SYSTEM FOR THE STORAGE OF FUEL GASES

Abstract

Disclosed is a gas storage, preferably of hydrogen, and is in the form of a multi-capillary structure. The multi-capillary structure has a constant section over a certain length, which section then reduces sharply, down to a value at which the multi-capillaries become sufficiently flexible. The area of flexibility of the multi-capillaries has a length sufficient for the transportation of hydrogen to a fuel element. In this way, a flexible multi-capillary gas pipeline is created, which pipeline is integrated with a volume of stored hydrogen, the function of which pipeline is to supply hydrogen to the fuel element. The technical result consists of the provision of rapid priming of a micro-capillary vessel with high pressure gas and the regulated release of the gas from the vessel into a collector, where a moderate pressure (<1 MPa), required for operation of the fuel element, is maintained.

Claims

1. Multicapillary gas storage system, including a bundle of micro-capillaries, closed at one end, characterized in that the microcapillaries are sealed with metal plugs, the space between the microcapillaries is filled with polymer material, and the microcapillaries themselves are cylindrical in shape and have a constant cross-section at closed ends, which then decreases closer to the open ends to the value at which the microcapillaries become flexible to form a flexible gas pipeline.

2. Multi-capillary gas storage system, including a bundle of microcapillaries, closed at one end, characterized in that the microcapillaries are sealed with metal plugs, microcapillaries are made in the form of hexagonal prisms with common faces, while for the extreme microcapillaries of the beam, their parts facing outward of the beam are cylindrical, with the capillaries having a constant cross-section near the closed ends, which then decreases closer to the open ends to the value at which microcapillaries become flexible to form a flexible gas pipeline.

3. The multicapillary structure as claimed in claim 1, wherein the microcapillaries are made of glass, or of quartz, or of basalt.

4. The multicapillary structure as claimed in claim 2, wherein the microcapillaries are made of glass, or of quartz, or of basalt.

5. The multicapillary structure as claimed in claim 1, wherein a metal alloy having a low melting point and high adhesion.sub.i to the material of microcapillaries is chosen as the material of the metal plugs.

6. The multicapillary structure as claimed in claim 2, wherein the metal alloy having a low melting point is chosen as the material of the metal plugs with high adhesion to micro-capillary material.

7. The multicapillary structure as claimed in claim 5, wherein indium-tin alloy is chosen as the material of the plugs.

8. The multicapillary structure as claimed in claim 6, wherein indium-tin alloy is chosen as the material of the plugs.

9. The multicapillary structure as claimed in claim 1, wherein the length of the tube L is determined by the formula: $L>\frac{P*r}{2*k}$ where r is the internal diameter of the capillary, k is the adhesion force of the alloy with a unit of the glass surface, and P is the required gas pressure inside the capillary.

10. The multicapillary structure as claimed in claim 2, wherein the length of the tube L is determined by the formula: $L>\frac{P*r}{2*k}$ where r is the internal diameter of the capillary, k is the adhesion force of the alloy with a unit of the glass surface, and P is the required gas pressure inside the capillary.

11. The multicapillary structure as claimed in claim 1, wherein the ratio of the wall thickness to the radius of the microcapillaries at any capillary cross section should be from 0.1% to 10%.

12. The multicapillary structure as claimed in claim 2, wherein the ratio of the wall thickness to the radius of the microcapillaries at any capillary cross section should be from 0.1% to 10%.

13. The multicapillary structure as claimed in claim 11, wherein the ratio is wall thickness to the radius of microcapillaries at any capillary cross section should be from 0.1% to 2%.

14. The multicapillary structure as claimed in claim 12, wherein the ratio of the wall thickness to the radius of the microcapillaries at any capillary cross section should be from 0.1% to 2%.

15. The multicapillary structure as claimed in claim 1, characterized in that epoxy resin or epoxy glue is used as polymer material.

16. The multi-capillary structure as claimed in claim 2, characterized in that epoxy resin or epoxy glue is used as polymer material.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0029] FIG. 1the cross section of the structure of densely packed cylindrical glass micro-capillaries within the gas storage area.

