EP0570525A1 - Supraleitende verbindung - Google Patents
Supraleitende verbindungInfo
- Publication number
- EP0570525A1 EP0570525A1 EP19920907270 EP92907270A EP0570525A1 EP 0570525 A1 EP0570525 A1 EP 0570525A1 EP 19920907270 EP19920907270 EP 19920907270 EP 92907270 A EP92907270 A EP 92907270A EP 0570525 A1 EP0570525 A1 EP 0570525A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- powder
- superconducting
- superconductor
- composite
- precursor material
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 44
- 239000000843 powder Substances 0.000 claims abstract description 34
- 229920006397 acrylic thermoplastic Polymers 0.000 claims abstract description 11
- 239000002887 superconductor Substances 0.000 claims description 53
- 239000002245 particle Substances 0.000 claims description 28
- 239000000463 material Substances 0.000 claims description 21
- 239000010949 copper Substances 0.000 claims description 9
- 238000000034 method Methods 0.000 claims description 9
- 238000009826 distribution Methods 0.000 claims description 7
- 239000007787 solid Substances 0.000 claims description 6
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 238000003825 pressing Methods 0.000 claims description 2
- 239000002243 precursor Substances 0.000 claims 8
- BTGZYWWSOPEHMM-UHFFFAOYSA-N [O].[Cu].[Y].[Ba] Chemical group [O].[Cu].[Y].[Ba] BTGZYWWSOPEHMM-UHFFFAOYSA-N 0.000 claims 2
- 229910021521 yttrium barium copper oxide Inorganic materials 0.000 claims 2
- IQAKAOAPBMJSGJ-UHFFFAOYSA-N [Cu].[Y].[Ba] Chemical compound [Cu].[Y].[Ba] IQAKAOAPBMJSGJ-UHFFFAOYSA-N 0.000 claims 1
- 238000000137 annealing Methods 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 claims 1
- 238000002844 melting Methods 0.000 claims 1
- 230000008018 melting Effects 0.000 claims 1
- 238000002156 mixing Methods 0.000 claims 1
- 238000004781 supercooling Methods 0.000 claims 1
- 229920001169 thermoplastic Polymers 0.000 claims 1
- 239000004416 thermosoftening plastic Substances 0.000 claims 1
- 230000001131 transforming effect Effects 0.000 claims 1
- 239000011159 matrix material Substances 0.000 abstract description 7
- 230000004907 flux Effects 0.000 description 8
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 6
- 230000008859 change Effects 0.000 description 4
- 230000001965 increasing effect Effects 0.000 description 4
- 239000007788 liquid Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- 230000003993 interaction Effects 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 229910052761 rare earth metal Inorganic materials 0.000 description 2
- 150000002910 rare earth metals Chemical class 0.000 description 2
- 229910000938 samarium–cobalt magnet Inorganic materials 0.000 description 2
- VVQNEPGJFQJSBK-UHFFFAOYSA-N Methyl methacrylate Chemical compound COC(=O)C(C)=C VVQNEPGJFQJSBK-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000013590 bulk material Substances 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 239000012700 ceramic precursor Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 238000007873 sieving Methods 0.000 description 1
- 238000010583 slow cooling Methods 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/04—Bearings not otherwise provided for using magnetic or electric supporting means
- F16C32/0406—Magnetic bearings
- F16C32/0408—Passive magnetic bearings
- F16C32/0436—Passive magnetic bearings with a conductor on one part movable with respect to a magnetic field, e.g. a body of copper on one part and a permanent magnet on the other part
- F16C32/0438—Passive magnetic bearings with a conductor on one part movable with respect to a magnetic field, e.g. a body of copper on one part and a permanent magnet on the other part with a superconducting body, e.g. a body made of high temperature superconducting material such as YBaCuO
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N60/00—Superconducting devices
- H10N60/80—Constructional details
- H10N60/85—Superconducting active materials
- H10N60/855—Ceramic superconductors
- H10N60/857—Ceramic superconductors comprising copper oxide
Definitions
- This invention relates to superconducting composites and superconducting bearings using such composites.
