BULK METALLIC GLASS PRESSURE VESSELS
20200300413 ยท 2020-09-24
Inventors
- John CHAY (Hamden, CT, US)
- Jan SCHROERS (Guilford, CT, US)
- Jason Sagaci (Stratford, CT, US)
- Jittisa Ketkaew (North Branford, CT, US)
- Evgenia PEKARSKAYA (New York, NY, US)
Cpc classification
F17C2203/0604
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0131
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/036
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2221/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2260/012
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C22F1/00
CHEMISTRY; METALLURGY
C22C45/10
CHEMISTRY; METALLURGY
F17C2203/0636
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0648
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
F17C2270/0197
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0194
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0128
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/033
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0189
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2203/0675
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/058
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C22C45/04
CHEMISTRY; METALLURGY
F17C2209/2127
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2209/232
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2201/0185
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0161
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2270/0178
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
C22C45/003
CHEMISTRY; METALLURGY
B21D51/24
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A pressure vessel containing a main body with at least one opening. The pressure vessel is made from a BMG material. The pressure vessel may contain an additional part such as a neck, a liner, a rib, a lattice, a fin, and a diaphragm. The pressure vessel may be free of a welded joint in entirety. The pressure vessel may contain multiple parts in the main body, each of which is free of a welded joint. The pressure vessel may be made through thermoplastic forming.
Claims
1. A pressure vessel, the pressure vessel comprising: a main body with at least one opening, wherein the main body is made from a BMG material, and wherein the pressure vessel is capable of receiving a pressurized fluid or gas.
2. The pressure vessel of claim 1, wherein the pressure vessel is made through thermoplastic forming such that the pressure vessel is seamless in entirety.
3. The pressure vessel of claim 2, wherein the thermoplastic forming temperature is below 700 C.
4. The pressure vessel of claim 1, wherein the internal stress within the pressure vessel is less than 20% of the material's yield strength.
5. The pressure vessel of claim 1, wherein the pressure vessel has an inherent ductile state greater than the critical fictive temperature (T.sub.f>T.sub.f.sup.c).
6. The pressure vessel of claim 1, wherein the pressure vessel has a crystallinity less than 10%.
7. The pressure vessel of claim 1, wherein the pressure vessel has a Young's modulus greater than 10 GPa and a yield strength greater than 1200 MPa.
8. The pressure vessel of claim 1, wherein the pressure vessel has one or more rotational symmetry along a single axis.
9. The pressure vessel of claim 1, wherein the pressure vessel has a spherical shape and a ratio of a diameter of the spherical shape to a corresponding wall thickness of the main body is between 10 and 10,000.
10. The pressure vessel of claim 1, wherein the pressure vessel has a cylindrical shape with a length-to-width ratio between 0.5 and 30.
11. The pressure vessel of claim 1, wherein the main body has the thinnest part and the thickest part, wherein the thickness of the thinnest part is no more than a of the thickness of the thickest part.
12. The pressure vessel of claim 1, wherein the wall thickness of the main body is non-uniform.
13. The pressure vessel of claim 1, wherein the wall thickness of the main body is uniform.
14. The pressure vessel of claim 1, wherein the pressure vessel further comprises a rib, a lattice, and/or a fin structure on an outside surface of the main body to enhance a burst strength of the pressure vessel and/or to reduce the overall weight of the pressure vessel.
15. The pressure vessel of claim 1, wherein the pressure vessel has a thin wall thickness such that a supporting outside shell is required to withstand the pressure.
16. The pressure vessel of claim 1, wherein the pressure vessel is configured to act as a support for an insert which is in contact with a pressurized medium.
17. The pressure vessel of claim 1, wherein the pressure vessel is a satellite tank.
18. The pressure vessel of claim 1, wherein the pressure vessel is an aircraft tank.
19. The pressure vessel of claim 1, wherein the pressure vessel is a satellite tank and further comprises a diaphragm.
20. The pressure vessel of claim 17, wherein the pressure vessel has an exterior design that resembles the overall geometry of the satellite to utilize an open space of the satellite.
21. The pressure vessel of claim 1, wherein the pressure vessel is a fuel tank for vehicles including automobiles or aircrafts.
22. The pressure vessel of claim 1, wherein the pressure vessel is a gas tank for vehicles including automobiles or aircrafts.
