HYDROGEN STORAGE TANK WITH LEAK MANAGEMENT FUNCTIONALITY
20220228713 · 2022-07-21
Assignee
Inventors
Cpc classification
F17C2203/0604
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/042
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/066
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/054
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0663
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C1/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0621
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0109
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/056
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2250/0443
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2227/0157
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0189
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H01M2250/20
ELECTRICITY
F17C1/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0184
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/038
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0178
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0624
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F17C1/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C13/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A hydrogen storage tank has a composite laminate wall, a hydrogen-porous layer in contact with the outer surface of the composite laminate wall and a hydrogen-non-porous layer in contact with the outer surface of the hydrogen-porous layer, the hydrogen-non-porous layer having an output port for venting hydrogen which passes through the composite laminate wall and the hydrogen-porous layer from the interior of the tank. The tank allows hydrogen which leaks through the composite laminate wall to be collected and re-used. The invention also allows for the rate of hydrogen leakage from the tank to be measured, providing a measure of the structural integrity of the tank.
Claims
1. A hydrogen storage tank having a composite laminate wall, a hydrogen-porous layer in contact with the outer surface of the composite laminate wall and a hydrogen-non-porous layer in contact with the outer surface of the hydrogen-porous layer, the hydrogen-non-porous layer having an output port for venting hydrogen which passes through the composite laminate wall and the hydrogen-porous layer from the interior of the tank.
2. A hydrogen storage tank according to claim 1, wherein the hydrogen-porous layer comprises open-cell foam or consists of an open-cell foam layer.
3. A hydrogen storage tank according to claim 1, wherein the hydrogen-porous layer is a layer of fibrous material.
4. A hydrogen storage tank according to claim 1, wherein the hydrogen-non-porous layer is a rubber-based or polymeric layer.
5. A hydrogen storage tank according to claim 1, wherein the hydrogen-non-porous layer is a closed-cell foam layer.
6. A hydrogen storage tank according to claim 1, wherein the hydrogen-non-porous layer is separable from the hydrogen-porous layer and replaceable.
7. A hydrogen storage tank according to claim 1, wherein the hydrogen-porous layer is permanently mechanically deformable.
8. A hydrogen storage tank according to claim 1, the tank being generally cylindrical and comprising a plurality of impact-protecting ribs on the exterior of the tank, the ribs extending azimuthally and/or longitudinally with respect to the central longitudinal axis of the tank.
9. A hydrogen storage tank according to claim 8, wherein the ribs are integral with the hydrogen-non-porous layer.
10. A hydrogen storage tank according to claim 8, wherein the ribs are applied to the exterior of the tank.
11. Apparatus comprising a hydrogen storage tank according to claim 1, and a measuring system for measuring the flow rate of hydrogen passing through the output port of the hydrogen storage tank.
12. Apparatus comprising a hydrogen storage tank according to claim 1, a hydrogen-fueled fuel cell or a hydrogen-fueled gas turbine engine and a conveying system arranged to convey hydrogen from the output port of the tank to the fuel cell or gas turbine engine.
13. Apparatus according to claim 12, comprising means for measuring the flow rate of hydrogen within the conveying system.
14. Apparatus according to claim 12, further comprising a compressor arranged to compress hydrogen within the conveying system prior to delivery of the hydrogen to the fuel cell or gas turbine engine.
15. An aircraft comprising a hydrogen storage tank according to claim 1.
16. An aircraft comprising apparatus according to claim 12.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Examples are described below with reference to the accompanying drawings in which:
[0014]
[0015]
[0016]
DETAILED DESCRIPTION
[0017] Referring to
[0018] The conduit 109 may be connected by a conveying system to a second hydrogen storage tank for collection of hydrogen which has leaked from storage volume 120 of the tank 100. Alternatively, the conveying system may transfer hydrogen which has leaked from the tank 100 to a PEM fuel cell or a hydrogen-burning gas turbine engine. The conveying system may include a flow meter for measuring the rate at which hydrogen leaks from the tank 100. Where the conveying means is arranged to transport hydrogen from the conduit 109 to a fuel-cell or gas turbine engine, a compressor may be used increase the pressure of the hydrogen prior to its input to the fuel-cell or gas turbine engine. Measurements over time of the flow rate of hydrogen leaking from the internal storage volume 120 of the tank 100 through the output port 108 may be used to detect degradation of the composite laminate wall 114, for example by micro-cracking or de-lamination. A high rate of leakage compared to the rate of leakage when the tank 100 is first brought into service, or a sudden increase in the rate of leakage, may indicate imminent failure of the tank 100, allowing for its timely replacement.
[0019] The hydrogen storage tank 100 is a so-called ‘Type IV’ tank due to the presence of the polymer liner 112, however in a variant tank the liner 112 may be omitted so that the variant tank is a so-called ‘Type V’ tank.
[0020] The hydrogen-porous layer 110 may be an open-cell foam layer or may comprise open-cell foam. Preferably the layer 104 is permanently mechanically deformable, allowing impacts experienced by the tank 100 to be recorded. The mechanical integrity of the tank 100 may be inferred at least in part from a history of impacts experienced by the tank 100. Alternatively, the hydrogen-porous layer 110 may be a layer of fibrous material.
[0021] The hydrogen-non-porous layer 104 may be a flexible rubber-based or polymeric layer, since the layer 104 is only required to contain leaked hydrogen at approximately atmospheric pressure rather than at the pressure within the internal storage volume 120 of the tank 100. The hydrogen-non-porous layer 104 may alternatively be a layer of closed-cell foam material.
[0022] The hydrogen-non-porous layer 104 may be separable from the hydrogen-porous layer 110 and replaceable since it is the outer layer of the tank 100. The layer 104 can be tested to ensure its gas-tightness by applying a small positive pressure to the port 108 and monitoring its decay over time.
[0023]
[0024] In other variants of the second example tank, azimuthal and/or longitudinal ribs may be applied to the outer surface of the hydrogen-non-porous layer rather than being formed integrally with it.