Fuel tank inerting system

US11040306B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11040306-B2
Application numberUS-201815946211-A
CountryUS
Kind codeB2
Filing dateApr 5, 2018
Priority dateApr 5, 2018
Publication dateJun 22, 2021
Grant dateJun 22, 2021

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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.

A fuel tank inerting system is disclosed, comprising a fuel tank and an electrochemical cell comprising a cathode and an anode separated by a separator comprising an anion transfer medium. A cathode fluid flow path is in operative fluid communication with a catalyst at the cathode between a cathode fluid flow path inlet and a cathode fluid flow path outlet. An anode fluid flow path is in operative fluid communication with a catalyst at the anode, and includes an anode fluid flow path outlet. An electrical connected to a power source is arranged to provide a voltage difference between the anode and the cathode. An air source is in operative fluid communication with either or both of the cathode flow path inlet and the anode flow path inlet. An inert gas flow path is in operative fluid communication with the cathode flow path outlet and the fuel tank.

First claim

Opening claim text (preview).

What is claimed is: 1. A fuel tank inerting system, comprising a fuel tank; an electrochemical cell comprising a cathode and an anode separated by a separator comprising an anion transfer medium, wherein the anion transfer medium comprises a solid polymer membrane comprising quaternary ammonium groups, quaternary pyridinium groups, quaternary imidazolium groups, amino groups, imidazole groups, or combinations thereof; a cathode fluid flow path in operative fluid communication with a catalyst at the cathode between a cathode fluid flow path inlet and a cathode fluid flow path outlet; an anode fluid flow path in operative fluid communication with a catalyst at the anode, including an anode fluid flow path outlet; an electrical connection to a power source, arranged to provide a voltage difference between the anode and the cathode; an air source in operative fluid communication with either or both of the cathode fluid flow path inlet and the anode fluid flow path inlet; and an inert gas flow path in operative fluid communication with the cathode fluid flow path outlet and the fuel tank. 2. The fuel tank inerting system of claim 1 , wherein the anion transfer medium comprises quaternary ammonium groups. 3. The fuel tank inerting system of claim 1 , wherein the anode fluid flow path is in fluid communication with the catalyst at the anode between an anode fluid flow path inlet and the anode fluid flow path outlet. 4. The fuel tank inerting system of claim 1 , further comprising a regenerative or replaceable carbon dioxide absorber in operative fluid communication with the air source and the cathode fluid flow path. 5. The fuel tank inerting system of claim 1 , further comprising a water source in operative fluid communication with the cathode fluid flow path. 6. A fuel tank inerting and power generation system, comprising the fuel tank inerting system of claim 1 ; an electrical connection between a power sink and the anode and cathode; and a controller configured to alternatively operate the electrochemical cell in a mode selected from a plurality of modes including at least: a first mode in which air and water is directed to the cathode, electric power is directed from the power source to the anode and cathode to provide a voltage difference between the anode and the cathode, and oxygen-depleted air is directed from the cathode to the fuel tank, and a second mode in which fuel is directed to the anode, electric power is directed from the anode and cathode to the power sink, and oxygen-depleted air is directed from the cathode to the fuel tank. 7. An aircraft fuel tank inerting system comprising an aircraft body and an engine, said engine in operative fluid communication with the fuel tank of the fuel tank inerting system of claim 1 . 8. An aircraft fuel tank inerting and air management system, comprising the fuel tank inerting system of claim 1 ; and a cabin air flow circulation path in operative fluid communication with a pressurized environmentally controlled cabin and the anode fluid flow path inlet and anode fluid flow path outlet.

Assignees

Inventors

Classifications

  • Reactant storage and supply, e.g. means for feeding, pipes · CPC title

  • Fuel cells · CPC title

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

  • Oxygen · CPC title

  • for containers filled with inflammable liquids · CPC title

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Frequently asked questions

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What does patent US11040306B2 cover?
A fuel tank inerting system is disclosed, comprising a fuel tank and an electrochemical cell comprising a cathode and an anode separated by a separator comprising an anion transfer medium. A cathode fluid flow path is in operative fluid communication with a catalyst at the cathode between a cathode fluid flow path inlet and a cathode fluid flow path outlet. An anode fluid flow path is in operat…
Who is the assignee on this patent?
Hamilton Sundstrand Corp, Hamilton Sunstrand Corp
What technology area does this patent fall under?
Primary CPC classification A62C3/08. Mapped technology areas include Human Necessities.
When was this patent published?
Publication date Tue Jun 22 2021 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 5 related publications on this page (citations in our corpus or others sharing the same primary CPC).