23. The pressure vessel of claim 1, wherein the pressure vessel is a submarine vessel.
24. The pressure vessel of claim 1, wherein the pressure vessel is a pressure chemical reactor vessel.
25. The pressure vessel of claim 1, wherein the BMG material comprises, as a constituent element, one or more of: Zr, Ti, Ni, Pd, Mg, Al, La, Ce, Fe, Pt, Nb, Ir, Mo, W, Cu, Au, Ag, Hf, Co, Gd, Be, B, C, P, Si, and Rh.
26. The pressure vessel of claim 1, wherein the BMG material is one of: Zr.sub.44Ti.sub.11Cu.sub.10Ni.sub.10Be.sub.25, Zr.sub.41Ti.sub.14Cu.sub.12.5Ni.sub.10Be.sub.22.5, Zr.sub.35Ti.sub.30Cu.sub.7.5Be.sub.27.5, Zr.sub.46Cu.sub.46Be.sub.8, Zr.sub.57Nb.sub.5Cu.sub.15.4Ni.sub.12.6Al.sub.10, Zr.sub.65Al.sub.10Ni.sub.10Cu.sub.15, Zr.sub.65Al.sub.7.5Ni.sub.10Cu.sub.12.5Ag.sub.5, Zr.sub.66.4Nb.sub.6.4Cu.sub.10.5Ni.sub.8.7Al.sub.8, Zr.sub.55Cu.sub.30Al.sub.10Ni.sub.5, Zr.sub.46Cu.sub.46Be.sub.8, Ti.sub.41Zr.sub.25Be.sub.28Fe.sub.6, Ti.sub.45Zr.sub.20Be.sub.29Fe.sub.6, Ti.sub.35Zr.sub.30Be.sub.25, Ti.sub.30Zr.sub.35Be.sub.25, Ti.sub.40Zr.sub.10Cu.sub.34Pd.sub.14Sn.sub.2, Ti.sub.40Zr.sub.10Cu.sub.32Pd.sub.14Sn.sub.4, Pd.sub.43Cu.sub.27Ni.sub.10P.sub.20, Pd.sub.40Ni.sub.10Cu.sub.30P.sub.20, Pd.sub.40Ni.sub.40P.sub.20, Pt.sub.57.5Ni.sub.14.7Cu.sub.5.3P.sub.22.5, Au.sub.49Ag.sub.5.5Pd.sub.2.3Cu.sub.26.9Si.sub.16.3, Ni.sub.45Pd.sub.35P.sub.17B.sub.3, Ni.sub.45Ti.sub.20Zr.sub.25Al.sub.10, Ni.sub.40Ti.sub.17Zr.sub.28Al.sub.10Cu.sub.5, Ni.sub.62Pd.sub.19Si.sub.2P.sub.17, Cu.sub.46Zr.sub.42Al.sub.7Y.sub.5, Mg.sub.65Cu.sub.25Y.sub.10, Mg.sub.65Cu.sub.7.5Ni.sub.7.5Zn.sub.5Ag.sub.5Y.sub.10, La.sub.55Al.sub.25Co.sub.5Cu.sub.10Ni.sub.5, Fe.sub.41Co.sub.7Cr.sub.15Mo.sub.14C.sub.15B.sub.6Y.sub.2, and a mixture thereof.
27. A diaphragm, wherein the diaphragm is made of a BMG material, and wherein the diaphragm is capable of operating in a pressure vessel.
28. The diaphragm of claim 27, wherein the crystallinity of the diaphragm is less than 10%.
29. The diaphragm of claim 27, wherein the diaphragm has a Young's modulus greater than 10 GPa, an elasticity greater than 1%, and a yield strength greater than 1200 MPa.
30. The diaphragm of claim 27, wherein the diaphragm is capable of deforming elastically.
31. The diaphragm of claim 27, wherein the diaphragm is made through thermoplastic forming at a forming temperature below 700 C.
32. The diaphragm of claim 27, wherein the diaphragm operates under the elastic strain region where the material exhibits a strain of less than 2%.
33. The diaphragm of claim 27, wherein the diaphragm has an inherent ductile state greater than the critical fictive temperature (T.sub.f>T.sub.f.sup.c).
34. The diaphragm of claim 27, wherein the inherent ductile state of the diaphragm (T.sub.f>T.sub.f.sup.c) of the glass is realized.
35. The diaphragm of claim 27, wherein the BMG material comprises, as a constituent element, one or more of: Zr, Ti, Ni, Pd, Mg, Al, La, Ce, Fe, Pt, Nb, Ir, Mo, W, Cu, Au, Ag, Hf, Co, Gd, Be, B, C, P, Si and Rh.
