Inerting system

Patent metadata

Field	Value
Publication number	US-11260346-B2
Application number	US-201816018017-A
Country	US
Kind code	B2
Filing date	Jun 25, 2018
Priority date	Jun 25, 2018
Publication date	Mar 1, 2022
Grant date	Mar 1, 2022

Abstract

A system is disclosed for providing inerting gas to a protected space. The system includes an electrochemical cell including a cathode, an anode separated by a separator that includes an ion transfer medium, and an electrical connection to a power source or power sink. 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, and an anode fluid flow path is in operative fluid communication with a catalyst at the anode, and includes an anode fluid flow path outlet. A cathode supply fluid flow path is disposed between the protected space and the cathode fluid flow path inlet, and an inerting gas flow path is in operative fluid communication with the cathode flow path outlet and the protected space.

First claim

What is claimed is:

1. A system for providing inerting gas to a protected space, comprising
an electrochemical cell comprising a cathode and an anode separated by a separator comprising an ion transfer medium;
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;
a cathode supply fluid flow path between the protected space and the cathode fluid flow path inlet;
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 or power sink;
an inerting gas flow path in operative fluid communication with the cathode flow path outlet and the protected space;
a gas treatment module configured to remove fuel vapor, smoke, or a contaminant from the cathode supply flow path, wherein the gas treatment module includes a membrane separator comprising the cathode supply fluid flow path on a first side of a membrane, and the inerting gas flow path as a sweep gas on a second side of the membrane.

2. The system of claim 1 , further comprising a water removal module on the cathode supply fluid flow path, or the cathode fluid flow path, or the inerting gas flow path.

3. The system of claim 2 , wherein the water removal module is on the inerting gas flow path.

4. The system of claim 2 , wherein the water removal module includes any one or combination of: a heat exchanger condenser, a gas-liquid separator, a membrane dryer, a desiccant.

5. The system of claim 4 , wherein the water removal module comprises a heat exchanger condenser and a membrane dryer.

6. The system of claim 5 , wherein the membrane dryer includes the inerting gas flow path on a first side of a membrane, and a sweep gas flow path comprising ram air exhaust from a heat absorption side of the heat exchanger condenser.

7. The system of claim 1 , wherein the ion transfer medium comprises a proton exchange membrane, and the electrochemical cell is configured to produce protons at the anode and transfer the protons across the proton exchange membrane to the cathode.

8. The system of claim 1 , wherein the ion transfer medium comprises a solid oxide, and the electrochemical cell is configured to produce oxygen anions at the cathode and transfer the oxygen anions across the solid oxide ion transfer medium to the anode.

9. The system of claim 1 , wherein the inerting gas flow path is further in operative communication with a fire suppression system.

10. The system of claim 1 , wherein the protected space comprises a fuel tank ullage space.

11. An aircraft comprising:
an aircraft body and an engine;
an electrochemical cell comprising a cathode and an anode separated by a separator comprising an ion transfer medium;
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;
a cathode supply fluid flow path between the protected space and the cathode fluid flow path inlet;
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 or power sink;
an inerting gas flow path in operative fluid communication with the cathode flow path outlet and the protected space;
a gas treatment module configured to remove fuel vapor, smoke, or a contaminant from the cathode supply flow path, wherein the gas treatment module includes a membrane
separator comprising the cathode supply fluid flow path on a first side of a membrane, and the inerting gas flow path as a sweep gas on a second side of the membrane.

12. The aircraft of claim 11 , wherein the protected space is selected from a fuel tank ullage space, a cargo hold, or an equipment bay.

13. The aircraft of claim 12 , wherein the cathode supply fluid flow path receives fluid flow from any one or more of the fuel tank ullage space, cargo hold, or equipment bay, and the inerting gas flow path delivers inerting gas to any one or more of the fuel tank ullage space, cargo hold, or equipment bay.

14. The aircraft of claim 11 , wherein the protected space comprises a fuel tank ullage space.

15. A method of inerting a protected space, comprising
delivering gas from the protected space to a cathode of an electrochemical cell;
reducing oxygen at the cathode to generate oxygen-depleted air at the cathode of the electrochemical cell;
directing the oxygen-depleted air from the cathode of the electrochemical cell along an inerting gas flow path to the protected space;
directing gas from a cathode supply flow path to a gas treatment module configured to remove fuel vapor, smoke, or a contaminant from the cathode supply flow path, wherein the gas treatment module includes a membrane separator comprising the cathode supply fluid flow path on a first side of a membrane, and the inerting gas flow path as a sweep gas on a second side of the membrane.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Rheaume Jonathan

Classifications

• B01D53/265

  by refrigeration (condensation) · CPC title

• B01D53/326 Primary

  in electrochemical cells · CPC title

• B01D53/268

  by diffusion · CPC title

• B01D2256/10

  Nitrogen · CPC title

• B01D2259/4575

  in aeroplanes or space ships · CPC title