Fuel cell and fuel cell system for an aircraft

Patent metadata

Field	Value
Publication number	US-11876265-B2
Application number	US-202117462297-A
Country	US
Kind code	B2
Filing date	Aug 31, 2021
Priority date	Sep 16, 2020
Publication date	Jan 16, 2024
Grant date	Jan 16, 2024

Abstract

In order to improve usability of hybrid or fully electric aircraft, a fuel cell having improved efficiency and increased volume/weight specific energy density is provided. The fuel cell has a self-supporting membrane structure that is formed as a triply periodic level surface, which separates a first cavity supplied with gaseous fuel from a second cavity supplied with gaseous oxidizer in a gas-sealed manner while connecting the cavities in an ion-conductive manner.

First claim

The invention claimed is:

1. A fuel cell for a fuel cell system, the fuel cell comprising:
a first cavity that is open-pored and comprises one or more first gas channels;
a second cavity that is open-pored and comprises one or more second gas channels;
a membrane structure that is self-supporting; and
a plurality of interconnector elements that are elongate and straight, one or more interconnector elements of the plurality of interconnector elements comprising:
an interconnector body; and
a conductive strip that is wound helically around the interconnector body;

wherein the membrane structure ion-conductively connects together the first cavity and the second cavity and separates them from one another in a gas-tight manner;
wherein the first cavity and the second cavity are mutually penetrating;
wherein the one or more first gas channels is/are configured for receiving one or more first interconnector elements of the plurality of interconnector elements;
wherein the one or more first gas channels is/are configured for receiving one or more second interconnector elements of the plurality of interconnector elements;
wherein each of the one or more first interconnector elements is inserted into one of the one or more first gas channels and contacts the membrane structure; and
wherein each of the one or more second interconnector elements is inserted into one of the one or more second gas channels and contacts the membrane structure.

2. The fuel cell of claim 1 , wherein the membrane structure and the one or more interconnector elements define a gas passage region configured to allow a flow of gas along an outside of the one or more interconnector elements.

3. The fuel cell of claim 1 , wherein the membrane structure comprises a membrane structure region that connects together two adjacent first gas channels, two adjacent second gas channels, or one of the one or more first gas channels that is adjacent to one of the one or more second gas channels ion-conductively and separates them from one another in a gas tight manner.

4. The fuel cell of claim 1 , wherein at least one of the one or more first gas channels is arranged skewed relative to at least one of the one or more second gas channels.

5. The fuel cell of claim 1 , wherein the membrane structure contains a solid electrolyte.

6. The fuel cell of claim 1 , comprising:
an anode layer that is electrically conductive; and
a cathode layer that is electrically conductive;
wherein the anode layer and the cathode layer are arranged on the membrane structure;
wherein the anode layer is arranged in one of the first cavity and the second cavity and the cathode layer is arranged in the other of the first cavity and the second cavity.

7. The fuel cell of claim 6 , wherein the plurality of interconnector elements are configured to contact the anode layer and the cathode layer.

8. The fuel cell of claim 7 , wherein at least one interconnector element of the plurality of interconnector elements is configured to:
form a helical linear contact with the membrane structure and/or the anode/cathode layer when the at least one interconnector element is inserted in one of the first cavity and the second cavity; and/or
define, with the membrane structure and/or the anode/cathode layer, a gas passage region which allows a flow of gas in a longitudinal direction and/or in a circumferential direction and/or a helical flow of gas along the at least one interconnector element when the at least one interconnector element is inserted in one of the first cavity and the second cavity.

9. The fuel cell of claim 1 , comprising:
at least one gas distributor which is on an inlet side and/or an outlet side of the membrane structure;
wherein:
when the at least one gas distributor is arranged on the inlet side, the at least one gas distributor is configured such that one of the first cavity and the second cavity can be loaded with gaseous fuel and another of the first cavity and the second cavity can be loaded with gaseous oxidation agent; and/or
when the at least one gas distributor is arranged on the outlet side, the at least one gas distributor is configured such that reaction products and/or residual gas can be discharged from a respective one of the first cavity and the second cavity.

10. The fuel cell of claim 1 , wherein the membrane structure is in a form of a triply periodic level surface.

11. The fuel cell of claim 10 , wherein a shape of the triply periodic level surface is selected from a group of surface shapes consisting of a gyroid shape, a gyroid-like shape, a diamond shape, a diamond-like shape, an iWP shape, an iWP-like shape, a solid P-shape, a solid P-like shape, and also surface shapes which deviate from such shapes by less than 10%.

12. The fuel cell of claim 1 , where the fuel cell is a solid oxide fuel cell of an aircraft.

13. A fuel cell system for an aircraft comprising a plurality of fuel cells of claim 1 , which are electrically connected together in series, in parallel, or in series and parallel.

14. An aircraft comprising a fuel cell of claim 1 .

15. An aircraft comprising a fuel cell system of claim 13 .

16. A method of using a triply periodic level surface shape as a membrane structure of a fuel cell, the fuel cell comprising:
a first cavity that is open-pored and comprises one or more first gas channels;
a second cavity that is open-pored and comprises one or more second gas channels;
a membrane structure that is self-supporting;
a plurality of interconnector elements that are elongate and straight, one or more interconnector elements of the plurality of interconnector elements comprising:
an interconnector body; and
a conductive strip that is wound helically around the interconnector body;

wherein the membrane structure ion-conductively connects together the first cavity and the second cavity and separates them from one another in a gas-tight manner;
wherein the first cavity and the second cavity are mutually penetrating;
wherein the one or more first gas channels is/are configured for receiving one or more first interconnector elements of the plurality of interconnector elements;
wherein the one or more first gas channels is/are configured for receiving one or more second interconnector elements of the plurality of interconnector elements;
wherein each of the one or more first interconnector elements is inserted into one of the one or more first gas channels and contacts the membrane structure; and
wherein each of the one or more second interconnector elements is inserted into one of the one or more second gas channels and contacts the membrane structure;

the method comprising:
loading the first cavity with a fuel; and
loading the second cavity with an oxidation agent.

17. The method of claim 16 , wherein the membrane structure and the one or more interconnector elements define a gas passage region configured to allow a flow of gas along an outside of the one or more interconnector elements.

18. The method of claim 17 , comprising at least one gas distributor which is on an inlet side and/or an outlet side of the membrane structure, wherein the interconnector body of each of the one or more interconnector elements is in a form of a bar with circular cross-section.

Assignees

• Airbus Defence & Space Gmbh

Inventors

• Zimmermann Kristian
• Friedl Stephan
• Metzner Christian

Classifications

• H01M8/10 Primary

  Fuel cells with solid electrolytes · CPC title

• H01M8/0258

  characterised by the configuration of channels, e.g. by the flow field of the reactant or coolant · CPC title

• H01M8/0269

  Separators, collectors or interconnectors including a printed circuit board · CPC title

• H01M8/1006 Primary

  Corrugated, curved or wave-shaped MEA · CPC title

• H01M8/122

  Corrugated, curved or wave-shaped MEA · CPC title