36. The diaphragm of claim 27, wherein the BMG material is one of: Zr.sub.44Ti.sub.11Cu.sub.10Ni.sub.10Be.sub.25, Zr.sub.41Ti.sub.14Cu.sub.12.5Ni.sub.10Be.sub.22.5, Zr.sub.35Ti.sub.30Cu.sub.7.5Be.sub.27.5, Zr.sub.46Cu.sub.46Be.sub.8, Zr.sub.57Nb.sub.5Cu.sub.15.4Ni.sub.12.6Al.sub.10, Zr.sub.65Al.sub.10Ni.sub.10Cu.sub.15, Zr.sub.65Al.sub.7.5Ni.sub.10Cu.sub.12.5Ag.sub.5, Zr.sub.66.4Nb.sub.6.4Cu.sub.10.5Ni.sub.8.7Al.sub.8, Zr.sub.55Cu.sub.30Al.sub.10Ni.sub.5, Zr.sub.46Cu.sub.46Be.sub.8, Ti.sub.41Zr.sub.25Be.sub.28Fe.sub.6, Ti.sub.45Zr.sub.20Be.sub.29Fe.sub.6, Ti.sub.35Zr.sub.30Be.sub.25, Ti.sub.30Zr.sub.35Be.sub.25, Ti.sub.40Zr.sub.10Cu.sub.34Pd.sub.14Sn.sub.2, Ti.sub.40Zr.sub.10Cu.sub.32Pd.sub.14Sn.sub.4, Pd.sub.43Cu.sub.27Ni.sub.10P.sub.20, Pd.sub.40Ni.sub.10Cu.sub.30P.sub.20, Pd.sub.40Ni.sub.40P.sub.20, Pt.sub.57.5Ni.sub.14.7Cu.sub.5.3P.sub.22.5, Au.sub.49Ag.sub.5.5Pd.sub.2.3Cu.sub.26.9Si.sub.16.3, Ni.sub.45Pd.sub.35P.sub.17B.sub.3, Ni.sub.45Ti.sub.20Zr.sub.25Al.sub.10, Ni.sub.40Ti.sub.17Zr.sub.28Al.sub.10Cu.sub.5, Ni.sub.62Pd.sub.19Si.sub.2P.sub.17, Cu.sub.46Zr.sub.42Al.sub.7Y.sub.5, Mg.sub.65Cu.sub.25Y.sub.10, Mg.sub.65Cu.sub.7.5Ni.sub.7.5Zn.sub.5Ag.sub.5Y.sub.10, La.sub.55Al.sub.25Co.sub.5Cu.sub.10Ni.sub.5, Fe.sub.41Co.sub.7Cr.sub.15Mo.sub.14C.sub.15B.sub.6Y.sub.2, and a mixture thereof.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0019]
[0020]
[0021]
[0022]
[0023]
[0024]
DETAILED DESCRIPTION OF THE INVENTION
[0025] This invention relates to BMG pressure vessels, comprising a main body with at least one opening. The BMG pressure vessel may comprise an additional part such as a neck, a liner, a rib, a lattice, a fin, and a diaphragm. The BMG pressure vessel may be a one-piece, free of a welded joint in entirety. The BMG pressure vessel may contain multiple parts in the main body, each of which is free of a welded joint.
[0026] The BMG pressure vessel may be produced through the thermoplastic forming (TPF) process. The BMG pressure vessel may be a hollow walled vessel, essentially free of a welded joint in contrast to a conventional metal pressure vessel which contains a welded joint with the weld area that is comparable to the circumference of the pressure vessel. The BMG pressure vessel of present invention has one or more openings and can contain pressurized fluid or gas. The BMG pressure vessel can be formed through a TPF process in the BMG's supercooled liquid state, and, as a result, the BMG pressure vessel has a crystallinity of less than 10%. It has been known in the art that a material with crystallinity exceeding 10% suffers from properties deterioration, especially mechanically. Ketkaew, J., Liu, Z., Chen, W., & Schroers, J. (2015), Critical Crystallization for Embrittlement in Metallic Glasses, Physical Review Letters, 115(26), 265502 (Ketkaew et al., 2015). A critical capability offered by the present invention is that the TPF-based BMG pressure vessel is completely or essentially seamless and stress-free, has a uniform and consistent properties, and has a homogeneous glass state throughout the entire piece.
[0027]
[0028]
[0029]
[0030]
[0031] The diaphragm may be made from a set of BMG layer/diaphragm layer/BMG layer. The diaphragm operates under the elastic strain region where the material exhibits a strain of less than 2%. The diaphragm layer may be made of a BMG material. A diaphragm may be installed in any of the pressure vessels of the present invention.
