FUEL CELL AND FUEL CELL SYSTEM FOR AN AIRCRAFT

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.

Claims

1. A fuel cell for a fuel cell system wherein the fuel cell comprises a self-supporting membrane structure, wherein the membrane structure ion-conductively connects together a first open-pored cavity and a second open-pored cavity and separates them from one another in a gas-tight manner, wherein the first cavity and the second cavity are mutually penetrating.

2. The fuel cell of claim 1, wherein each of the first cavity and the second cavity is configured to receive at least one elongate straight interconnector body.

3. The fuel cell of claim 2, wherein each of the first cavity and the second cavity contains at least one gas channel which is configured to be elongate and straight such that the interconnector body can be received therein.

4. The fuel cell of claim 3, wherein a membrane structure region in each case connects together two adjacent gas channels ion-conductively and separates them from one another in a gas tight manner.

5. The fuel cell of claim 1, wherein a first straight gas channel contained in the first cavity and a second straight gas channel contained in the second cavity are arranged skewed relative to one another.

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

7. The fuel cell of claim 1, wherein an electrically conductive anode layer and an electrically conductive 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 another other of the first cavity and the second cavity.

8. The fuel cell of claim 1, further comprising a plurality of elongate interconnector elements which are configured to be inserted in each of the first cavity and the second cavity and to contact the membrane structure, the anode/cathode layer, or both the membrane structure and the anode/cathode layer.

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

10. The fuel cell of claim 1, further comprising at least one gas distributor which is on an inlet side and/or an outlet side of the membrane structure, wherein the gas distributor, which is arranged on the inlet side, 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 wherein the gas distributor, which is arranged on the outlet side, 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.

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

12. The fuel cell of claim 11, wherein the surface shape 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%.

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

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

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

16. An aircraft comprising a fuel cell system of claim 14.

17. A method of using a triply periodic level surface shape as a membrane structure of a fuel cell, comprising the membrane structure ion-conductively connecting together a volume which can be loaded with fuel and a volume which can be loaded with oxidation agent and separates them from one another in a gas tight manner.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0055] Example embodiments are explained in more detail below with reference to the appended schematic drawings. The drawings show:

[0056] FIG. 1 an example embodiment of a fuel cell;

[0057] FIG. 2 a series of diagonal sections of a membrane structure;

[0058] FIG. 3 a series of orthogonal sections of the membrane structure from FIG. 2;

[0059] FIG. 4A a view of an inserted interconnector element;

[0060] FIG. 4B a detail view of the contact region of the interconnector element with the membrane structure;

[0061] FIG. 5 an example embodiment of an interconnector element;

[0062] FIG. 6 an example embodiment of a gas distributor; and

[0063] FIG. 7 views of membrane structures with different triply periodic level surface shapes.

DETAILED DESCRIPTION

[0064] Reference is firstly made to FIGS. 1 through 3, which show an example embodiment of the fuel cell 10. The fuel cell 10 is configured as a solid oxide fuel cell. The fuel cell 10 is configured such that it can be used in a fuel cell system of an aircraft.

[0065] The fuel cell 10 comprises a self-supporting membrane structure 12. The membrane structure 12 creates a first open-pored cavity 14 and a second open-pored cavity 16. The membrane structure 12 separates the first cavity 14 and the second cavity 16 from one another gas-tightly. The membrane structure 12 connects the first cavity 14 and the second cavity 16 together ion-conductively.

[0066] The membrane structure 12 preferably comprises a solid electrolyte 15 which allows the ion conduction.

[0067] The membrane structure 12 is configured such that the first cavity 14 and the second cavity 16 are mutually penetrating.

[0068] The membrane structure 12 forms a triply periodic level surface, for example a gyroid 17. Other such surfaces are conceivable.

[0069] Each cavity 14, 16 contains at least one gas channel 18. The gas channel 18 is configured as an elongate, substantially straight region so that a corresponding elongate, straight body may be inserted therein.

[0070] Adjacent gas channels 18 are separated from one another gas-tightly, but connected together ion-conductively, by a membrane structure region 20 of the membrane structure 12.

[0071] The membrane structure 12 has an electrically conductive contact layer 22. Depending on the arrangement of the contact layer 22, the contact layer 22 in the one cavity, for example the first cavity 14, is known as the anode layer 24, and the contact layer 22 in the other cavity, for example the second cavity 16, is known as the cathode layer 26.