[0030] FIG. 2view of the structure of tightly welded hexagonal prismatic (hexagonal) capillaries from the closed ends of the capillaries.

[0031] FIG. 3the form of a multi-capillary structure in which the gas storage area goes into a flexible multi-capillary gas pipeline.

[0032] FIG. 4one of the possible schemes for combining multi-capillary structures into a single gas storage of arbitrary shape.

[0033] FIG. 5possible structure of a multi-capillary gas cable. In the drawings, the numbers denote the following elements:

[0034] 1. Micro-capillaries [0035] 2. Plastic material [0036] 3. Capillary plugs [0037] 4. Outer surfaces of the capillaries [0038] 5. Multi-capillary blocks [0039] 6. Parts of the gas pipeline [0040] 7. Gas pipeline [0041] 8. Pressure reducer [0042] 9. Buffer volume for hydrogen at reduced pressure [0043] 10. Fuel cells [0044] 11. Multi-capillary pipeline carrier [0045] 12. Polyethylene sheath [0046] 13. Winding of Kevlar or carbon fiber [0047] 14. Shockproof pipeline sheath

DESCRIPTION OF NON-LIMITING EMBODIMENTS

[0048] FIG. 1 shows the schematic cross section of the first embodiment multi-capillary unit for the storage and transportation of hydrogen to the fuel cell. The structure consists of a set of identical cylindrical thin-wall glass micro-capillaries (1), tightly packed into a hexagonal or other matrix, closed from the ends with metal plugs (3) with sufficiently low melting point of the metal, having sufficiently good adhesion to glass and chemical resistance to hydrogen, such as indium-tin alloy In50Sn. After cooling the melt inside the capillaries below the melting point, a solid metal plug (3) is formed. The length of the plug L is determined from the condition of exceeding the adhesive force of the plug with the inner surface of the capillary above the force that pushes the plug out if the capillary is filled with gas with pressure P.

[0049] According to calculations, the length of the tube L must satisfy the condition:

L>Pr/(2k)

Here r is the internal diameter of the capillary, k is the adhesion force of the alloy with a unit of the glass surface.

[0050] The material of the capillaries (1) can be various types of glass, quartz or basalt. Multi-capillaries can be drawn from the corresponding preforms by softening them at elevated temperatures without subsequent crystallization. To minimize the probability of occurrence of nanometer-size cracks with a critical depth on the surface of micro-capillaries their wall thickness should preferably be less than 10 microns, more preferably less than 2 microns.

[0051] To minimize the weight of the micro-capillary system, the ratio of the wall thickness to the radius of the micro-capillaries should preferably be from 0.1% to 10%, more preferably from 0.1% to 2%.

[0052] The space between micro-capillaries (1) is filled with plastic material (2), for example, epoxy glue, epoxy resin (for example, glue Colltech CT 1010), the liquid monomer phase of which has a low enough viscosity and is able to easily fill the space inside and between the micro-capillaries. It should be noted that other glue with similar characteristics can be used as well. Since the lifting height of the monomer (the liquid phase of the plastic material) due to capillary forces is inversely proportional to the diameter of the channel, the monomer penetrates into the inter-capillary space to a depth greater than that for the capillary themselves.

[0053] The polymerization of the monomeric phase of the adhesive occurs under the influence of ultraviolet radiation or heat. After the polymerization, the closed ends of the capillaries must be cut staying the inter-capillary space closed. Filling the inter-capillary space with a plastic material (2) provides a monolithic structure, prevents the diffusion of hydrogen through the walls of capillaries into the environment and increases the strength of capillaries due to the covering of possible nanometer-size cracks on the outer surface of capillaries. To create the plugs (3) the open ends of the micro-capillaries are immersed into the melted metal alloy and some rarefaction inside the capillaries is created with a pump.

