Fuel fractioning unit for inert gas generating system

US10272390B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10272390-B2
Application numberUS-201715468888-A
CountryUS
Kind codeB2
Filing dateMar 24, 2017
Priority dateMar 24, 2017
Publication dateApr 30, 2019
Grant dateApr 30, 2019

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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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Abstract

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An inert gas generating system includes a source of a liquid hydrocarbon fuel, and a fractioning unit configured to receive a portion of the liquid hydrocarbon fuel from the source. The fractioning unit includes a perm-selective membrane configured to separate the portion of the liquid hydrocarbon fuel into substantially sulfur-free vapors and a sulfur-containing remainder. The system further includes a catalytic oxidation unit configured to receive and react the substantially sulfur-free vapors to produce an inert gas.

First claim

Opening claim text (preview).

The invention claimed is: 1. An inert gas generating system comprising: a source of a liquid hydrocarbon fuel; a fractioning unit configured to receive a portion of the liquid hydrocarbon fuel from the source, the fractioning unit comprising a perm-selective membrane configured to separate the portion of the liquid hydrocarbon fuel into substantially sulfur-free vapors and a sulfur-containing remainder; a pressure differential generator in fluid communication with a permeate side of the perm-selective membrane, wherein the pressure differential generator is configured to create a partial pressure gradient across the perm-selective membrane; and a catalytic oxidation unit configured to receive and react the substantially sulfur-free vapors to produce an inert gas. 2. The system of claim 1 , wherein the pressure differential generator is an air source configured to provide an air stream. 3. The system of claim 2 , wherein the air stream is selected from the group consisting of ambient air, ram air, fan air, engine bleed air, cabin air, and combinations thereof. 4. The system of claim 1 , wherein the pressure differential generator is a vacuum source. 5. The system of claim 1 further comprising: a fuel pump configured to provide the portion of the liquid hydrocarbon fuel to the fractioning unit. 6. The system of claim 1 , wherein the perm-selective membrane is a reverse selective membrane comprising a plurality of hollow fibers. 7. The system of claim 1 , wherein the perm-selective membrane is a reverse selective membrane in planar form having a spiral-wound or plate-and-frame configuration. 8. The system of claim 1 , wherein the perm-selective membrane comprises a silicone-based material. 9. The system of claim 1 further comprising: an inert gas passageway configured to provide the inert gas to a defined space. 10. The system of claim 9 , wherein the defined space is one of a fuel tank or a cargo hold. 11. The system of claim 1 , wherein the fractioning unit is configured to provide the sulfur-containing remainder to a main fuel line, and wherein the main fuel line comprises an engine-bound fuel flow. 12. A method for generating inert gas, the method comprising: providing a portion of liquid hydrocarbon fuel from a fuel source to a fractioning unit, the fractioning unit comprising a perm-selective membrane configured to separate the portion of the liquid hydrocarbon fuel into substantially sulfur-free vapors and a sulfur-containing remainder; creating a partial pressure gradient using a pressure differential generator in fluid communication with a permeate side of the perm-selective membrane such that a partial pressure of the substantially sulfur-free vapors of the liquid hydrocarbon fuel is lower on the permeate side of the perm-selective membrane; providing an amount of the substantially sulfur-free vapors drawn through the perm-selective membrane to a catalytic oxidation unit; and reacting the amount of the substantially sulfur-free vapors to produce the inert gas. 13. The method of claim 12 , wherein generating the partial pressure gradient comprises flowing an air stream over the permeate side of the perm-selective membrane. 14. The method of claim 12 , wherein generating the partial pressure gradient comprises operating a vacuum source in fluid communication with the permeate side of the perm-selective membrane.

Assignees

Inventors

Classifications

  • Spiral-wound membrane modules · CPC title

  • Distillation, fractionation or rectification for separating fractions, components or impurities during preparation or upgrading of a fuel · CPC title

  • by adsorption, e.g. preparative gas chromatography {(solid sorbent compositions B01J20/00, preparation of inorganic compounds or elements C01)} · CPC title

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

  • characterised by specific membranes · CPC title

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What does patent US10272390B2 cover?
An inert gas generating system includes a source of a liquid hydrocarbon fuel, and a fractioning unit configured to receive a portion of the liquid hydrocarbon fuel from the source. The fractioning unit includes a perm-selective membrane configured to separate the portion of the liquid hydrocarbon fuel into substantially sulfur-free vapors and a sulfur-containing remainder. The system further i…
Who is the assignee on this patent?
Hamilton Sundstrand Corp
What technology area does this patent fall under?
Primary CPC classification B01D63/04. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Apr 30 2019 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).