[0072] The contact layer 22 serves to conduct the electrical energy generated in the fuel cell 10 to an electrical consumer, for example an electrically driven engine of the aircraft.

[0073] The fuel cell 10 furthermore comprises a plurality of interconnector elements 28 which are inserted in one of the gas channels 18. The interconnector element 28 is configured for example as a round bar or tube.

[0074] Reference is made below in particular to FIGS. 4A, 4B and FIG. 5. The interconnector element 28 preferably forms a linear contact 30 with the membrane structure 12. The linear contact 30 is helical in form. In other words, the linear contact 30 winds helically around the interconnector element 28 in its longitudinal direction.

[0075] The interconnector element 28 may have an interconnector body 32 which may be formed from an electrically conductive or isolating material. The interconnector element 28 may furthermore comprise a conductive strip 34 which is wound helically around the interconnector body 32 (FIG. 5).

[0076] The interconnector element 28 preferably defines, with the membrane structure 12, a gas passage region 36 which allows a gas flow along the outside of the interconnector elements 28. Alternatively or additionally, the gas stream may flow through the tubular interconnector element 28.

[0077] Reference is now made to FIG. 6. The fuel cell 10 may have a gas distributor 38. The gas distributor 38 is arranged for example on the inlet side 40 of the membrane structure 12. Further gas distributors, in particular on the outlet side of the membrane structure 12, may also be provided.

[0078] The gas distributor 38 is configured such that the fuel 40, for example hydrogen, can be conducted into the first cavity 14 while the oxidation agent 42, for example air, can be conducted into the second cavity 16.

[0079] The outlet-side gas distributor (not shown in detail) allows the discharge of the reaction products and residual gas. The outlet-side gas distributor is preferably configured identically to the inlet-side gas distributor 38.

[0080] FIG. 7 shows, as well as the gyroid 17, further triply periodic level surface shapes known as diamond, primitive and iWP. FIG. 7 also shows how the interconnector elements 28 are inserted in the gas channels 18.

[0081] Because of the intrinsic properties of the triply periodic level surface shapes, anodes 44 and cathodes 46 are preferably arranged alternately. As furthermore evident from FIG. 7, not all gas channels 18 need be equipped with an interconnector element 28.

[0082] In order to improve the usability of hybrid electric or fully electric aircraft, a fuel cell 10 is disclosed with improved efficiency and increased volume-specific or weight-specific energy density. The fuel cell 10 has a self-supporting membrane structure 12 which is configured as a triply periodic level surface which separates gas-tightly a first cavity 14 loaded with fuel 40, from a second cavity 16 loaded with oxidation agent 42, but connects the two cavities 14, 16 together ion-conductively.

[0083] While at least one example embodiment of the present invention(s) is disclosed herein, it should be understood that modifications, substitutions and alternatives may be apparent to one of ordinary skill in the art and can be made without departing from the scope of this disclosure. This disclosure is intended to cover any adaptations or variations of the example embodiment(s). In addition, in this disclosure, the terms “comprise” or “comprising” do not exclude other elements or steps, the terms “a”, “an” or “one” do not exclude a plural number, and the term “or” means either or both. Furthermore, characteristics or steps which have been described may also be used in combination with other characteristics or steps and in any order unless the disclosure or context suggests otherwise. This disclosure hereby incorporates by reference the complete disclosure of any patent or application from which it claims benefit or priority.

LIST OF REFERENCE SIGNS

[0084] 10 Fuel cell [0085] 12 Self-supporting membrane structure [0086] 14 First open-pored cavity [0087] 15 Solid electrolyte [0088] 16 Second open-pored cavity [0089] 17 Gyroid [0090] 18 Gas channel [0091] 20 Membrane structure region [0092] 22 Electrically conductive contact layer [0093] 24 Anode layer [0094] 26 Cathode layer [0095] 28 Interconnector element [0096] 30 Linear contact [0097] 32 Interconnector body [0098] 34 Conductive strip [0099] 36 Gas passage [0100] 38 Gas distributor [0101] 40 Fuel [0102] 42 Oxidation agent [0103] 44 Anode [0104] 46 Cathode