- Superconducting bearings can be constructed from such superconducting composites.
- Gyorgi et al. U.S. Patent No. 4,797,386 discloses a journal bearing having a cylindrical magnet, magnetized axially and disposed within a hollow cylinder made of superconducting material.
- Agarwala U.S. Patent No. 4,892,863 discloses a thrust bearing having a superconductor disk and a rotating permanent magnet coaxially above it. A Type II superconducting material is preferred for the disk.
- a superconducting composite comprises a superconductor powder and an acrylic thermoplastic blended between 1:1 and 3:1 by volume.
- the optimum volume of superconductor powder is between fifty five percent and sixty percent.
- This composite can be machined into a hollow cylinder for a journal bearing, or it can be machined into a disk for a thrust bearing.
- Fig. 1 is a flowchart of a method for formulating the superconducting composite of the present invention
- Fig. 2 is a plot of particle size versus bearing load capacity
- Fig. 3 is a plot of volume percentage of superconductor in the composite versus bearing load capacity
- Figs. 4 and 5 are perspective views of thrust and journal bearings fabricated from the superconducting composite described in connection with Fig. 1;
- Figs. 6 and 7 are plots of radial and axial load capacities for the thrust bearing shown in Fig. 4.
- a superconducting ceramic precursor material such as YBa_Cu 3 o 7 __. powder
- YBa_Cu 3 o 7 __. powder is first melted at temperatures in the range 1300°C to 1400°C for 5-10 minutes.
- the melt is then rapidly quenched to solidify the material in a homogeneous subatomic lattice. This may best be accomplished by pouring the melted material over copper plates that are cooled to liquid nitrogen temperatures (77°K).
- the quenched YBa_Cu 3 0 7 __- material is a black, brittle amorphous solid. This solid is then vacuum dried to remove any moisture that has condensed on the surface.
- the amorphous solid is ground to a fine powder with an average particle size which is preferably not greater than 175 microns.
- the fine powder is then pressed into bulk shapes such as disks or cylinders.
- the bulk shapes are melt textured in a heat treating process.
- the bulk shape is melted into a liquid; then the liquid is cooled slowly.
- This slow cooling promotes the growth of relatively long grains, i.e., grains having a length greater than 1 mm.
- This process can also be adapted to promote the growth of uniformly sized grains having any desired length up to slightly greater than 1cm.
- an optimal grain size which can be then ground to a preferred particle size, such as 700 microns, can be obtained by a adjusting the combination of initial melt temperature and cooling rate factors.
- the melt textured solid superconductor is then ground to a fine powder, having a particle size distribution between 20 microns and 1 mm in size.
- the optimal size of the resulting ground particles is believed to be in the range of between 600 to 800 microns.
- the superconductor powder is then sized by sieving through gradated screens.
- the heat treated and sized superconductor powder is next annealed in a second heat treatment carried out in an oxygen atmosphere. It is preferred to anneal the sized powder, as opposed to the bulk textured material, because of the higher surface area of the ground powder.
- the sized, annealed superconductor powder is subsequently mixed with a polymer such as an acrylic thermoplastic in the ratios 1:1 to 3:1.
- the sized superconducting powders may be selected to have an approximately uniform particle size, or alternatively, a selected gradation, combination, or distribution of particle sizes may be optimal.
- the acrylic thermoplastic such as methyl methacrylate
- the superconductor-acrylic composite mixture is ball milled with zirconia balls for 5 to 20 minutes to promote uniform wetting of the superconductor particles and insure a homogeneous distribution of acrylic and superconductor.
- the mixture is placed or injected into a mold of a press, and compacted under approximately 28kN of pressure at a temperature of about 180°C for approximately nine minutes.
- the sample is allowed to cool for three minutes and is then removed from the press.
- the result is a two-phase composite structure that combines the flux-pinning properties of the superconductor with the toughness and flexibility of a polymeric material.
