Method for controlling the purity/flow rate relationship of an inert gas injected into a fuel tank, an inerting system for carrying out the method

Patent metadata

Field	Value
Publication number	US-10603529-B2
Application number	US-201715804297-A
Country	US
Kind code	B2
Filing date	Nov 6, 2017
Priority date	Nov 8, 2016
Publication date	Mar 31, 2020
Grant date	Mar 31, 2020

Abstract

An inerting system of a fuel tank of an aircraft includes an air separation module supplied at the inlet with air at a certain pressure to generate at the outlet an inert gas to be injected into the fuel tank comprising a certain flow rate and a certain oxygen concentration. A control method includes, at a given instant and at a constant air temperature and atmospheric pressure, (1) reducing the inert gas flow rate to a determined value, and (2) reducing the air pressure in order to cause an increase in the oxygen concentration from an initial value to a determined value. Decreasing the inert gas flow rate is performed by compensating for a loss of inert gas flow caused by the air pressure reduction, and decreasing the air pressure is performed by compensating for a reduction in the oxygen concentration caused by the inert gas flow rate reduction.

First claim

The invention claimed is:

1. A method for controlling an inerting system of at least one fuel tank of an aircraft, the inerting system comprising at least one air separation module supplied at the inlet with air at a certain pressure in order to generate at the outlet an inert gas to be injected into the fuel tank comprising a certain flow rate and a certain oxygen concentration, wherein the method comprises, at a given instant and at constant temperature and atmospheric pressure:
an operation whereby the inert gas flow rate is reduced to a determined value;
an operation whereby the air pressure is reduced in order to cause an increase in the oxygen concentration from an initial value to a determined value;
and wherein:
the operation of reducing the inert gas flow rate is performed by compensating for a loss of inert gas flow caused by the air pressure reduction operation;
the operation of reducing the air pressure is performed by compensating for a reduction in the oxygen concentration caused by the inert gas flow rate reduction operation.

2. A method according to claim 1 , wherein the determined inert gas flow rate value corresponds to a value determined as a function of an actual inert gas flow rate requirement at the given instant.

3. A method according to claim 1 , wherein the determined oxygen concentration value corresponds to a value determined as a function of an actual oxygen concentration requirement at the given instant.

4. A method according to claim 1 , wherein the determined oxygen concentration value corresponds to the initial oxygen concentration value before the operation of reducing the inert gas flow rate.

Assignees

• Zodiac Aerotechnics

Inventors

• Vandroux Olivier
• Missou Jérémie

Classifications

• A62C3/08 Primary

  in aircraft {(A62C3/0207 takes precedence)} · CPC title

• B64D37/32

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

• A62C3/065

  for containers filled with inflammable liquids · CPC title

• A62C99/0018

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

• B60K2015/03381

  for preventing explosions · CPC title