System for generating an inert gas for an aircraft using liquid hydrogen

Patent metadata

Field	Value
Publication number	US-12540772-B2
Application number	US-202217972901-A
Country	US
Kind code	B2
Filing date	Oct 25, 2022
Priority date	Oct 27, 2021
Publication date	Feb 3, 2026
Grant date	Feb 3, 2026

Abstract

A system for generating an inert fluid, the system being carried on board an aircraft, the generation system including a plurality of devices configured each, in succession, to execute a separation of components of a primary fluid initially collected in the form of compressed hot air, the system including at least one heat exchanger configured to execute a separation of components, by change of phase of a component of the primary fluid, executing a cooling of the primary fluid using liquid hydrogen, supplied with liquid hydrogen collected from a tank of the aircraft. It is thus possible to generate an inert gas without requiring membrane separation of the nitrogen and the oxygen, and while at the same time making it easier to warm the liquid hydrogen stored and used in the aircraft as a source of energy.

First claim

The invention claimed is:

1 . A method for generating an inert fluid in an aircraft having a tank of liquid hydrogen, from a primary fluid initially collected from compressed hot air, the primary fluid comprising, as components, water, carbon dioxide, dioxygen, and nitrogen, the method comprising:
a first step of separating components of said primary fluid by cooling said primary fluid to extract water from said primary fluid in liquid form, a second step of separating components of said primary fluid by cooling said primary fluid to extract carbon dioxide from said primary fluid in liquid form, a third step of separating components of the primary fluid, by cooling said primary fluid after said second step to extract dioxygen from said primary fluid in liquid form, a step of liquefying said primary fluid after said third step of separating components to form liquid nitrogen by cooling the primary fluid with the liquid hydrogen, and followed by a step of pumping said liquid nitrogen towards a tank, wherein the first step of separating components of said primary fluid comprises cooling of the primary fluid in a first heat exchanger using ambient air; wherein the second step of the separating components of the primary fluid comprises cooling of the primary fluid in a second heat exchanger with said dioxygen extracted during the third step;
wherein the third step of separating components of the primary fluid comprises a cooling of the primary fluid using said liquid nitrogen;
wherein the first step of separating components, the second step of separating components, and the third step of separating components of said primary fluid occur by a change of a phase of a component of the primary fluid.

2 . The method for generating an inert fluid according to claim 1 , further comprising:
a step of liquefying said primary fluid, after said first step and said second step, and followed by a step of warming said liquefied primary fluid, suitable for extracting nitrogen in gaseous form.

3 . The method for generating an inert fluid according to claim 1 , wherein the successive steps of separating components of said primary fluid, by cooling said primary fluid, each use a heat exchanger, the heat exchangers used being fed in parallel, each via a motorized valve, from a liquid-hydrogen tank of the aircraft.

4 . The method for generating an inert fluid according to claim 1 , wherein the successive steps of separating components of said primary fluid, by cooling said primary fluid, each use a heat exchanger, the heat exchangers being arranged in series so that the liquid hydrogen used at an inlet of a heat exchanger for cooling said primary fluid during a component-separating step comes at least in part from an outlet of another heat exchanger used for cooling said primary fluid in another step of separating components of said primary fluid.

5 . The method for generating an inert fluid according to claim 1 , further comprising:
a step of liquefying said primary fluid, after said first step and second step, wherein the first step and second step of separating components of the primary fluid each comprise a cooling of the primary fluid in a heat exchanger by means of the liquefied primary fluid, and wherein said step of liquefying the primary fluid comprises a cooling of the primary fluid in a heat exchanger by means of said liquid hydrogen.

6 . The method of claim 1 , wherein the first step of separating components, the second step of separating components, and the third step of separating components of said primary fluid do not utilize a membrane for separation of the primary fluid.

Assignees

• Airbus Operations Sas

Inventors

• Belleville Mathieu
• Horde Théophile

Classifications

• F25J2210/40

  Air or oxygen enriched air, i.e. generally less than 30mol% of O2 · CPC title

• F25J1/0067

  Hydrogen · CPC title

• F25J1/0027

  Oxides of carbon, e.g. CO2 · CPC title

• F25J1/0015

  Nitrogen · CPC title

• F25J1/004 Primary

  by flash gas recovery (F25J1/0267 takes precedence) · CPC title