- the composite will not exhibit the zero resistance to electrical current property of a pure superconductor.
- Fig. 2 is a plot of particle size on the X-axis and bearing load capacity on the Y-axis for the YBa_.Cu 3 0 7 superconductor composite described above.
- the data for the graph was generated using 70% by volume of superconductor and 30% by volume acrylic thermoplastic.
- the graph suggests an increased load capacity as a function of particle size occurs when the particle size increases, particularly for particle sizes in the range of between about 600 and 800 microns.
- Fig. 3 is a plot of volume percentage of YBa 2 Cu 3 0 7 superconductor in the composite on the
- the X-axis and bearing load capacity on the Y-axis for the superconductor composite described above were generated using a mean particle size of 425 microns.
- the graph indicates that the bearing load capacity increases as the volume percentage of superconductor material is increased to between fifty five to sixty percent. Surprisingly however, the bearing load capacity actually decreases when the percentage of superconductor material is further increased.
- the preferred volume percentage of superconductor is in the range of between about fifty to seventy percent, and optimally between about fifty five to sixty percent. It is currently believed that this is the preferred range required to minimize the amount of acrylic thermoplastic yet still hold the superconductor particles together. Samples made with lower amounts of acrylic do not hold together as well, tending to deteriorate with time.
- the phenomena of a maximum load bearing capacity for the superconductor composite may result from two factors.
- a pure type II superconductor exhibits magnetic flux pinning, which is the result of a magnetic field being induced into the superconductor.
- the superconductor resists change or displacement of this induced magnetic field. Further, repulsive forces arise from the interaction of the pinned magnetic field with the remaining external magnetic field.
- the superconductor particles in the superconductor composite also exhibit flux pinning properties. A portion of the magneti" r lux can be visualized as penetrating the composites' ac./lic matrix along the magnetically invisible acrylic thermoplastic between the discreet superconductor particles held in the acrylic matrix.
- the magnetic flux traversing through the acrylic matrix is pinned in at least partially pinned in the superconductor particles.
- the interaction of this phenomena between and about the superconducting particles in the acrylic matrix changes the nature of the magnetic field internal to the composite, potentially increasing the flux-pinning property as viewed from a position external to the superconductor composite.
- the second factor concerns the magnetic fields established in the superconductor particles to support the flux pining magnetic fields.
- the acrylic matrix separates the superconducting particles.
- the magnetic fields are constrained in the individual superconducting particles, polarizing the individual particles with the axes of polarity being all generally in alignment along the magnetic field lines of the inducing magnetic field.
- Journal and thrust bearings can be constructed from the superconducting composite described above.
- T c critical temperature
- a rare earth cylindrical magnet 20, magnetized axially, is positioned near a surface of a superconductor composite disk 22.
- the magnet 20 is levitated above the surface of the disk 22.
- the magnet 20 can spin on its axis with very little resistance for essentially any orientation of the magnetic axis except parallel to the plane of the surface of the disk 22, and it exhibits a resistance to both axial and radial applied forces. This is attributed to flux pinning within the superconductor composite disk 22.
- the magnetic field pinned in the disk 22 is symmetrical and constant for any angular position of the magnet 20 about its magnetic axis.
- rotation of the magnet 20 about its magnetic axis does not alter the magnetic flux that is pinned in the superconducting material of the disk 22.
- translation of the magnet 20 in either the radial or axial direction, or a change in orientation of the magnetic axis changes the distribution of magnetic flux pinned in the disk 22. Because the Type II superconductor resists any change in a pinned magnetic flux, there arises a resisting force which counters the translation or change in orientation.
- An exemplary thrust bearing has an 18 Mega-Gauss Oersted (MGO) , samarium-cobalt magnet 20 and a disk 22 that is 0.6 cm thick and 1.8 cm in diameter.
- MGO Mega-Gauss Oersted
- samarium-cobalt magnet 20 and a disk 22 that is 0.6 cm thick and 1.8 cm in diameter.