[0032] The crystallinity of the diaphragm may be less than 10%. The diaphragm may have a Youngs modulus greater than 10 GPa, an elasticity greater than 1%, and a yield strength greater than 1200 MPa. The diaphragm may be capable of deforming elastically. The diaphragm may operate under the elastic strain region where the material exhibits a strain of less than 2%. The diaphragm may have an inherent ductile state greater than the critical fictive temperature (T.sub.f>T.sub.f.sup.c). The diaphragm may be made through thermoplastic forming such as blow molding at a forming temperature below 700 C.
[0033]
[0034] Conventional pressure vessels are constructed by welding, brazing, rolling, or joining of various pieces of a rigid material, usually metals, that is compatible with the fluid to be stored. These resulting seams act as the weak point of the pressure vessel, including a stress concentrationact as a point of origin for fracture, source of leakages, for example, hydrogen or other gases. For instance, U.S. Pat. No. 3,140,006A discusses the leakage due to the diffusion of hydrogen through metallurgical bonds, such as those formed by welding, brazing, or rolling ad used to construct the pressure vessel. Previous inventions in the art attempt to address this issue by overwrapping or implementing an inner liner, made of metal and non-metal composites or polymers, onto the pressure vessel. U.S. Pat. No. 6,401,963B1. However, none of the prior art has demonstrated an essentially seamless, free of a joint pressure vessel that is the origin of the leakage and weak point of the pressure vessel, which is disclosed here in the present invention.
[0035] The BMG pressure vessels of the present invention may be completely or essentially seamless, free of a welded joint. The BMG pressure vessel may be free of a welded joint in entirety. A main body may be welded to at least one neck. The main body and the at least one neck may be formed in a single forming step. The BMG pressure vessel may comprise or consist of multiple parts in the main body, each of which is free of a welded joint. A ratio of the diameter to the corresponding wall thickness may be between 10 and 10,000.
[0036] Referring to
[0037] In the step S1, a mold with a cavity and a BMG feedstock are separately provided. The shape of the cavity is selected according to the shape of the pressure vessel to be formed. The mold may be made of one or more of various materials such as brass, steel, stainless steel, and non-metal such as alumina.
[0038] In the step S2, the mold is heated up to a processing temperature which is in a supercooled liquid region between the glass transition temperature and the crystallization temperature of the BMG feedstock. The BMG feedstock is placed into the mold cavity, covering the opening of the mold cavity, before or after the mold temperature reaches the processing temperature.
[0039] In the step S3, after the temperature of the BMG feedstock reaches the processing temperature, which allows the BMG feedstock to become viscous and moldable, a pressure is applied to the BMG feedstock such that the BMG feedstock deforms toward the surface of the cavity. The BMG feedstock deforms until reaching the surface of the cavity and replicating the shape of the cavity. The duration of deforming the BMG feedstock, the processing temperature, and the applied pressure are pre-determined to control the thickness, the crystallinity, and other properties of the BMG pressure vessel to be formed. The applied pressure is selected to be larger than the flow stress of the BMG feedstock. The deformation duration is selected to be shorter than the amount of time that causes substantial crystallization such that the crystallinity of the BMG pressure vessel to be formed is minimized to be less than 10%.
[0040] In the step S4, once the BMG feedstock completely fills the cavity of the mold, the deformed BMG is cooled below its glass transition temperature to form a BMG pressure vessel.
[0041] In the step S5, the BMG pressure vessel is removed from the mold.
[0042] The above-descried method is one example of the methods of forming the BMG pressure vessels of the present invention.
[0043] In one embodiment, the processing temperature may be below 700 C., where the cooling rate variation within the pressure vessel is small, for example, less than 100K/s, and as a result of such small variation, the internal stresses within the pressure vessel are less than 10% of the yield strength in all locations within the pressure vessel, and the magnitude of the cooling rate warrants that the inherent ductile state, defined by the fictive temperature, is greater than the critical fictive temperature (T.sub.f>T.sub.f.sup.c) as defined and explained by Ketkaew et al., Ketkaew, et al., 2018, Mechanical glass transition revealed by the fracture toughness of metallic glasses, Nature Communications, 9(1), 1-7 (Ketkaew et al., 2018).
[0044] Furthermore, as additional consequences of the TPF process, the BMG pressure vessel has Young's modulus greater than 10 GPa and a yield strength greater than 1200 MPa, and the internal stress is reduced dramatically.
