Supply system and method for providing electric energy, oxygen depleted air and water as well and aircraft having such a supply system

Patent metadata

Field	Value
Publication number	US-10173086-B2
Application number	US-201514808273-A
Country	US
Kind code	B2
Filing date	Jul 24, 2015
Priority date	Jul 29, 2014
Publication date	Jan 8, 2019
Grant date	Jan 8, 2019

Abstract

A supply system for providing at least oxygen depleted air and water in a vehicle includes a catalytic converter, at least one hydrogen supply means, at least one air supply means, at least one outlet for oxygen depleted air, and a control unit coupled with the catalytic converter. The catalytic converter is couplable with the hydrogen supply means and is adapted for producing water under consumption of hydrogen from the at least one hydrogen supply means and oxygen. The catalytic converter is further couplable with the at least one air supply means for additionally producing oxygen depleted air. Further, the control unit is adapted for selectively operating the catalytic converter based on a demand of water and oxygen depleted air.

First claim

The invention claimed is:

1. A supply system for providing at least oxygen depleted air and water in a vehicle, the system comprising:
a fuel cell;
an independent catalytic converter;
at least one hydrogen supply means;
at least one air supply means;
at least one outlet for oxygen depleted air; and
a control unit coupled with the catalytic converter,
wherein the fuel cell and the independent catalytic converter are couplable with the hydrogen supply means,
wherein the fuel cell is adapted for producing water and electric energy through conducting a fuel cell process under consumption of hydrogen from the at least one hydrogen supply means and oxygen;
wherein the independent catalytic converter is adapted for producing water under consumption of hydrogen from the at least one hydrogen supply means and oxygen,
wherein the independent catalytic converter is couplable with the at least one air supply means for additionally producing oxygen depleted air, and
wherein the control unit is adapted for selectively operating one or both of the fuel cell and the independent catalytic converter based on a demand for water, oxygen depleted air, and electrical energy,
wherein the independent catalytic converter comprises a turbo machine having a compressor and a turbine.

2. The supply system of claim 1 , further comprising an oxygen supply means for providing oxygen to the fuel cell in the absence of an air supply.

3. The supply system of claim 1 , wherein the control unit is adapted for operating the independent catalytic converter and the fuel cell at the same time for producing at least water and electric energy.

4. The supply system of claim 1 , wherein the fuel cell is couplable with the at least one air supply means for additionally producing oxygen depleted air.

5. The supply system of claim 1 , further comprising at least one of a water separator and a condenser.

6. The supply system of claim 1 , wherein the at least one air supply means comprises a bleed air line from a turbojet engine.

7. The supply system of claim 1 ,
wherein the independent catalytic converter comprises a housing, which is arranged in an air channel, and
wherein the independent catalytic converter is adapted for condensing water generated in the catalytic converter at the housing.

8. The supply system of claim 1 ,
wherein an air inlet of the independent catalytic converter is coupled with an exhaust air outlet of a compartment in the vehicle, and
wherein the at least one outlet for oxygen depleted air is coupled with an air inlet of the compartment.

9. A method for providing at least oxygen depleted air and water in an aircraft, the method comprising:
operating a catalytic converter comprising a turbo machine having a compressor and a turbine for producing water under consumption of hydrogen from at least one hydrogen supply means couplable with a hydrogen supply means of the catalytic converter, wherein the catalytic converter is operated independently of a fuel cell, the fuel cell being adapted for producing water and electric energy through conducting a fuel cell process under consumption of hydrogen from the at least one hydrogen supply means and oxygen; and
coupling at least one air supply means with the catalytic converter and operating the catalytic converter for additionally producing oxygen depleted air based on a demand of water and oxygen depleted air.

10. The method of claim 9 , further comprising operating the fuel cell for producing water and electrical power under consumption of hydrogen from the at least one hydrogen supply means couplable with a hydrogen supply means of the fuel cell and oxygen.

11. The method of claim 9 , further comprising recirculating exhaust air from a compartment in the vehicle to an air inlet of the catalytic converter.

12. The method of claim 9 , wherein the method further comprises operating the turbo machine.

13. An aircraft having a supply system comprising:
a fuel cell;
an independent catalytic converter;
at least one hydrogen supply means;
at least one air supply means;
at least one outlet for oxygen depleted air; and
a control unit coupled with the independent catalytic converter,
wherein the fuel cell and the independent catalytic converter are couplable with the hydrogen supply means,
wherein the fuel cell is adapted for producing water and electric energy through conducting a fuel cell process under consumption of hydrogen from the at least one hydrogen supply means and oxygen,
wherein the independent catalytic converter is adapted for producing water under consumption of hydrogen from the at least one hydrogen supply means and oxygen,
wherein the independent catalytic converter is couplable with the at least one air supply means for additionally producing oxygen depleted air, and
wherein the control unit is adapted for selectively operating one or both of the fuel cell and the independent catalytic converter based on a demand for water, oxygen depleted air, and electrical energy, and
wherein the independent catalytic converter comprises a turbo machine having a compressor and a turbine.

Assignees

• Airbus Operations Gmbh

Inventors

• Hoffjann Claus
• Law Barnaby
• Klewer Guido
• Lüdders Hauke-Peer

Classifications

• H01M8/04761

  of fuel cell exhausts · CPC title

• B01J19/0006

  Controlling or regulating processes (controlling or regulating in general G05) · CPC title

• H01M8/04291

  Arrangements for managing water in solid electrolyte fuel cell systems (H01M8/04119 takes precedence) · CPC title

• B01J19/0053

  Details of the reactor · CPC title

• B01J2219/00186

  controlling the composition of the reactive mixture · CPC title