Hydrogen storage system and aircraft comprising a hydrogen storage system

Patent metadata

Field	Value
Publication number	US-11769889-B2
Application number	US-202217691395-A
Country	US
Kind code	B2
Filing date	Mar 10, 2022
Priority date	Mar 17, 2021
Publication date	Sep 26, 2023
Grant date	Sep 26, 2023

Abstract

A hydrogen storage system comprises a hydrogen tank and a system for controlling hydrogen evaporation in the hydrogen tank. This control system comprises a hydrogen discharge pipe connected to the hydrogen tank, on the one hand, and to a controllable valve, on the other hand, as well as a processing unit configured to control the valve as a function of the pressure in the tank. The hydrogen storage system further comprises a fuel cell permanently connected to the hydrogen tank and the processing unit being electrically powered by the fuel cell.

First claim

The invention claimed is:

1. An aircraft comprising:
a hydrogen storage system comprising a hydrogen tank and a control system for controlling hydrogen evaporation in the hydrogen tank, the control system comprising:
a hydrogen discharge pipe connected at one end to the hydrogen tank and to a controllable valve at a second end;
a controller configured to control the valve as a function of a pressure value in the tank, to ensure that the pressure value inside the hydrogen tank does not exceed a first predetermined pressure threshold;
a fuel cell permanently and unbrokenly fluidically coupled to the hydrogen tank separately from the hydrogen discharge pipe to permanently generate electricity even when the aircraft is parked on ground as long as hydrogen remains in the tank, wherein the controller is electrically powered by the fuel cell.

2. The aircraft according to claim 1 , further comprising a propulsion system powered with energy by the hydrogen originating from the hydrogen storage system.

3. The aircraft according to claim 2 , wherein the propulsion system comprises an engine operating by the combustion of hydrogen originating from the hydrogen storage system.

4. The aircraft according to claim 2 , wherein the propulsion system comprises an electric motor and a fuel cell assembly supplied with hydrogen by the hydrogen storage system, the fuel cell assembly comprising an electric power supply for the electric motor.

5. The aircraft according to claim 4 , wherein the fuel cell of the hydrogen storage system forms part of the fuel cell assembly electrically powering the electric motor.

6. The aircraft according to claim 4 , wherein the fuel cell of the hydrogen storage system is independent of the fuel cell assembly electrically powering the electric motor.

7. The aircraft according to claim 6 , further comprising an electrical circuit configured to supply electric power to the electric motor via the fuel cell of the hydrogen storage system, in addition to the electric power supply to said motor via the fuel cell assembly.

8. The aircraft according to claim 6 , further comprising a non-propulsive system normally supplied with electricity by an on-board main electrical source of the aircraft, independent of the fuel cell of the hydrogen storage system and of the fuel cell assembly, and an electrical circuit configured to electrically power the non-propulsive system via the fuel cell of the hydrogen storage system in an event of a failure of the main electrical source.

9. The aircraft according to claim 4 , further comprising an electrical system separate from the controller, as well as an electrical circuit configured to electrically power this electrical system via the fuel cell of the hydrogen storage system when the aircraft is parked on the ground.

10. The aircraft according to claim 9 , wherein said electrical system corresponds to a system for heating at least one of the fuel cells of the fuel cell assembly.

11. The aircraft according to claim 4 , further comprising an electrical circuit configured to allow an external electrical system to be connected to the aircraft when the aircraft is parked on the ground, and to electrically power this electrical system via the fuel cell of the hydrogen storage system.

Assignees

• Airbus Sas
• Airbus Operations Sas

Inventors

• Landolt Jonathan
• Raspati Olivier

Classifications

• B64D27/355

  using fuel cells · CPC title

• B64D27/34

  All-electric aircraft · CPC title

• H01M8/04201

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

• B60L2200/10

  Air crafts · CPC title

• B60L50/70

  using power supplied by fuel cells (in combination with batteries B60L50/75) · CPC title