[0045] The BMG pressure vessels disclosed in the present invention may be made out of one or more of seamless pieces to form a seamless or essentially seamless vessel. Each of the multiple seamless pieces may be formed by a method similar to the above-described method. It is extremely challenging to create parts where the wall thickness is significantly smaller than the other dimensions, such as the diameter. Such structural characteristics of a pressure vessel can be achieved by the method of the present invention.
[0046] Embodiments of the present invention are not limited to a particular BMG composition. Any suitable BMG alloy composition can be utilized to form the BMG pressure vessel. A suitable alloy composition has one of the following constituent elements as a base element: Zr, Ti, Ni, Pd, Mg, Al, La, Ce, Fe, Pt, Nb, Ir, Mo, W, Cu, Au, Ag, Hf, Co, Gd, Be, B, C, P, Si, Rh, and a mixture thereof. For another example, a suitable BMG alloy composition is one of Zr.sub.44Ti.sub.11Cu.sub.10Ni.sub.10Be.sub.25, Zr.sub.41Ti.sub.14Cu.sub.12.5Ni.sub.10Be.sub.22.5, Zr.sub.35Ti.sub.30Cu.sub.7.5Be.sub.27.5, Zr.sub.46Cu.sub.46Be.sub.8, Zr.sub.57Nb.sub.5Cu.sub.15.4Ni.sub.12.6Al.sub.10, Zr.sub.65Al.sub.10Ni.sub.10Cu.sub.15, Zr.sub.65Al.sub.7.5Ni.sub.10Cu.sub.12.5Ag.sub.5, Zr.sub.66.4Nb.sub.6.4Cu.sub.10.5Ni.sub.8.7Al.sub.8, Zr.sub.55Cu.sub.30Al.sub.10Ni.sub.5, Zr.sub.46Cu.sub.46Be.sub.8, Ti.sub.41Zr.sub.25Be.sub.28Fe.sub.6, Ti.sub.45Zr.sub.20Be.sub.29Fe.sub.6, Ti.sub.35Zr.sub.30Be.sub.25, Ti.sub.30Zr.sub.35Be.sub.25, Ti.sub.40Zr.sub.10Cu.sub.34Pd.sub.14Sn.sub.2, Ti.sub.40Zr.sub.10Cu.sub.32Pd.sub.14Sn.sub.4, Pd.sub.43Cu.sub.27Ni.sub.10P.sub.20, Pd.sub.40Ni.sub.10Cu.sub.30P.sub.20, Pd.sub.40Ni.sub.40P.sub.20, Pt.sub.57.5Ni.sub.14.7Cu.sub.5.3P.sub.22.5, Au.sub.49Ag.sub.5.5Pd.sub.2.3Cu.sub.26.9Si.sub.16.3, Ni.sub.45Pd.sub.35P.sub.17B.sub.3, Ni.sub.45Ti.sub.20Zr.sub.25Al.sub.10, Ni.sub.40Ti.sub.17Zr.sub.28Al.sub.10Cu.sub.5, Ni.sub.62Pd.sub.19Si.sub.2P.sub.17, Cu.sub.46Zr.sub.42Al.sub.7Y.sub.5, Mg.sub.65Cu.sub.25Y.sub.10, Mg.sub.65Cu.sub.7.5Ni.sub.7.5Zn.sub.5Ag.sub.5Y.sub.10, La.sub.55Al.sub.25Co.sub.5Cu.sub.10Ni.sub.5, Fe.sub.41Co.sub.7Cr.sub.15Mo.sub.14C.sub.15B.sub.6Y.sub.2 and a mixture thereof.
[0047] The BMG pressure vessels of the present invention has a lightweight with high strength and is corrosion resistant. The BMG pressure vessels, especially ones that are processed through the TPF process, exhibit consistently high strength with very little scatter burst strength throughout the pressure vessel structure. The drastic reduction of stress concentrations in the BMG pressure vessel eliminates or significantly reduces stresses. Surprisingly, the present inventors found that, when using metallic glasses that are thermoplastically molded, the burst pressure is not only significantly higher, but also the variation in burst pressure is very low as compared to crystalline materials, allowing to operate these pressure vessels at a pressure much closer to the yield stress limit which translates into a lower required factor of safety. The present inventors contribute this result to the fact that all stresses were reduced from the fabrication during the thermoplastic forming.
[0048] The TPF methods of the present invention allow a BMG feedstock to be shaped seamlessly into a pressure vessel in a single process, free of welds and joints that serve as failure points. Multiple BMG deformed through TPF may be separately shaped seamlessly to be placed into a pressure vessel. In addition, the homogeneous and isotropic characteristics of the BMG materials yield high strength and superior corrosion-resistant properties.