Structural vehicle components for hydrogen storage
Vehicle structural components and additive manufacturing methods for forming the components are described. The structural components incorporate hydrogen storage materials for use in conjunction with hydrogen fuel cells in electric-powered vehicles such as unmanned aerial vehicles. The hydrogen storage materials can be in the form of a 3D printed metal foam that includes a metal hydride and an inert structural metal. The material can exhibit a very low weight density able to store hydrogen in a low pressure solid-state form at a high energy density. The structural components that carry the hydrogen storage materials can be exchangeable components of a vehicle, and the vehicle can be refueled by merely exchanging an exhausted component for a replacement component that is fully-charged with hydrogen.
1. A removably attachable structural component configured for attachment to a vehicle, the structural component comprising:
a) a metal foam, the metal foam comprising sintered particles, the sintered particles comprising first particles including a metal hydride and second particles comprising an inert scaffolding material;
b) a casing surrounding the metal foam;
c) a fluid line in fluid communication with the metal foam; and
d) an attachment device configured to retain the structural component in place during use and configured to release the structural component from the vehicle;
wherein the attachment device is configured such that upon the attachment and release, the metal foam is placed into and taken out of, respectively, fluid communication with a hydrogen fuel cell via the fluid line.
2. The structural component of claim 1 , wherein the inert scaffolding metal comprises aluminum.
3. The structural component of claim 1 , the casing comprising aluminum.
4. The structural component of claim 1 , the metal foam having a weight density of 3 g/cc or less and/or a power density of 0.5 W-h/g or more.
5. The structural component of claim 1 , wherein the first particles and the second particles are present in the metal foam as nano- or micro-scale particles.
6. A method for forming the structural component of claim 1 , the method comprising:
depositing a metal powder, the metal powder including the first particles and the second particles;
sintering the first and second particles of the metal powder to form the metal foam; and
surrounding the metal foam with the casing, the casing having a shape of a structural component of a vehicle or a portion thereof.
7. The structural component of claim 1 , the metal foam comprising the inert scaffolding metal in an amount of 5 wt. % to 25 wt. % of the metal foam.
8. The structural component of claim 1 , the metal foam defining a series of interconnected pores, the pores each having a pore size of from 40 micrometers to 500 micrometers.
9. The structural component of claim 1 , the metal foam having a porosity of 75% to 95%.
10. The structural component of claim 1 , the metal foam comprising the metal hydride in an amount from 65 wt. % to 95 wt. % of the metal foam.
11. The structural component of claim 1 , the attachment device comprising a mounting clip, an alignment pin, or a magnet.
12. The structural component of claim 1 , wherein the metal hydride comprises magnesium or a magnesium alloy.
13. The structural component of claim 12 , the metal foam further comprising third particles comprising an additive, the additive comprising palladium, titanium, titanium oxide, titanium fluoride, scandium, zirconium, nickel, cobalt, manganese, iron, vanadium, silicon, iron oxide, platinum, ruthenium, or any combination thereof.
14. The structural component of claim 13 , the metal foam comprising the additive in an amount of less than 10 wt. % of the metal foam.
15. An unmanned aerial vehicle comprising the structural component of claim 1 , the unmanned aerial vehicle further comprising:
a fluid connection between the fluid line that is in communication with the metal foam and the hydrogen fuel cell;
a motor in electrical communication with the hydrogen fuel cell; and
a control system configured to controllably release hydrogen from the metal hydride of the metal foam.
16. The unmanned aerial vehicle of claim 15 , the vehicle comprising a body, the body comprising the structural component.
17. The unmanned aerial vehicle of claim 15 , the vehicle comprising a landing gear, the landing gear comprising the structural component.
18. The unmanned aerial vehicle of claim 15 , the vehicle comprising a motor support, the motor support comprising the structural component.
19. The unmanned aerial vehicle of claim 15 , the vehicle comprising a rotor mount, the rotor mount comprising the structural component.