The present invention relates to high-temperature superconductive devices and assemblies. More particularly, the present invention relates to assemblies which include magnets, motors, or generators wound with high-temperature superconducting wires and tapes coated with dielectric ceramic insulators.
Magnets, motors and generators wound with high-temperature superconducting wires and tapes are of great interest for a variety of applications, including use in both military and commercial applications. Conventional applications have generally utilized magnets which were operated in superconducting states at temperatures ranging from 20-30 K. Such conventional applications require refrigeration systems that are large and heavy, and thus inefficient and costly. If magnets were placed in superconducting environments operating near 77 K this would relieve most of these refrigeration penalties, however quench protection would become a secondary issue at these higher temperatures.
Quench protection prevents a magnet from self-destructing during use in a superconductive environment. During operation often a portion, or zone, of the superconductor wound around the magnet will lose its superconductivity and become resistive at this “normal” zone. Due to the large electrical current, this normal zone will rapidly increase in temperature, thus causing neighboring regions to heat and also become normal zones. This propagation of normal zones can ultimately destroy the magnet. As such, a quench protection mechanism is needed to prevent such a failure from taking place.
Quench protection becomes increasingly important as the temperature is increased from 20-30 K to 77 K because the thermal diffusivity of the superconductor decreases and the quench propagation velocity slows to a few cm/sec, causing the magnet energy to be discharged rapidly into a small volume, thereby possibly destroying the magnet. Thus, improved methods of quench protection are needed to allow a superconductor to operate at higher temperatures (above 30 K) in order to minimize refrigeration size and weight.
According to one embodiment, a high-temperature superconductive device includes a superconducting substrate and a dielectric ceramic insulator. The superconducting substrate comprises a superconducting material having superconductive properties above about 60 K. The dielectric ceramic insulator is applied to the superconducting substrate. The dielectric ceramic insulator comprises a thermal conductivity of at least about 0.2 W/cm-K at a temperature ranging from about 60 K to about 90 K and has a grain size of at least about 2 microns.
According to another embodiment, a high-temperature superconductive assembly includes a superconducting substrate, a dielectric ceramic insulator and a superconductive structure. The superconducting substrate comprises a superconducting material in the form of a tape or wire having superconductive properties above about 60 K. The dielectric ceramic insulator is applied to the superconducting substrate. The dielectric ceramic insulator comprises ZnO, or in the alternative, Zn2GeO4. The superconductive structure consists of a magnet, motor or generator and is adapted to be wound with the superconducting substrate to provide quench protection.
The following detailed description of specific embodiments of the present invention can be best understood when read in conjunction with the following figures, where like structure is indicated with like reference numerals and in which:
Generally various embodiments of the present invention relate to high-temperature superconductive devices and assemblies. Such high-temperature superconductive devices and assemblies are directed for use in environments requiring less refrigeration than low-temperature superconducting systems (20 K -30 K) thus providing more efficient and less costly options for a variety of uses and applications.
Referring initially to
The dielectric ceramic insulator 14 is applied to the superconducting substrate 12 and can be done so through a variety of methods. For example, such applications can include applying the dielectric ceramic insulator 14 to the superconducting substrate 12 by sputtering, ion-beam-assisted sputtering, pulsed laser deposition, or chemical vapor deposition. The dielectric ceramic insulator 14 has a thermal conductivity of at least about 0.2 W/cm-K at every temperature in a range from about 60 K to about 90 K. This large thermal conductivity in such a temperature range provides quench protection for the superconducting material in the high-temperature superconducting environment. For example, heat generated in a normal zone of the superconducting material will dissipate efficiently through the dielectric ceramic insulator, thus preventing the normal zone on the superconducting material from propagating, and thus destroying the superconductor.
In addition to the thermal conductive qualities of the dielectric ceramic insulator 12, such insulators 12 utilized in the high-temperature superconductive device 10 as shown in
According to one embodiment of the present invention, two dielectric ceramic insulators, ZnO and Zn2GeO4, can be used as part of the high-temperature superconductive device because these dielectric ceramic insulators have large thermal conductivities at lower temperatures in general and more specifically near 77 K. Thus, both ZnO and Zn2GeO4 provide sufficient quench protection to the superconducting material so that the superconducting material can operate at higher temperatures (i.e., 60 K to 90 K), thus minimizes refrigeration size and weight.
It is important to note that the data for ZnO in the
Referring now to
It is noted that terms like “preferably,” commonly,” and “typically,” when utilized herein, should not be read to limit the scope of the claimed invention or to imply that certain features are critical, essential, or even important to the structure or function of the claimed invention. Rather, these terms are merely intended to highlight alternative or additional features that may or may not be utilized in a particular embodiment of the present invention.
Having described the invention in detail and by reference to specific embodiments thereof, it will be apparent that modifications and variations are possible without departing from the scope of the invention defined in the appended claims. More specifically, although some aspects of the present invention are identified herein as preferred or particularly advantageous, it is contemplated that the present invention is not necessarily limited to these preferred aspects of the invention.
The present application is filed under 35 U.S.C. 111(a) as a continuation-in-part of international patent application no. PCT/US2006/016511 (LAE 0034 PB), filed Apr. 28, 2006, which international application designates the United States and claims the benefit of U.S. Provisional Application Ser. No. 60/677,521 (LAE 0034 MA), filed May 4, 2005.
Number | Date | Country | |
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60677521 | May 2005 | US |
Number | Date | Country | |
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Parent | PCT/US2006/016511 | Apr 2006 | US |
Child | 11934439 | US |