- the gap between the magnet 20 and disk 22 ranges between 0.025 and 0.05 centimeters.
- a plot of the radial (perpendicular to shaft axis) load capacity is shown in Fig. 6, and a plot of the axial (parallel to shaft axis) thrust load capacity is shown in Fig. 7.
- the axial stiffness was measured at 0.34 kgf/cm 2 per bearing for a 0.05 cm. gap.
- a rare earth cylindrical magnet 20' magnetized axially, is placed inside a hollow cylinder 22' made of the superconducting composite described above. The cylinder 22' is chilled below the superconductor's critical temperature T e .
- the magnet 20* levitates axially within the superconductor composite cylinder 22' .
- the cylindrical magnet 20' can be easily made to spin on its axis with very little resistance.
- the magnet 20' exhibits a resistance to both axial and radial applied forces.
- An exemplary journal bearing has an 18 Mega-Gauss
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Mechanical Engineering (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
- Sliding-Contact Bearings (AREA)
- Inorganic Compounds Of Heavy Metals (AREA)
Applications Claiming Priority (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US65171991A | 1991-02-06 | 1991-02-06 | |
US651839 | 1991-02-06 | ||
US07/652,341 US5126611A (en) | 1991-02-06 | 1991-02-06 | Composite superconductor disc bearing |
US07/651,839 US5130588A (en) | 1991-02-06 | 1991-02-06 | Cylindrical composite superconductor bearing |
US651719 | 1991-02-06 | ||
US652341 | 2000-08-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
EP0570525A1 true EP0570525A1 (de) | 1993-11-24 |
Family
ID=27417867
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19920907270 Withdrawn EP0570525A1 (de) | 1991-02-06 | 1992-02-05 | Supraleitende verbindung |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0570525A1 (de) |
JP (1) | JPH06505832A (de) |
WO (1) | WO1992014271A1 (de) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2999607B2 (ja) * | 1991-09-30 | 2000-01-17 | 日本精工株式会社 | 超電導軸受装置とその操作方法 |
US5747426A (en) * | 1995-06-07 | 1998-05-05 | Commonwealth Research Corporation | High performance magnetic bearing systems using high temperature superconductors |
EP0817284A1 (de) * | 1996-06-25 | 1998-01-07 | Hitachi Europe Limited | Supraleitende Struktur |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB8821446D0 (en) * | 1987-09-24 | 1988-10-12 | Ici Plc | Superconducting shaped article |
US4892863A (en) * | 1988-09-30 | 1990-01-09 | Eastman Kodak Company | Electric machinery employing a superconductor element |
US4954481A (en) * | 1988-12-29 | 1990-09-04 | The United States Of America As Represented By The Secretary Of Commerce | Superconductor-polymer composites |
US4956571A (en) * | 1989-03-01 | 1990-09-11 | Mpb Corporation | Superconducting magnetic bearing |
-
1992
- 1992-02-05 EP EP19920907270 patent/EP0570525A1/de not_active Withdrawn
- 1992-02-05 JP JP4507033A patent/JPH06505832A/ja active Pending
- 1992-02-05 WO PCT/US1992/000889 patent/WO1992014271A1/en not_active Application Discontinuation
Non-Patent Citations (1)
Title |
---|
See references of WO9214271A1 * |
Also Published As
Publication number | Publication date |
---|---|
JPH06505832A (ja) | 1994-06-30 |
WO1992014271A1 (en) | 1992-08-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 19930730 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): DE FR GB |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: SAVILLE, MARSHALL, P. Inventor name: RIGNEY, THOMAS K. Inventor name: ESOPA, JOHN, R. Inventor name: ARMSTRONG, TIMOTHY, R. |
|
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: ALLIEDSIGNAL INC. |
|
RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: SAVILLE, MARSHALL, P. Inventor name: RIGNEY, THOMAS K. Inventor name: ESOPA, JOHN, R. Inventor name: ARMSTRONG, TIMOTHY, R. |
|
17Q | First examination report despatched |
Effective date: 19950220 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 19950704 |