module includes a canister, a separator, and a first end cap. The canister has an interior, a first open end in fluid communication with the interior of the canister, and a second end opposite the first open end of the canister. The separator is arranged within the interior of the canister, the separator fluidly coupling the second open end of the canister with the first open …
Who is the assignee on this patent?
Hamilton Sundstrand Corp
What technology area does this patent fall under?
Primary CPC classification B64D37/32. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Aug 23 2022 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 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).