Emergency power system for an aircraft

Patent metadata

Field	Value
Publication number	US-9617006-B2
Application number	US-200913139066-A
Country	US
Kind code	B2
Filing date	Dec 11, 2009
Priority date	Dec 12, 2008
Publication date	Apr 11, 2017
Grant date	Apr 11, 2017

Abstract

The present invention relates to an emergency power system for an aircraft having at least one fuel cell unit for producing electric power, wherein the fuel cell unit is cooled via at least one cooling circuit which includes at least one heat exchanger, and wherein the heat exchanger is connected to at least one air distribution system of the aircraft cabin so that exhaust air heated by the heat exchanger in the operation of the emergency power system can be distributed via the air distribution system in the aircraft cabin.

First claim

The invention claimed is:

1. A method of providing electric power to an aircraft in an emergency comprising the steps of
operating an emergency power system for the aircraft such that electric energy is provided to the aircraft in an emergency upon breakdown or failure of a main power system of the aircraft, wherein the emergency power system comprises at least one fuel cell unit for generating the electrical energy,
connecting the fuel cell unit by at least one air distribution system of the aircraft to a cabin of the aircraft,
in emergency operation of the emergency power system, exhausting heated air generated by the fuel cell unit over the air distribution system and distributing said heated air into the aircraft cabin for internal cooling of the fuel cell unit in a pressure mode and withdrawing air from the aircraft cabin in a suction mode,
selectively additionally cooling the fuel cell unit during said emergency operation in said pressure mode and said suction mode by at least one separate cooling circuit comprising at least one heat exchanger receiving the air from the aircraft cabin,
cooling the heated air generated by the fuel cell by the heat exchanger, and
exhausting the heated air generated by the heat exchanger downstream of the heat exchanger over the air distribution system and distributing the heated air into the aircraft cabin for internal cooling of the fuel cell unit.

2. The method of claim 1 , wherein the air distribution system comprises a mixing chamber, or at least one distribution line, and comprising the additional step of
introducing into the mixing chamber, exhaust air of the heat exchanger and/or the fuel cell unit by pressure operation or removing from the mixing chamber, inflow air of the heat exchanger and/or the fuel cell unit by suction operation.

3. The method of claim 1 , comprising the additional step of
supplying the fuel cell unit with air from the environment of the fuel cell unit, from the environment of the heat exchanger, from at least one pipe or passage, or from at least one other air inflow line.

4. The method of claim 1 , wherein a regulation unit and at least one fan are provided, and comprising the additional step of
regulating power of the at least one fan or carrying out an on/off control of the at least one fan with the regulating unit, wherein the fan is at least one of a recirculation fan of the air distribution system or a separate fan associated with the fuel cell unit.

5. The method of claim 1 , comprising the additional step of
providing at least one isolation valve such that one or more zones of the aircraft cabin can be blocked and not charged with the heated air generated by the heat exchanger and/or fuel cell unit.

6. The method of claim 1 , wherein the air distribution system comprises
at least one recirculation fan,
at least one line or recirculation line which opens into a mixing chamber of the air distribution system and into which line air flow can be produced by the recirculation fan, and comprising the additional step of
opening at least one exhaust air line of the heat exchanger and/or the fuel cell unit into the line downstream or upstream of the recirculation fan.

7. The method of claim 6 , comprising the additional steps of
arranging at least one recirculation filter in the line upstream of the recirculation fan, and
opening the exhaust air line of the heat exchanger and/or of the fuel cell unit into the line between the recirculation filter and the recirculation fan.

8. The method of claim 1 , wherein the air distribution system comprises at least one recirculation fan and at least one mixing chamber, and comprising the additional steps of
opening at least one line or recirculation line into the mixing chamber such that an air flow is produced by the recirculation fan, and
branching off at least one inflow air line of the heat exchanger and/or fuel cell unit from the line downstream or upstream of the recirculation fan.

9. The method of claim 8 , wherein at least one recirculation filter is provided in a conduit of the recirculation line upstream of the recirculation fan, and comprising the additional step of
branching off an inflow line of the heat exchanger and/or fuel cell unit from the recirculation line, upstream of the recirculation filter and the recirculation fan, between the recirculation filter and the recirculation fan, or downstream of the recirculation filter and the recirculation fan.

10. The method of claim 9 , wherein a plurality of recirculation fans, having at least one exhaust air line or at least one inflow air line, are provided in the air distribution system, and comprising the additional step of
connecting the at least one exhaust air line or at least one inflow air line during emergency operation, to at least one exhaust air line or at least one inflow air line of the heat exchanger and/or of the fuel cell unit by at least one connection line.

11. The method of claim 1 , comprising the additional step of
arranging at least one bypass valve such that it enables a throughflow of a line of the air distribution system without a throughflow of the heat exchanger and/or the fuel cell unit when in a first position and enables a throughflow of the heat exchanger and/or the fuel cell unit in a second position, is provided.

12. The method of claim 1 , comprising the additional step of
arranging at least one recirculation fan such that the heat exchanger and/or the fuel cell unit is directly in the suction train of the recirculation fan.

13. The method of claim 1 , comprising the additional step of
providing and arranging at least one fan in association with the fuel cell unit and upstream and/or downstream of the fuel cell unit,
opening at least one exhaust air line of the heat exchanger and/or the fuel cell unit into one of a mixing chamber of the air distribution system or an air distribution line of the air distribution system, and
arranging the heat exchanger and/or fuel cell unit such that inflow air is supplied to it from the environment of the fuel cell unit, from the heat exchanger, from at least one pipe or passage, or from at least one other inflow line.

14. The method of claim 13 , comprising the additional step of
connecting the inflow line of the heat exchanger and/or fuel cell unit to a mixing chamber of the air distribution system or branching off the inflow line of the heat exchanger from a line or recirculation line such that air can be conducted into a mixing chamber of the air distribution system by a recirculation fan of the air distribution system.

15. The method of claim 1 , wherein the air distribution system comprises a mixing chamber having at least one exhaust air line by which air is conducted from a mixing chamber of the air distribution system into at least one zone of the aircraft cabin, and comprising the additional step of
arranging the heat exchanger and/or fuel system such that it is flowed through by air flowing through the exhaust air line of the mixing chamber of the air distribution system,
wherein the air throughflow of the heat exchanger and/or the fuel cell unit takes place by at least one recirculation fan of the air distribution system and/or at least one fan associated with the fuel cell unit and arranged upstream and/or downstream of the heat exchanger and/or of the fuel cell unit.

16. The method of claim 1 , wherein a mixing chamber of the air distribution system is provided, such that the mixing chamber has at least one exhaust air line by which air can be conducted from the mixing chamber into at least one zone of the aircraf

Assignees

• Brugger Ralf
• Frick Jörn
• Herzog Jacques
• Metzler Dirk
• Liebherr Aerospace Lindenberg GmbH

Inventors

• Brugger Ralf
• Frick Jörn
• Herzog Jacques
• Metzler Dirk

Classifications

• B64D2041/005

  Fuel cells · CPC title

• Y02T90/36

  Cross-Sectional Technologies · mapped topic

• B64D2041/002

  Mounting arrangements for auxiliary power units (APU's) · CPC title

• B64D13/08 Primary

  the air being heated or cooled · CPC title

• B64D41/00

  Power installations for auxiliary purposes · CPC title