Catalytic fuel tank inerting apparatus for aircraft
US-2018148189-A1 · May 31, 2018 · US
US11834191B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11834191-B2 |
| Application number | US-202117526355-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 15, 2021 |
| Priority date | Oct 2, 2018 |
| Publication date | Dec 5, 2023 |
| Grant date | Dec 5, 2023 |
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A system and method for providing dried inert gas to a protected space is disclosed.
Opening claim text (preview).
What is claimed is: 1. A system for providing inert gas to a protected space, comprising a boost compressor configured to receive pressurized air and boost a pressure of the pressurized air; a chemical inert gas generator; and an inert gas flow path in operative fluid communication with the chemical inert gas generator, a condenser and the protected space, wherein the condenser operates at a pressure greater than or equal to 2 atmospheres absolute pressure and is located between the chemical inert gas generator and the protected space along the inert gas flow path. 2. The system of claim 1 , wherein the chemical inert gas generator comprises a catalytic oxidation unit. 3. The system of claim 2 , wherein the catalytic oxidation unit operates at a temperature greater than 150° C. 4. The system of claim 1 , wherein the chemical inert gas generator comprises a proton exchange membrane electrochemical device. 5. The system of claim 4 , wherein the pressurized air flow path further comprises a heat exchanger. 6. The system of claim 4 , wherein the pressurized air flow path comprises a heat exchanger before the boost compressor and an additional heat exchanger after the boost compressor. 7. The system of claim 1 , wherein the chemical inert gas generator comprises a solid oxide electrochemical device. 8. The system of claim 7 , wherein the chemical inert gas generator operates at a temperature greater than 700° C. 9. The system of claim 7 , wherein the inert gas flow path further comprises a heat exchanger between the chemical inert gas generator and the compressor. 10. The system of claim 1 , wherein the pressurized air flow path comprises a bypass valve in parallel with the boost compressor.
Safety measures not otherwise provided for, e.g. preventing explosive conditions · CPC title
by refrigeration (condensation) · CPC title
in electrochemical cells · CPC title
using gases or vapours that do not support combustion, e.g. steam, carbon dioxide · CPC title
in aircraft {(A62C3/0207 takes precedence)} · CPC title
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