EP0570525A1 - Supraleitende verbindung - Google Patents

Supraleitende verbindung

Info

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Withdrawn
Application number
EP19920907270
Other languages
English (en)
French (fr)
Inventor
Timothy R. Armstrong
John R. Esopa
Thomas K. Rigney
Marshall P. Saville
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honeywell International Inc
Original Assignee
AlliedSignal Inc
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from US07/652,341 external-priority patent/US5126611A/en
Priority claimed from US07/651,839 external-priority patent/US5130588A/en
Application filed by AlliedSignal Inc filed Critical AlliedSignal Inc
Publication of EP0570525A1 publication Critical patent/EP0570525A1/de
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/0408Passive magnetic bearings
    • F16C32/0436Passive 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
    • F16C32/0438Passive 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
    • HELECTRICITY
    • H10SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10NELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N60/00Superconducting devices
    • H10N60/80Constructional details
    • H10N60/85Superconducting active materials
    • H10N60/855Ceramic superconductors
    • H10N60/857Ceramic 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)
EP19920907270 1991-02-06 1992-02-05 Supraleitende verbindung Withdrawn EP0570525A1 (de)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
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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Inventor name: SAVILLE, MARSHALL, P.

Inventor name: RIGNEY, THOMAS K.

Inventor name: ESOPA, JOHN, R.

Inventor name: ARMSTRONG, TIMOTHY, R.

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Owner name: ALLIEDSIGNAL INC.

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Inventor name: SAVILLE, MARSHALL, P.

Inventor name: RIGNEY, THOMAS K.

Inventor name: ESOPA, JOHN, R.

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