[0054] The second embodiment is shown schematically in FIG. 2. In this case internal micro-capillaries (1) have the shape of hexagonal prisms with common faces, forming a honeycomb structure in cross section, and the outer micro-capillaries have a special shape, where instead of flat faces they have cylindrical faces (4) on the outer surface and therefore do not experience bending deformation when the structure is under the internal gas pressure that may be critical for the glass strength. The corresponding shape of the outer capillaries can be obtained, for example, from flat edges, if the multi-capillary structure of fully hexagonal prisms is first soldered at both ends and then heated. Arising internal pressure due to the air expansion inside the capillaries deforms the faces of the outer capillaries as necessary, if the viscosity of glass is low enough. To create the plugs (3), the initially open end of the micro-capillaries is immersed in the melted metal alloy and some rarefaction inside the capillaries is created using a pump.

[0055] A general view of the hexagonal multi-capillary block is shown schematically in FIG. 3. Multi-capillary block (5) may contain from several tens to several hundred thousand micro-capillaries (1) and have a cross-sectional area in the gas storage area from several square millimeters to several tens of square centimeters. The shape of the block is not limited to the hexagon and may have a different geometric shape, for example, the shape of a parallelepiped or another shape, allowing the subsequent close packing of blocks in a micro-capillary system. In the area of gas transportation (6), the transverse dimensions of the block should provide sufficient flexibility for multi-capillaries (1), preferably these are transverse dimensions below 300 microns. The flexible ends of the micro-capillary block (5) can be obtained, for example, by heating multi-capillaries (1) to a temperature when the viscosity is glass is reduced to a value at which the waist of the block becomes possible. Such a procedure is used, for example, when creating glass multi-capillary structures with a variable cross section for X-ray optics in TOSS LLC (http://www.tegs.ru/?p=261). When hauling, the internal structure of the multi-capillary (1) is scaled to a smaller size, preserving its geometry.

[0056] A micro-capillary system for mobile storage of fuel gases and their transportation to fuel cells is schematically shown in FIG. 4. Such a system can be obtained by sintering or gluing (or another similar operation) several blocks (5) into a structure of arbitrary shape, while the flexible ends (6) of multi-capillaries are combined into a multi-capillary cable (7). Cable end (7) is connected, for example, with epoxy glue to the inlet of a control valve of high pressure (pressure regulator) (8). The output of the gearbox (8) is connected to the buffer volume (collector) (9), where the gas pressure is maintained at the level required for normal operation of the fuel cell (10). For example, if the hydrogen pressure in the micro-capillary system can reach 100 MPa, then in the buffer volume it should be reduced to 0.1-0.5 MPa. As a reducer (8), any known high-pressure valve can be used, for example, the well-known BuTech 316SS valve, designed to work with hydrogen at an inlet pressure of up to 100 MPa.

[0057] The cross-section of the multi-capillary pipeline is illustrated schematically in FIG. 5. The multi-capillary pipeline (7) may have a supporting cable made of fiberglass or metal (11), preferably covered with a polyethylene sheath (12), which serves to center individual gas pipelines (6), impart mechanical rigidity to the cable (7) and to secure the cable in the coupling gearbox (8). The cable may be covered with a layer of aramid or carbon filaments (13) and/or a soft sheath (14), for example, from polyurethane foam, to protect against accidental external damage during its installation from multi-capillary blocks to the buffer volume.

INDUSTRIAL APPLICABILITY

[0058] The invention can be implemented on the basis of the present description. Everything the necessary means and methods are disclosed in the description or are known to the person skilled in the art.

[0059] It should also be understood that the graphics presented in this application are for illustrative purposes only and are not intended in order to be limiting. It should be noted that the drawings illustrating various examples of the device according to the present invention are given for clarity without respecting the scale and proportions. It should also be noted that the blocks and other elements in these figures are exclusively functional units, so that the functional relationships between by these units, and not by any physical connections and/or physical interactions. You can add that the invention can be implemented in the framework of the claimed formula and other options other than those described which would be obvious to a person skilled in this technical field.